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_ T. i- -'14:CICE COPY OFFICE COPY 6. 5 _.. OFFICE COPY ENGINEERING DATA RECEIVED DEC 212021 • CRE CR SCRE CITY OFTIGARD f BUILDING DIVISION l'I Core Velocity(fpm) 300 400 500 600 700 800 1000 1200 1400 Nominal Nominal Core Velocity Pressure 0.006 0.010 0.016 0.022 0.031 0.040 0.062 0.090 0.122 Duct Size Duct Area Area 1" Neg.Static Pressure 0.013 0.024 0.037 0.054 0.073 0.096 0.150 0.216 0.294 (in.) (ft.2) (ft.2) 1/2" Neg.Static Pressure 0.013 0.024 0.037 0.053 0.073 0.095 0.148 0.213 0.290 ) Airflow(CFM) 57 76 95 114 133 152 160 228 266 6x6 0.25 0.19 NC - - 11 16 20 28 34 39 i Airflow(CFM) 78 104 130 156 182 208 260 312 364 8x6 0.33 0.26 NC - - 12 17 22 29 35 40 !' 102 136 170 204 238 272 340 408 476 10x6 0.42 0.34 Airflow(CFM) NC - - - 13 19 23 30 36 41 i st 111 148 185 222 259 296 370 444 518 8x8 0.44 0.37 Airflow(CFM) t NC - - - 14 19 23 31 37 42 ' Airflow(CFM) 123 164 205 246 287 328 410 492 574 12x6 0.5 0.41 NC - - 14 19 24 31 37 42 Airflow(CFM) 144 192 240 288 336 384 480 576 672 9 14x6 0.58 0.48 NC - - - 15 20 24 32 38 43 a. 16x6 Airflow(CFM) 171 228 285 342 399 456 570 684 798 12x8 0.67 0.57 NC - - - 16 21 25 33 38 44 a) (/) ' , Airflow(CFM) 177 236 295 354 413 472 590 708 826 .� 10x10 0.69 0.59 NC - 16 21 25 33 39 44 - . (I) v Airflow(CFM) 189 252 315 378 441 504 630 756 882 18x6 0.75 0.63 NC - 16 21 26 33 39 44 20x6 Airflow(CFM) 216 288 360 432 504 576 720 864 1008 0.83 0.72 12x10 NC - - 11 17 22 26 34 40 45 Notes: 1. Static pressures are negative,in.wc,tested in accordance with ANSI/ASHRAE 70-1991. 2. NC based on room absorption of 10dB,re 10'2 watts,tested in accordance with ANSI/ASHRAE 70-1991. 3. Dash"-"indicates NC value less than 10. Y C/EC— CD 7� {112 5ZA — V l9 r ' j rjVv II6Iv�A GR150 7/14 www.tuttleandbailey.com ` Ty_, ENGINEERING DATA CRE, CR, SCRE Core Velocity(fpm) 300 400 500 600 700 800 1000 1200 1400 Nominal Nominal Core Velocity Pressure 0.006 0.010 0.016 0.022 0.031 0.040 0.062 0.090 0.122 Duct Size Duct Area Area 1" Neg.Static Pressure 0.013 0.024 0.037 0.054 0.073 0.096 0.150 0.216 0.294 (in.) (ft•2) (ft!) 1/2" Neg.Static Pressure 0.013 0.024 0.037 0.053 0.073 0.095 0.148 0.213 0.290 Airflow(CFM) 231 308 385 462 539 616 770 924 1078 ", 22x6 0.92 0.77 NC - - 11 17 22 26 34 40 45 24x6 Airflow(CFM) 264 352 440 528 616 704 880 1056 1232 12x12 1.00 0.88 NC - - 12 18 23 27 34 40 45 30x6 Airflow(CFM) 333 444 555 666 777 888 1110 1332 1554 1.25 1.11 18x10 NC 13 19 24 28 35 41 46 Airflow(CFM) 366 488 610 732 854 976 1220 1464 1708 14x14 1.36 1.22 NC - - 13 19 24 28 36 42 47 Airflow(CFM) 405 540 675 810 945 1080 1350 1620 1890 36x6 1.5 1.35 NC - - 14 19 25 29 36 42 47 Airflow(CFM) 411 548 685 822 959 1096 1370 1644 1918 22x10 1.53 1.37 NC - - 14 20 25 29 36 42 47 30x8 Airflow(CFM) 447 596 745 894 1043 1192 1490 1788 2086 1.67 1.49 24x10 NC - - 14 20 25 29 37 43 48 Ax W I Airflow(CFM) 477 636 795 954 1113 1272 1590 1908 2226 (/) 42x6 1.75 1.59 NC _ 14 20 25 30 37 43 48 Airflow(CFM) 486 648 810 972 1134 1296 1620 1944 2268 r1 id 16x16 1.78 1.62 NC 14 20 25 30 37 43 48 24x12 Airflow(CFM) 546 728 910 1092 1274 1456 1820 2184 2548 18x16 2 1.82 NC - - 15 21 26 30 38 44 49 Notes: 1. Static pressures are negative,in.wc,tested in accordance with ANSI/ASHRAE 70-1991. 2. NC based on room absorption of 10dB,re 10-'2 watts,tested in accordance with ANSI/ASHRAE 70-1991. 3. Dash""indicates NC value less than 10. www.tuttleandbailey.com 7/14 GR151 1` T613 ENGINEERING DATA CRE, CR, SCRE Core Velocity(fpm) 300 400 500 600 700 800 1000 1200 1400 Nominal Nominal Core Velocity Pressure 0.006 0.010 0.016 0.022 0.031 0.040 0.062 0.090 0.122 Duct Size Duct Area Area 1" Neg.Static Pressure 0.013 0.024 0.037 0.054 0.073 0.096 0.150 0.216 0.294 (in.) (ft.2) (ft•2) 1/2" Neg.Static ';. Pressure 0.013 0.024 0.037 0.053 0.073 0.095 0.148 0.213 0.290 Airflow(CFM) 621 828 1035 1242 1449 1656 2070 2484 2898 18x18 2.25 2.07 NC ', - - 15 21 26 31 38 44 49 , Airflow(CFM) 642 856 1070 1284 1498 1712 2140 2568 2996 24x14 2.33 2.14 NC - - 16 21 27 31 38 44 49 30x12 2.50 2.29 Airflow(CFM) 687 916 1145 1374 1603 1832 2290 2748 3206 NC - - 16 22 27 31 39 45 50 Airflow(CFM) 738 984 1230 1476 1722 1968 2460 2952 3444 t! 24x16 2.67 2.46 NC ) - - 16 22 27 32 39 45 50 ( )". I 771 1028 1285 1542 1799 2056 2570 3084 3598 `r 20x20 2.78 2.57 AirfIoNC(CFM) 16 22 27 32 39 45 50 F - e Airflow(CFM) 825 1100 1375 1650 1925 2200 2750 3300 3850 36x12 3.00 2.75 NC 17 23 28 32 39 45 50 '' 30x16 Airflow(CFM) 933 1244 1555 1866 2177 2488 3110 3732 4354 " 24x20 3.33 3.11 NC - - 17 23 28 33 40 46 51 N N a--: Airflow(CFM) 942 1256 1570 1884 2198 2512 3140 3768 4396 22x22 3.36 3.14 NC - - 17 23 28 33 40 46 51 1 fLn n'', v Airflow(CFM) 966 1288 1610 1932 2254 2576 3220 3864 4508 l 42x12 3.5 3.22 NC - 17 23 28 33 40 46 51 ii Airflow(CFM) 1029 1372 1715 2058 2401 2744 3430 4116 4802 1 24x22 3.67 3.43 NC - - 18 24 29 33 40 46 51 I j Notes: I 1. Static pressures are negative,in.wc,tested in accordance with ANSI/ASHRAE 70-1991. 2. NC based on room absorption of 10dB,re 10 12 watts,tested in accordance with ANSI/ASHRAE 70-1991. 3. Dash"-' indicates NC value less than 10. il GR152 7/14 www.tuttleandbailey.com T ENGINEERING DATA - CRE, CR, SCREr _ Core Velocity(fpm) 300 400 500 600 700 800 1000 1200 1400 Nominal Nominal Core Velocity Pressure 0.006 0.010 0.016 0.022 0.031 0.040 0.062 0.090 0.122 Duct Size Duct Area Area 1" Neg.Static Pressure 0.013 0.024 0.037 0.054 0.073 0.096 0.150 0.216 0.294 (in.) (ft•2) (ft.2) 1/2" Neg.Static Pressure 0.013 0.024 0.037 0.053 0.073 0.095 0.148 0.213 0.290 Airflow(CFM) 1050 1400 1750 2100 2450 2800 3500 4200 4900 30x18 3.75 3.50 NC 18 24 29 33 40 46 51 48x12 Airflow(CFM) 1125 1500 1875 2250 2625 3000 3750 4500 5250 I 24x24 4.00 3.75 NC - 11 18 24 29 33 41 47 52 1 Airflow(CFM) 1266 1688 2110 2532 2954 3376 4220 5064 5908 36x18 4.50 4.22 NC 11 18 24 29 34 41 47 52 36x20 Airflow(CFM) 1413 1884 2355 2826 3297 3768 4710 5652 6594 5.00 4.71 30x24 NC - 12 19 25 30 34 42 48 53 Airflow(CFM) 1482 1976 2470 2964 3458 3952 4940 5928 6916 42x18 5.25 4.94 NC 12 19 25 30 35 42 48 53 Airflow(CFM) 1548 2064 2580 3096 3612 4128 5160 6192 7224 28x28 5.44 5.16 NC 12 19 25 30 35 42 48 53 42x20 Airflow(CFM) 1653 2204 2755 3306 3857 4408 5510 6612 7714 5.83 5.51 30x28 NC - 12 20 26 31 35 42 48 53 ,,x w 1 48x18 Airflow(CFM) 1698 2264 2830 3396 3962 4528 5660 6792 7924 Cl) 6.00 5.66 a) 36x24 NC - 12 20 26 31 35 42 48 54 — iv 1- 1 Airflow(CFM) 1782 2376 2970 3564 4158 4752 5940 7128 8316 v Id 30x30 6.25 5.94 NC 13 20 26 31 35 43 49 54 42x24 Airflow(CFM) 1998 2664 3330 3996 4662 5328 6660 7992 9324 7.00 6.66 36x28 NC - 13 20 26 31 36 43 49 54 Notes: 1. Static pressures are negative,in.wc,tested in accordance with ANSI/ASHRAE 70-1991. 2. NC based on room absorption of 10dB,re 10-12 watts,tested in accordance with ANSI/ASHRAE 70-1991. 3. Dash"-"indicates NC value less than 10. www.tuttleandbailey.com 7/14 GR153 -. i ENGINEERING DATA :.: CRE CR SCRE i Core Velocity(fpm) 300 400 500 600 700 800 1000 1200 1400 Ai( Nominal Nominal Core Velocity Pressure 0.006 0.010 0.016 0.022 0.031 0.040 0.062 0.090 0.122 - Duct Size Duct Area Area 1" Neg.Static Pressure 0.013 0.024 0.037 0.054 0.073 0.096 0.150 0.216 0.294 i (in.) (ft•2) (ft!) .Y :..• 1/2" Neg.Static Pressure 0.013 0.024 0.037 0.053 0.073 0.095 0.148 0.213 0.290 Airflow(CFM) 2004 2672 3340 4008 4676 5344 6680 8016 9352 46x22 7.03 6.68 NC - 13 20 26 31 36 43 49 54 Airflow(CFM) 2034 2712 3390 4068 4746 5424 6780 8136 9492 32x32 7.11 6.78 NC 13 21 26 32 36 43 49 54 li Airflow(CFM) 2148 2864 3580 4296 5012 5728 7160 8592 10024 36x30 7.50 7.16 NC 13 21 27 32 36 43 49 55 48x24 Airflow CFM 2289 3052 3815 4578 5341 6104 7630 9156 10682 8.00 7.63 (CFM) 36x32 NC - 14 21 27 32 36 44 50 55 Airflow(CFM) 2304 3072 3840 4608 5376 6144 7680 9216 10752 34x34 8.03 7.68 NC 14 21 27 32 36 44 50 55 .1 i Airflow(CFM) 2442 3256 4070 4884 5698 6512 8140 9768 11396 36x34 8.50 8.14 NC 14 21 27 32 37 44 50 55 Airflow(CFM) 2514 3352 4190 5028 5866 6704 8380 10056 11732 42x30 8.75 8.38 NC 14 21 27 32 37 44 50 55 - p� 36x36 9.00 8.63 Airflow(CFM) 2589 3452 4315 5178 6041 6904 8630 10356 12082 NC - 14 22 28 33 37 44 50 55 N ' = 0 42x34 Airflow(CFM) 2880 3840 4800 5760 6720 7680 9600 11520 13440 L 48x30 10.00 9.6 NC 15 22 28 33 37 45 51 56 1 t Airflow(CFM) 2892 3856 4820 5784 6748 7712 9640 11568 13496 e, 38x38 10.03 9.64 NC - 15 22 28 33 37 45 51 56 f iIi Airflow(CFM) 3030 4040 5050 6060 7070 8080 10100 12120 14140 42x36 10.50 10.1 NC I15 22 28 33 38 45 51 56 Airflow(CFM) 3135 4180 5225 6270 7315 8360 10450 12540 14630 { 46x34 10.86 10.45 NC 1 - 15 22 28 33 38 45 51 56 Notes: + 1. Static pressures are negative,in.wc,tested in accordance with ANSI/ASHRAE 70-1991. 11 2. NC based on room absorption of 10dB,re 10-12 watts,tested in accordance with ANSI/ASHRAE 70-1991. i 3. Dash"-"indicates NC value less than 10. 1 i GR154 7/14 www.tuttleandbailey.com T6 B PRODUCT DIMENSIONS l CRE, CR SF Margin Style Model A B Models: CRE500, CRE510, CRE1000 1/2 RE�00/2 1-1/16 2-9/16 j Duct plus 13/4 - grid core Duct minus 3/4 --11/4H 1 CRE510* 3"s 1/2 x 1/2 x 1 1-9/16 3-1/16 grid core /I B_ + CRE1000 Optional �y j Dam g x 1 x 1 1-9/16 3-1/6 , Opposed Blade J� rid core F , Duct minus 1/2 *CRE510 core consists of two Nominal Duct Size - 1/2 x 1/2 x 1/2 cores stacked U Frame Core Only Models: CR5000, CR510U, CR1000U Models: CR500C, CR510C, CR1000C + C e � , f f �►G►G►� A Nl /F'�,�'�/ i H = 1/2 for 1/2 x 1/2 x 1/2 �i��I�� 11 I Duct-1/a Grid Core A=5/8 I I Ceiling Module Size B=1 I� 1 H = 1 for 1/2 x 1/2 x 1, ( minus 114 C=3/8 �II� and 1"x 1"x 1"Grid Cores \I/Duct-1/4 a)06 NR Margin Style a) LT Margin Style a) Models: CRE500, CRE510, CRE1000 = CD Models: CRE500, CRE510, CRE1000 s— Q) 24 0 CC ,- Duct-1/2 - Optional Opposed a;.Q e /Blade Damper a• ,a.. - -/ 0 I a.. ' ..=1111111.11.111111111111111 _ 1---. 1 Eil L..........I inCeiling Module Size minus 1/4 1 kDuct-3/4 1 23-3/8 - - 23-3/4 - GR148 7/14 www.tuttleandbailey.com Dimensions In Inches T B PRODUCT DIMENSIONS SCRE Model A B I CRE500 1/2 x 1/2 x1/2 1-1/16 2-9/16 grid core CRE510* SF Margin Style 1/2 x 1/2 x 1 1-9/16 3-1/16 <' Models: SCRE500, SCRE510, SCRE1000 grid core CRE1000 1 x 1 x 1 1-9/16 3-1/6 --ft Duct plus 1 3/4 grid core Duct minus 3/4 *CRE510 core consists of two -- 1 1/4 --.*— 1/4 1/2 x 1/2 x 1/2 cores stacked Aluminum Core l / 1 Steel Margin Imo— 1 VIA 1 B Optional Opposed Blade Damper --.1— Duct minus 1/2 Nominal Duct Size LT Margin Style 'l` Models: SCRE500, SCRE510, SCRE1000 t oo 1 N^` 9- aa W - .•v a21j • �/ Ceiling Module Size minus 1/4 Dimensions In Inches www.tuttleandbailey.com 7/14 GR149 .. TT, ENGINEERING DATA T50, T60, T52, T62, T54, T64 Core Vel.(fpm) _ 300 400 500 600 700 800 1000 1200 1400 Vel.Pressure 0.006 0.010 0.016 0.022 0.031 0.040 0.062 0.090 0.122 Nom Duct Size 0° 0.016 0.029 0.046 0.066 0.090 0.117 0.183 0.263 0.358 Total Pressure 22.5° 0.018 0.033 0.051 0.074 0.100 0.131 0.204 0.294 0.401 45° 0.028 0.049 0.077 0.111 0.152 0.198 0.309 0.445 0.606 Airflow(CFM) 57 76 95 114 133 152 190 228 266 0° 5-7-14 7-10-16 8-12-18 10-14-20 12-15-21 13-16-23 15-18-25 16-20-28 17-21-30 6x6 Throw(ft.) 22.5° 4-6-11 5-8-12 6-10-14 8-11-15 9-12-16 10-12-18 11-14-20 12-15-22 13-16-23 45° 2-3-6 3-4-7 4-6-8 4-6-9 5-7-10 6-7-10 7-8-11 7-9-12 8-10-13 NC - - - 15 20 24 31 36 41 Airflow(CFM) 78 104 130 156 182 208 260 312 364 0° 5-9-16 8-12-19 10-15-21 12-16-23 14-18-25 15-19-27 17-21-30 19-23-32 20-25-35 8x6 Throw(ft.) 22.5° 4-7-13 6-9-15 8-11-16 9-13-18 11-14-19 12-15-21 13-16-23 15-18-25 16-19-27 45° 2-4-7 3-5-8 4-7-9 5-7-10 6-8-11 7-8-12 8-9-13 8-10-15 9-11-16 NC - - 11 17 21 • 25 32 38 42 Airflow(CFM) 102 136 170 204 238 272 340 408 476 0° 6-10-19 9-13-21 11-17-24 13-19-26 16-20-28 18-21-30 20-24-34 21-26-37 23-28-40 10x6 Throw(ft.) 22.5° 5-8-14 7-10-17 9-13-19 10-14-20 12-16-22 14-17-23 15-19-26 17-20-29 18-22-31 45° 3-4-8 4-6-10 5-7-11 6-8-12 7-9-13 8-10-14 9-11-15 10-12-17 10-13-18 NC - - 12 18 23 27 33 39 43 Airflow(CFM) 111 148 185 222 259 296 370 444 518 0° 6-10-19 9-14-22 12-17-25 14-19-27 16-21-30 18-22-32 20-25-35 22-27-39 24-30-42 8x8 Throw(ft.) 22.5° 5-8-15 7-11-17 9-13-19 11-15-21 13-16-23 14-17-25 16-19-27 17-21-30 19-23-32 45° 3-5-9 4-6-10 5-8-11 6-9-12 7-9-13 8-10-14 9-11-16 10-12-17 11-13-19 NC - - 13 18 23 27 34 39 44 Airflow(CFM) 123 164 205 246 287 328 410 492 574 0° 7-11-20 10-15-24 12-18-26 15-20-29 17-22-31 19-24-33 21-26-37 24-29-41 25-31-44 12x6 Throw(ft.) 22.5° 5-8-16 8-11-18 9-14-20 11-16-22 13-17-24 15-18-26 17-20-29 18-22-32 20-24-34 45° 3-5-9 4-7-11 5-8-12 7-9-13 8-10-14 9-11-15 10-12-17 11-13-18 11-14-20 NC - - 13 19 23 27 34 40 44 06 Airflow(CFM) 144 192 240 288 336 384 480 576 672 Cn 0° 7-12-22 11-16-25 13-20-28 16-22-31 18-24-34 21-25-36 23-28-40 25-31-44 28-34-48 14x6 Throw(ft.) 22.5° 6-9-17 8-12-20 10-15-22 12-17-24 14-18-26 16-20-28 18-22-31 20-24-34 21-26-37 - �, 45° 3-5-10 5-7-11 6-9-13 7-10-14 8-11-15 9-11-16 10-13-18 11-14-20 12-15-21 • NC - - 14 19 24 28 35 40 45 (^ ea Airflow(CFM) 171 228 285 342 399 456 570 684 798 �/ 0° 8-13-24 11-17-28 14-22-31 17-24-34 20-26-37 23-28-39 25-31-44 28-34-48 30-37-52 16x6 Throw(ft.) 22.5° 6-10-19 9-13-22 11-17-24 13-19-26 16-20-28 18-22-30 20-24-34 22-26-37 23-28-40 12x8 45° 4-6-11 5-8-12 6-10-14 8-11-15 9-12-17 10-12-18 11-14-20 12-15-22 13-17-23 NC - - 15 20 25 29 35 41 45 Notes: 1. Tests conducted in accordance with ANSI/ASHRAE 70-1991 at isothermal conditions. 2. Tests conducted with a straight rigid inlet condition. Other inlet conditions may alter performance. 3. Performance data includes damper in the full open position. 4. 0°,22.5°and 45°represent blade deflection angles. 5. Units:Face Velocity=fpm;Total Pressure=in.we 6. Throw based on terminal velocities of 150 fpm,100 fpm and 50 fpm. 7. NC is based upon 10dB room absorption(Re:10-12 watts)evaluated at 125 through 4000 Hz octave bands. 8. Dash"-"indicates NC value less than 10. www.tuttleandbailey.com 7/14 GR17 T C i : '-t:: ENGINEERING DATA T50, T60, T52, T62, T54, T64 rlCore Vel.(fpm) 300 400 500 600 700 800 1000 1200 1400 } Nom Duct Vel.Pressure 0.006 0.010 0.016 0.022 0.031 0.040 0.062 0.090 0.122 11 Size 0° 0.016 0.029 0.046 0.066 0.090 0.117 0.183 0.263 0.358 Total Pressure 22.5° 0.018 0.033 0.051 0.074 0.100 0.131 0.204 0.294 0.401 45° 0.028 0.049 0.077 0.111 0.152 0.198 0.309 0.445 0.606 Airflow(CFM) 177 236 295 354 413 472 590 708 826 00 8-13-24 12-18-28 15-22-32 18-24-35 20-26-37 23-28-40 26-32-45 28-35-49 31-37-53 7- 10x10 Throw(ft.) 22.5° 6-10-19 9-14-22 11-17-24 14-19-27 16-20-29 18-22-31 20-24-35 22-27-38 24-29-41 45° 4-6-11 5-8-13 7-10-14 8-11-16 9-12-17 10-13-18 12-14-20 13-16-22 14-17-24 ( NC - - 15 20 25 29 35 41 46 Airflow(CFM) 189 252 315 378 441 504 630 756 882 j 0° 8-14-25 12-18-29 15-23-33 18-25-36 21-27-39 24-29-41 27-33-46 29-36-51 32-39-55 18x6 Throw(ft.) 22.5° 7-11-20 9-14-23 12-18-25 14-20-28 16-21-30 18-23-32 21-25-36 23-28-39 24-30-42 450 4-6-11 5-8-13 7-10-15 8-11-16 9-12-17 11-13-19 12-15-21 13-16-23 14-17-25 NC - 15 20 25 29 36 41 46 Airflow(CFM) 216 288 360 432 504 576 720 864 1008 0° 9-15-27 13-19-31 16-24-35 19-27-38 23-29-41 25-31-44 28-35-49 31-38-54 24-41-58 20x6 Throw(ft.) 22.5° 7-11-21 10-15-24 12-19-27 15-21-30 17-23-32 20-24-34 22-27-38 24-30-42 26-32-45 i 12x10 45° 4-7-12 6-9-14 7-11-16 9-12-17 10-13-19 11-14-20 13-16-22 14-17-24 15-19-26 NC - - 16 21 26 30 36 42 46 Airflow(CFM) 231 308 385 462 539 616 770 924 1078 0° 9-15-28 13-20-32 17-25-36 20-28-40 23-30-43 26-32-46 29-36-51 32-40-56 35-43-60 ) 22x6 Throw(ft.) 22.5° 7-12-22 10-16-25 13-19-28 16-22-31 18-23-33 20-25-35 23-28-40 25-31-43 27-33-47 45° 4-7-13 6-9-15 8-11-16 9-13-18 11-14-19 12-15-21 13-16-23 15-18-25 16-19-27 ' NC - - 16 21 26 30 37 42 47 di Airflow(CFM) 264 352 440 528 616 704 880 1056 1232 24x6 0° 10-16-30 14-21-34 18-27-39 21-30-42 25-32-46 28-34-49 31-39-55 34-42-60 37-46-65 18x8 Throw(ft.) 22.5° 8-12-23 11-17-27 14-21-30 17-23-33 19-25-35 22-27-38 24-30-42 27-33-46 29-35-50 12x12 45° 4-7-13 6-10-16 8-12-17 10-13-19 11-15-21 13-16-22 14-17-25 16-19-27 17-21-29 NC - - 16 22 26 30 37 43 47 Ax U) W t` a) Airflow(CFM) 333 444 555 666 777 888 1110 1332 1554 (/) 17 0° 11-18-34 16-24-39 20-30-43 24-34-47 28-36-51 32-39-55 25-43-61 39-47-67 42-51-72 30x6 Throw(ft.) 22.5° 9-14-26 12-19-30 16-23-34 19-26-37 22-28-40 25-30-42 27-34-47 30-37-52 32-40-56 18x10 45° 5-8-15 7-11-17 9-14-19 11-15-21 13-16-23 14-17-25 16-19-28 17-21-30 19-23-33 rrann ��// NC - - 17 23 27 31 38 44 48 V L.1� Airflow(CFM) 366 488 610 732 854 976 1220 1464 1708 0° 12-19-35 17-25-41 21-31-45 25-35-50 29-38-54 33-41-57 37-45-64 41-50-70 44-54-76 14x14 Throw(ft.) 22.5° 9-15-27 13-20-31 16-24-35 20-27-39 23-29-42 26-31-45 29-35-50 31-39-55 34-42-59 45° 5-8-16 8-11-18 9-14-20 11-16-22 13-17-24 15-18-26 17-20-29 18-22-32 20-24-34 tt, s� t a NC - 11 18 23 28 32 39 44 49 Notes: 1. Tests conducted in accordance with ANSI/ASHRAE 70-1991 at isothermal conditions. 2. Tests conducted with a straight rigid inlet condition. Other inlet conditions may alter performance. 3. Performance data includes damper in the full open position. 4. 0°,22.5°and 45°represent blade deflection angles. 5. Units:Face Velocity=fpm;Total Pressure=in.we 6. Throw based on terminal velocities of 150 fpm,100 fpm and 50 fpm. 7. NC is based upon 10dB room absorption(Re:10-12 watts)evaluated at 125 through 4000 Hz octave bands. 8. Dash"-"indicates NC value less than 10. GR18 7/14 www.tuttleandbailey.com TSB ENGINEERING DATA T50, T60, T52, T62, T54, T64 Core Vel.(fpm) _ 300 400 500 600 700 800 1000 1200 1400 Vel.Pressure 0.006 0.010 0.016 0.022 0.031 0.040 0.062 0.090 0.122 Nom Duct Size 0° 0.016 0.029 0.046 0.066 0.090 0.117 0.183 0.263 0.358 Total Pressure 22.5° 0.018 0.033 0.051 0.074 0.100 0.131 0.204 0.294 0.401 45° 0.028 0.049 0.077 0.111 0.152 0.198 0.309 0.445 0.606 Airflow(CFM) 405 540 675 810 945 1080 1350 1620 1890 36x6 0° 12-20-37 18-26-43 22-33-48 26-37-52 31-40-57 . 25-43-60 39-48-68 43-52-74 46-57-80 27x8 Throw(ft.) 22.5° 10-15-29 14-21-33 17-26-37 21-29-41 24-31-44 27-33-47 30-37-52 33-41-57 36-44-62 18x12 45° 6-9-17 8-12-19 10-15-21 12-17-24 14-18-25 16-19-27 18-21-30 19-24-33 21-25-36 NC - 12 18 24 28 32 39 44 49 Airflow(CFM) 411 548 685 822 959 1096 1370 1644 1918 0° 12-20-37 18-27-43 22-33-48 27-37-53 31-40-57 35-43-61 39-48-68 43-53-75 46-57-81 22x10 Throw(ft.) 22.5° 10-16-29 14-21-33 17-26-37 21-29-41 24-31-44 27-33-47 30-37-53 33-41-58 36-44-62 45° 6-9-17 8-12-19 10-15-22 12-17-24 14-18-26 16-19-27 18-22-31 19-24-34 21-26-36 NC - 12 18 24 28 32 39 44 49 Airflow(CFM) 447 596 745 894 1043 1192 1490 1788 2086 0° 13-21-39 19-28-45 23-35-50 28-39-55 32-42-59 37-45-63 41-50-71 45-55-78 48-59-84 30x8 Throw(ft.) 22.5° 10-16-30 14-22-35 18-27-39 22-30-43 25-33-46 28-35-49 32-39-55 35-43-60 38-46-65 24x10 45° 6-9-17 8-13-20 10-16-23 13-17-25 15-19-27 16-20-29 18-23-32 20-25-35 22-27-38 NC - 12 19 24 29 33 39 45 49 Airflow(CFM) 477 636 795 954 1113 1272 1590 1908 2256 0° 13-22-40 19-29-46 24-36-52 29-40-57 34-43-61 38-46-66 42-52-73 46-57-80 50-61-87 42x6 Throw(ft.) 22.5° 10-17-31 15-22-36 19-28-40 22-31-44 26-34-48 29-36-51 33-40-57 36-44-62 39-48-67 18x14 45° 6-10-18 9-13-21 11-16-23 13-18-26 15-20-28 17-21-30 19-23-33 21-26-36 23-28-39 NC - 12 19 24 29 33 40 45 50 Airflow(CFM) 486 648 810 972 1134 1296 1620 1944 2268 0° 14-22-41 19-29-47 24-36-52 29-41-57 34-44-62 38-47-66 43-52-74 47-57-81 51-62-88 16x16 Throw(ft.) 22.5° 11-17-31 15-22-36 19-28-41 23-31-44 26-34-48 30-36-51 33-41-57 36-44-63 39-48-68 45° 6-10-18 9-13-21 11-16-24 13-18-26 15-20-28 17-21-30 19-24-33 21-26-36 23-28-39 NC - 12 19 24 29 33 40 45 50 ,max W 1 Airflow(CFM) 546 728 910 1092 1274 1456 1820 2184 2548 Cl) 48x6 0° 14-23-43 20-31-50 26-38-55 31-43-61 36-46-66 41-50-70 45-55-78 50-61-86 54-66-93 _ '�, 36x8 -Throw(ft.) 22.5° 11-18-33 16-24-38 20-30-43 24-33-47 28-36-51 31-38-54 35-43-61 38-47-67 42-51-72 '� 1 24x12 18x16 45° 6-10-19 9-14-22 12-17-25 14-19-27 16-21-30 18-22-32 20-25-35 22-27-39 24-30-42 /9 ,A NC - 13 19 25 30 34 40 46 50 � Airflow(CFM) 621 828 1035 1242 1449 1656 2070 2484 2898 0° 15-25-46 22-33-53 27-41-59 33-46-65 38-49-70 43-53-75 48-59-84 53-65-92 57-70-99 18x18 Throw(ft.) 22.5° 12-19-36 17-25-41 21-32-46 25-36-50 30-38-54 33-41-58 37-46-65 41-50-71 44-54-77 45° 7-11-21 10-15-24 12-18-27 15-21-29 17-22-31 19-24-34 22-27-38 24-29-41 26-31-45 NC - 13 20 25 30 34 41 46 51 Notes: 1. Tests conducted in accordance with ANSI/ASHRAE 70-1991 at isothermal conditions. 2. Tests conducted with a straight rigid inlet condition. Other inlet conditions may alter performance. 3. Performance data includes damper in the full open position. 4. 0°,22.5°and 45°represent blade deflection angles. 5. Units:Face Velocity=fpm;Total Pressure=in.we 6. Throw based on terminal velocities of 150 fpm,100 fpm and 50 fpm. 7. NC is based upon 10dB room absorption(Re:10-12 watts)evaluated at 125 through 4000 Hz octave bands. 8. Dash""indicates NC value less than 10. www.tuttleandbailey.com 7/14 GR19 T6-B ENGINEERING DATA T50, T60, T52, T62, T54, T64 1 Core Vel.(fpm) 300 400 500 600 700 800 1000 1200 1400 Vel.Pressure 0.006 0.010 0.016 0.022 0.031 0.040 0.062 0.090 0.122 Nom Duct Size 0° 0.016 0.029 0.046 0.066 0.090 0.117 0.183 0.263 0.358 Total Pressure 22.5° 0.018 0.033 0.051 0.074 0.100 0.131 0.204 0.294 0.401 45° 0.028 0.049 0.077 0.111 0.152 0.198 0.309 0.445 0.606 Airflow(CFM) 642 856 1070 1284 1498 1712 2140 2568 2996 0° 16-25-47 22-33-54 28-42-60 33-47-66 39-50-71 44-54-76 49-60-85 54-66-93 58-71-101 :i 42x8 Throw(ft.) 22.5° 12-19-36 17-26-42 22-32-47 26-36-51 30-39-55 32-42-59 38-47-66 45-51-72 45-55-78 24x14 ' 45° 7-11-21 10-15-24 13-19-27 15-21-30 18-23-32 20-24-34 22-27-38 24-30-42 26-32-45 NC - 13 20 26 30 34 41 46 51 Airflow(CFM) 687 916 1145 1374 1603 1832 2290 2748 3206 0° 16-26-48 23-34-56 29-43-62 34-48-68 40-52-74 45-56-79 51-62-88 56-68-96 60-74-104 36x10 Throw(ft.) 22.5° 12-20-37 18-27-43 22-33-48 27-37-53 31-40-57 35-43-61 39-48-68 43-53-75 47-57-81 30x12 45° 7-12-22 10-16-25 13-19-28 16-22-31 18-23-33 20-25-35 23-28-40 25-31-43 27-33-47 NC - 14 20 26 30 34 41 47 51 Airflow(CFM) 738 984 1230 1476 1722 1968 2460 2952 3444 0° 17-27-50 24-36-58 30-45-64 36-50-71 42-54-76 47-58-82 53-64-91 58-71-100 62-76-108 48x8 Throw(ft.) 22.5° 13-21-39 18-28-45 23-35-50 28-39-55 32-42-59 36-45-63 41-50-71 45-55-77 48-59-84 I 24x16 j 45° 8-12-22 11-16-26 13-20-29 16-22-32 19-24-34 21-26-37 24-29-41 26-32-45 28-34-49 • NC 14 21 26 31 35 41 47 51 Airflow(CFM) 771 1028 1285 1542 1799 2056 2570 3084 3598 0° 17-27-51 24-37-59 30-46-66 37-51-75 43-55-78 48-59-83 54-66-93 59-72-102 64-78-110 20x20 Throw(ft.) 22.5° 13-21-40 19-28-46 24-35-51 28-40-56 33-43-60 37-46-65 42-51-72 46-56-79 49-60-85 i 45° 8-12-23 11-16-27 14-21-30 16-23-32 19-25-35 22-27-38 24-30-42 27-32-46 29-35-50 NC - 14 21 26 31 35 42 47 52 Airflow(CFM) 825 1100 1375 1650 1925 2200 2750 3300 3850 0° 18-28-53 25-38-61 31-47-68 38-53-75 44-57-81 50-61-86 56-68-96 61-75-106 68-81-114 36x12 Throw(ft.) 22.5° 14-22-41 20-29-47 24-37-53 29-41-58 34-44-63 39-47-67 43-53-75 47-58-82 51-63-88 24x18 45° 8-13-24 11-17-27 14-21-31 17-24-34 20-26-36 22-27-39 25-31-43 27-34-48 30-36-51 „ S L NC - 15 21 27 31 35 42 47 52 N u) .4-, Q.) .- Airflow(CFM) 933 1244 1555 1866 2177 2488 3110 3732 4354 C) 48x10 0° 19-30-56 27-40-65 33-50-72 40-56-79 47-61-86 53-65-92 59-72-103 65-79-112 70-86-121 L Q) 30x16 Throw(ft.) 22.5° 15-23-44 21-31-50 26-39-56 31-44-62 36-47-66 41-50-71 46-56-79 50-62-87 54-66-94 n 24x20 450 8-14-25 12-18-29 15-23-33 18-25-36 21-27-39 24-29-41 27-33-46 29-36-51 32-39-55 �J L.L NC - 15 22 27 32 36 42 48 52 Airflow(CFM) 942 1256 1570 1884 2198 2512 3140 3768 4396 0° 19-30-56 27-40-65 34-50-73 40-56-80 47-61-86 53-65-92 59-73-103 65-80-113 70-86-122 22x22 Throw(ft.) 22.5° 15-23-44 21-31-50 26-39-56 31-44-62 37-47-67 41-50-71 46-56-80 50-62-87 55-67-94 45° 8-14-25 12-18-29 15-23-33 18-25-36 21-27-39 24-29-41 27-33-46 29-36-51 32-39-55 NC - 15 22 27 32 36 42 48 53 Notes: 1. Tests conducted in accordance with ANSI/ASHRAE 70-1991 at isothermal conditions. 2. Tests conducted with a straight rigid inlet condition. Other inlet conditions may alter performance. 3. Performance data includes damper in the full open position. 4. 0°,22.5°and 45°represent blade deflection angles. 5. Units:Face Velocity=fpm;Total Pressure=in.we 6. Throw based on terminal velocities of 150 fpm,100 fpm and 50 fpm. 7. NC is based upon 10dB room absorption(Re:10-12 watts)evaluated at 125 through 4000 Hz octave bands. 8. Dash"-"indicates NC value less than 10. GR20 7/14 www.tuttleandbailey.com Ty, B ENGINEERING DATA T50, T60, T52, T62, T54, T64 Core Vel.(fpm) 300 _ 400 500 600 700 800 1000 1200 1400 Vel.Pressure 0.006 0.010 0.016 0.022 0.031 0.040 0.062 0.090 0.122 Nom Duct Size 0° 0.016 0.029 0.046 0.066 0.090 0.117 0.183 0.263 0.358 Total Pressure 22.5° 0.018 0.033 0.051 0.074 0.100 0.131 0.204 0.294 0.401 45° 0.028 0.049 0.077 0.111 0.152 0.198 0.309 0.445 0.606 Airflow(CFM) 966 1288 1610 1932 2254 2576 3220 3864 4508 0° 19-31-57 27-41-66 34-51-74 41-57-81 48-62-87 54-66-93 60-74-104 66-81-114 71-87-123 42x12 Throw(ft.) 22.5° 15-24-44 21-32-51 26-40-57 32-44-63 37-48-68 42-51-72 47-57-81 51-63-89 55-68-96 36x14 45° 9-14-26 12-18-30 15-23-33 18-26-36 21-28-39 24-30-42 27-33-47 30-36-51 32-39-56 NC - 15 22 27 32 36 43 48 53 Airflow(CFM) 1029 1372 1715 2058 2401 2744 3430 4116 4802 0° 20-32-59 28-42-68 35-53-76 42-59-83 49-64-90 56-68-96 62-76-108 68-83-118 74-90-127 24x22 Throw(ft.) 22.5° 15-25-46 22-33-53 27-41-59 33-46-65 38-49-70 43-53-75 48-59-83 53-65-91 57-70-99 45° 9-14-27 13-19-31 16-24-34 19-27-38 22-29-41 25-31-43 28-34-48 31-38-53 33-41-57 NC - 15 22 28 32 36 43 48 53 Airflow(CFM) 1050 1400 1750 2100 2450 2800 3500 4200 4900 0° 20-32-60 28-34-69 36-53-77 43-60-84 50-64-91 56-69-97 63-77-109 69-84-119 74-91-129 30x18 Throw(ft.) 22.5° 15-25-46 22-33-53 28-41-60 33-46-65 39-50-71 44-53-75 49-60-84 53-65-92 58-71-100 45° 9-14-27 13-19-31 16-24-35 19-27-38 22-29-41 25-31-44 28-35-49 31-38-54 33-41-58 NC - 16 22 28 32 36 43 48 53 Airflow(CFM) 1125 1500 1875 2250 2625 3000 3750 4500 5250 48x12 0° 21-33-62 29-44-71 37-55-80 44-62-87 51-67-94 58-71-101 65-80-113 71-87-123 77-94-133 36x16 Throw(ft.) 22.5° 16-26-48 23-34-55 29-43-62 34-48-68 40-52-73 45-55-78 50-62-87 55-68-96 60-73-103 24x24 45° 9-15-28 13-20-32 17-25-36 20-28-39 23-30-42 26-32-45 29-36-51 32-39-55 35-42-60 NC - 16 22 28 33 37 43 49 53 Airflow(CFM) 1266 1688 2110 2532 2954 3376 4220 5064 5908 0° 22-35-65 31-47-76 39-59-84 47-65-93 55-71-100 62-76-107 69-84-119 76-93-131 82-100-141 36x18 Throw(ft.) 22.5° 17-27-51 24-36-59 30-45-65 36-51-72 42-55-77 48-59-83 53-65-93 59-72-101 63-77-110 45° 10-16-29 14-21-34 18-26-38 21-29-42 25-32-45 28-34-48 31-38-54 34-42-59 37-45-64 NC - 16 23 28 33 37 44 49 54 045 Airflow(CFM) 1413 1884 2355 2826 3297 3768 4710 5652 6594 0° 23-37-69 33-49-80 41-62-89 49-69-98 58-75-106 65-80-113 73-89-126 80-98-138 86-106-149 N 36x20 31x24 Throw(ft.) 22.5° 18-29-54 26-38-62 32-48-69 38-54-76 45-58-82 50-62-87 56-69-98 67-76-107 67-82-116 - • - ir 45° 10-17-31 15-22-36 19-28-40 22-31-44 26-34-48 29-36-51 33-40-57 36-44-62 39-48-67 •- NC - 17 23 29 33 37 44 50 54 (.9 ,d Airflow(CFM) 1482 1976 2470 2964 3458 3952 4940 5928 6916 0° 24-38-71 34-51-82 42-63-91 51-71-100 59-76-108 67-82-116 75-91-129 82-100-142 88-108-153 42x18 Throw(ft.) 22.5° 18-29-55 26-39-63 33-49-71 39-55-71 46-59-84 52-63-90 58-71-100 63-78-110 68-84-118 45° 11-17-32 15-23-37 19-28-41 19-28-41 27-34-49 30-37-52 34-41-58 37-45-64 40-49-69 NC - 17 24 24 34 38 44 50 54 Notes: 1. Tests conducted in accordance with ANSI/ASHRAE 70-1991 at isothermal conditions. 2. Tests conducted with a straight rigid inlet condition. Other inlet conditions may alter performance. 3. Performance data includes damper in the full open position. 4. 0°,22.5°and 45°represent blade deflection angles. 5. Units:Face Velocity=fpm;Total Pressure=in.we 6. Throw based on terminal velocities of 150 fpm,100 fpm and 50 fpm. 7. NC is based upon 10dB room absorption(Re:10-12 watts)evaluated at 125 through 4000 Hz octave bands. 8. Dash"-"indicates NC value less than 10. www.tuttleandbailey.com 7/14 GR21 • T6-B ENGINEERING DATA T50, T60, T52, T62, T54, T64 Core Vel.(fpm) 300 400 500 600 700 800 1000 1200 1400 d Vel.Pressure 0.006 0.010 0.016 0.022 0.031 0.040 0.062 0.090 0.122 ri Nom Duct 0° 0.016 0.029 0.046 0.066 0.090 0.117 0.183 0.263 0.358 Size Total Pressure 22.5° 0.018 0.033 0.051 0.074 0.100 0.131 0.204 0.294 0.401 45° 0.028 0.049 0.077 0.111 0.152 0.198 0.309 0.445 0.606 Airflow(CFM) 1548 2064 2580 3096 3612 4128 5160 6192 7224 0° 24-39-72 35-52-84 43-65-93 52-72-102 60-78-110 68-84-118 76-93-132 84-102-145 90-110-156 28x28 Throw(ft.) 22.5° 19-30-56 27-40-65 33-50-72 40-56-79 47-61-86 53-65-92 59-72-102 65-79-112 70-86-121 45° 11-17-33 16-23-38 19-29-42 23-33-46 27-35-50 31-38-53 _ 34-42-59 38-46-65 41-50-70 NC - 17 24 29 34 38 45 50 55 Airflow(CFM) 1653 2204 2755 3306 3857 4408 5510 6612 7714 0° 25-40-75 36-54-86 45-67-96 54-75-106 62-81-114 70-86-122 79-96-136 86-106-149 93-114-161 42x20 Throw(ft.) 22.5° 19-31-58 28-41-67 35-52-75 41-58-82 48-63-88 55-67-95 61-75-106 67-82-116 72-88-125 j 30x28 1 45° 11-18-34 16-24-39 20-30-43 24-34-48 28-36-51 32-39-55 35-43-61 39-48-67 42-51-73 NC - 17 24 30 34 38 45 50 55 Airflow(CFM) 1698 2264 2830 3396 3962 1 4528 5660 6792 7924 0° 25-41-76 36-54-87 45-68-98 54-76-107 63-82-116 71-87-124 80-98-138 87-107-152 94-116-164 48x18'' 36x24 Throw(ft.) 22.5° 20-32-59 28-42-68 35-53-76 42-59-83 49-63-90 55-68-96 62-76-107 68-83-117 73-90-127 45° 11-18-34 16-24-39 20-31-44 24-34-48 28-37-52 32-39-56 36-44-62 39-48-68 43-52-74 NC - 18 24 30 34 38 45 50 55 1 Airflow(CFM) 1782 2376 2970 3564 4158 4752 5940 7128 8316 ji 0° 26-42-78 37-56-90 46-69-100 56-78-110 65-84-119 73-90-127 82-100-142 90-110-155 97-119-168 30x30 Throw(ft.) 22.5° 20-32-60 29-43-69 36-54-78 43-60-85 50-65-92 57-69-98 63-78-110 69-85-120 75-92-130 45° 12-19-35 17-25-40 21-31-45 25-35-49 29-38-53 33-40-57 37-45-64 40-49-70 44-53-75 ii NC - 18 24 30 34 38 45 51 55 I s Airflow(CFM) 1998 2664 3330 3996 4662 5328 6660 7992 9324 0° 28-44-82 39-59-95 49-74-106 59-82-116 69-89-126 77-95-134 87-106-150 95-116-164 102-126-178 42x24 Throw(ft.) 22.5° 21-34-64 30-46-74 38-57-82 46-64-90 53-69-97 60-74-104 67-82-116 74-90-127 79-97-138 36x28 45° 12-20-37 18-26-43 22-33-48 26-37-52 31-40-56 35-43-60 39-48-68 43-52-74 46-56-80 NC - 18 25 30 35 39 46 51 56 Ax ( W Airflow(CFM) 2004 2672 3340 4008 4676 5344 6680 8016 9352 0° 28-44-82 39-59-95 49-74-106 59-82-116 69-89-126 78-95-134 87-106-150 95-116-165 103-126-178 '- 46x22 Throw(ft.) 22.5° 21-34-64 30-46-74 38-57-82 46-64-90 53-69-97 60-74-104 67-82-116 74-90-128 80-97-138 -L Q) 45° 12-20-37 18-27-43 22-33-48 27-37-52 31-40-57 35-43-60 39-48-68 43-52-74 46-57-80 n N NC - 18 25 30 35 36 46 51 56 LL Airflow(CFM) 2034 2712 3390 4068 4746 5424 6780 8136 9492 I 0° 28-45-83 40-59-96 49-74-107 59-83-117 69-90-127 78-96-135 87-107-151 96-117-166 103-127-179 ?I 32x32 Throw(ft.) 22.5° 22-34-64 31-46-74 38-57-83 46-64-91 54-69-98 61-74-105 68-83-117 74-91-129 80-98-139 45° 12-20-37 18-27-43 22-33-48 27-37-53 31-40-57 35-43-61 39-48-68 43-53-75 47-57-81 NC - 18 25 30 35 39 46 51 56 Notes: 1. Tests conducted in accordance with ANSI/ASHRAE 70-1991 at isothermal conditions. 2. Tests conducted with a straight rigid inlet condition. Other inlet conditions may alter performance. 3. Performance data includes damper in the full open position. 4. 0°,22.5°and 45°represent blade deflection angles. 5. Units:Face Velocity=fpm;Total Pressure=in.we 6. Throw based on terminal velocities of 150 fpm,100 fpm and 50 fpm. 7. NC is based upon 10dB room absorption(Re:1012 watts)evaluated at 125 through 4000 Hz octave bands. 8. Dash"-"indicates NC value less than 10. GR22 7/14 www.tuttleandbailey.com ENGINEERING DATA T50, T60, T52, T62, T54, T64 . Core Vel.(fpm) 300 400 500 600 700 800 1000 1200 1400 -`- Vel.Pressure 0.006 0.010 0.016 0.022 0.031 0.040 0.062 0.090 0.122 Nom Duct Size 0° 0.016 0.029 0.046 0.066 0.090 0.117 0.183 0.263 0.358 Total Pressure 22.5° 0.018 0.033 0.051 0.074 0.100 0.131 0.204 0.294 0.401 45° 0.028 0.049 0.077 0.111 0.152 0.198 0.309 0.445 0.606 Airflow(CFM) 2148 2864 3580 4296 5012 5728 7160 8592 10024 0° 29-46-85 41-61-98 51-76-110 61-85-121 71-92-130 80-98-139 90-110-156 98-121-170 106-130-184 36x30 Throw(ft.) 22.5° 22-35-66 32-47-76 39-59-85 47-66-93 55-71-101 62-76-108 70-85-121 76-93-132 _ 82-101-143 45° 13-21-38 18-27-44 23-34-50 27-38-54 32-41-59 36-44-63 40-50-70 44-54-77 48-59-83 NC - 19 25 31 35 39 46 51 56 Airflow(CFM) 2289 3052 3815 4578 5341 6104 7630 9156 10682 0° 29-47-88 42-63-102 52-79-114 63-88-124 73-95-134 83-102-144 93-114-161 102-124-176 110-134-147 48x24 Throw(ft.) 22.5° 23-37-68 33-49-79 41-61-88 49-68-96 57-74-104 64-79-111 72-88-124 79-96-136 85-104-147 36x32 45° 13-21-40 19-28-46 24-35-51 28-40-56 33-43-60 37-46-65 42-51-72 46-56-79 49-60-86 NC - 19 25 31 35 39 46 52 56 Airflow(CFM) 2304 3072 3840 4608 5376 6144 7680 9216 10752 0° 30-47-88 42-63-102 53-79-114 63-88-125 74-95-135 83-102-144 93-114-161 102-125-176 110-135-191 34x34 Throw(ft.) 22.5° 23-37-68 33-49-79 41-61-88 49-68-97 57-74-104 64-79-112 72-88-125 79-97-137 85-104-148 45° 13-21-40 19-28-46 24-36-51 28-40-56 33-43-61 37-46-65 42-51-73 46-56-79 50-61-86 _._ t i NC - 19 25 31 36 40 46 52 56 - Airflow(CFM) 2442 3256 4070 4884 5698 6512 8140 9768 11396 0° 30-49-91 43-65-105 54-81-117 65-91-128 76-98-139 86-105-148 96-117-166 105-128-182 113-139-196 36x34 Throw(ft.) 22.5° 24-38-70 34-50-81 42-63-91 50-70-100 59-76-108 66-81-115 74-91-129 81-100-141 88-108-152 ' 45° 14-22-41 20-29-47 24-37-53 29-41-58 34-44-62 39-47-67 43-53-75 47-58-82 51-62-88 NC - 19 26 31 36 40 46 52 56 Airflow(CFM) 2514 3352 4190 5028 5866 6704 8380 10056 11732 0° 31-49-92 44-66-106 55-82-119 66-92-130 77-100-141 87-106-151 97-119-168 106-130-184 115-141-199 42x30 Throw(ft.) 22.5° 24-38-71 34-51-82 43-64-92 51-71-101 60-77-109 67-82-117 75-92-130 82-101-143 89-109-154 45° 14-22-41 20-30-48 25-37-54 30-41-59 35-45-63 39-48-68 44-54-76 48-59-83 52-63-90 NC 11 19 26 31 36 40 47 52 57 Airflow(CFM) 2589 3452 4315 5178 6041 6904 8630 10356 12082 Qi II 0° 31-50-94 45-67-108 56-84-121 67-94-132 78-101-143 88-108-153 99-121-171 108-132-187 117-143-202 fn 36x36 Throw(ft.) 22.5° 24-39-72 35-52-84 43-65-94 52-72-103 61-78-111 68-84-118 76-94-132 84-103-145 90-111-157 j • 45° 14-23-42 20-30-49 25-38-54 30-42-60 35-45-64 40-49-69 44-54-77 49-60-84 53-64-91 = 411' NC 11 19 26 31 36 40 47 52 57 .S.-. CD id Airflow(CFM) 2880 3840 4800 5760 6720 7680 9600 11520 13440 0° 33-53-99 47-71-114 59-88-127 71-99-140 82-107-151 93-114-161 104-127-180 114-140-197 123-151-213 42x34 Throw(ft.) 22.5° 26-41-76 36-55-88 46-68-99 55-76-108 64-83-117 72-88-125 81-99-140 88-108-153 95-117-165 48x30 45° 15-24-44 21-32-51 26-40-57 32-44-63 37-48-68 42-51-73 47-57-81 51-63-89 55-68-96 NC 11 20 26 32 36 40 47 53 57 Notes: 1. Tests conducted in accordance with ANSI/ASHRAE 70-1991 at isothermal conditions. 2. Tests conducted with a straight rigid inlet condition. Other inlet conditions may alter performance. 3. Performance data includes damper in the full open position. 4. 0°,22.5°and 45°represent blade deflection angles. 5. Units:Face Velocity=fpm;Total Pressure=in.we 6. Throw based on terminal velocities of 150 fpm,100 fpm and 50 fpm. 7. NC is based upon 10dB room absorption(Re:10-'2 watts)evaluated at 125 through 4000 Hz octave bands. 8. Dash"-"indicates NC value less than 10. www.tuttleandbailey.com 7/14 GR23 T�� ... ENGINEERING DATA T50, T60, T52, T62, T54, T64 } Core Vel.(fpm) 300 400 500 600 700 800 1000 1200 1400 Vel.Pressure 0.006 0.010 0.016 0.022 0.031 0.040 0.062 0.090 0.122 Nom Duct Size 0° 0.016 0.029 0.046 0.066 0.090 0.117 0.183 0.263 0.358 Total Pressure 22.5° 0.018 0.033 0.051 0.074 0.100 0.131 0.204 0.294 0.401 45° 0.028 0.049 0.077 0.111 0.152 0.198 0.309 0.445 0.606 j{ Airflow(CFM) 2892 3856 4820 5784 6748 7712 9640 11568 13496 0° 33-53-99 47-71-114 59-88-128 71-99-140 83-107-151 93-114-161 104-128-181114-140-198123-151-214 38x38 Throw(ft.) 22.5° 26-41-77 37-55-88 46-69-99 55-77-108 64-83-117 72-88-125 81-99-140 88-108-153 96-117-166 45° 15-24-44 21-32-51 27-40-57 32-44-63 37-48-68 42-51-73 47-57-81 51-63-89 55-68-96 NC 11 20 26 32 36 40 47 53 57 Airflow(CFM) 3030 4040 5050 6060 7070 8080 10100 12120 14140 0° 34-54-101 48-72-117 60-91-131 72-101-143 85-109-155 95-117-165 107-131-185117-143-202126-155-219 42x36 Throw(ft.) 22.5° 26-42-78 37-56-91 47-70-101 56-78-111 65-85-120 74-91-128 83-101-143 91-111-157 98-120-169 45° 15-24-46 22-33-53 27-41-59 33-46-64 38-49-70 43-53-74 48-59-83 53-64-91 57-70-98 NC 11 20 27 32 37 41 47 53 57 Airflow(CFM) 3135 4180 5225 6270 7315 8360 10450 12540 14630 0° 34-55-103 49-74-119 61-92-133 74-103-146 86-111-157 97-119-168 109-133-188119-146-206128-157-222 46x34 Throw(ft.) 22.5° 27-43-80 38-57-92 48-71-103 57-80-113 67-86-122 75-92-130 84-103-146 92-113-160 99-122-172 45° 16-25-46 22-33-53 28-41-60 33-46-66 39-50-71 44-53-76 49-60-85 53-66-93 58-71-100 NC 11 20 27 32 37 41 47 53 58 • Airflow(CFM) 3201 4268 5335 6402 7469 8536 10670 12804 14938 0° 35-56-104 50-74-120 62-93-134 74-104-147 84-112-159 98-120-170 110-134-190120-147-208130-159-225 42x38 Throw(ft.) 22.5° 27-43-81 38-58-93 48-72-104 58-81-114 67-87-123 76-93-132 85-104-147 93-114-161 101-123-174 45° 16-25-47 22-34-54 28-42-60 34-47-66 39-51-71 44-54-76 49-60-85 54-66-94 58-71-101 NC 12 20 27 32 37 41 48 53 58 Airflow(CFM) 3210 4280 5350 6420 7490 8560 10700 12840 14980 0° 35-56-104 50-75-120 62-93-134 75-104-147 87-113-159 98-120-170 110-134-190120-147-208130-159-225 40x40 Throw(ft.) 22.5° 27-43-81 39-58-93 48-72-104 58-81-114 67-87-123 76-93-132 85-104-147 93-114-161 101-123-174 45° 16-25-47 22-34-54 28-42-61 34-47-66 39-51-72 44-54-77 49-61-86 54-66-94 58-72-101 ^X (n NC 12 20 27 32 37 44 48 53 58 �J( L- U) Airflow(CFM) 3471 4628 5785 6942 8099 9256 11570 13884 16198 Q) 0° 36-58-108 52-78-125 65-97-140 78-108-153 90-117-165 102-125-177114-140-198125-153-217135-165-234 - CD 48x36 Throw(ft.) 22.5° 28-45-84 40-60-97 50-75-108 60-84-119 70-91-128 79-97-137 88-108-153 97-119-168 105-128-181 L' 45° 16-26-49 23-35-56 29-44-63 35.49-69 41-53-74 46-56-80 51-63-89 56-69-97 61-74-105 I' 0 CC. NC 12 21 27 33 37 41 48 53 58 Airflow(CFM) 3546 4728 5910 7092 8274 9456 11820 14184 16548 0° 37-59-109 52-78-126 65-98-141 78-109-155 91-118-167 103-126-179115-141-200126-155-219137-167-236 42x42 Throw(ft.) 22.5° 24-46-85 40-61-126 51-76-110 61-85-120 71-92-130 80-98-139 89-110-155 98-120-170 106-130-183 45° 16-26-49 24-35-57 29-44-64 35-49-70 41-53-75 46-57-80 52-64-90 57-70-99 61-75-106 NC 12 27 27 33 37 41 48 53 58 Notes: 1. Tests conducted in accordance with ANSI/ASHRAE 70-1991 at isothermal conditions. 2. Tests conducted with a straight rigid inlet condition. Other inlet conditions may alter performance. 3. Performance data includes damper in the full open position. 4 0°,22.5°and 45°represent blade deflection angles. 5. Units:Face Velocity=fpm;Total Pressure=in.we 6. Throw based on terminal velocities of 150 fpm,100 fpm and 50 fpm. 7. NC is based upon 10dB room absorption(Re:1012 watts)evaluated at 125 through 4000 Hz octave bands. 8. Dash"-"indicates NC value less than 10. GR24 7/14 www.tuttleandbailey.com Ty, ENGINEERING DATA T50, T60, T52, T62, T54, T64 Core Vel.(fpm) 300 400 500 600 700 800 1000 1200 1400 Vel.Pressure 0.006 0.010 0.016 0.022 0.031 0.040 0.062 0.090 0.122 Nom Duct Size 0° 0.016 0.029 0.046 0.066 0.090 0.117 0.183 0.263 0.358 Total Pressure 22.5° 0.018 0.033 0.051 0.074 0.100 0.131 0.204 0.294 0.401 45° 0.028 0.049 0.077 0.111 0.152 0.198 0.309 0.445 0.606 Airflow(CFM) 3897 5196 6495 7794 9093 10392 12990 15588 18186 0° 38-62-115 55-82-133 68-103-148 82-115-162 96-124-175 108-133-187121-148-210133-162-230143-175-248 44x44 Throw(ft.) 22.5° 30-48-89 42-64-103 53-80-115 64-89-126 74-96-136 84-103-145 94-115-162 103-126-178 111-136-192 45° 17-28-52 25-37-60 31-46-67 37-52-73 43-55-79 49-60-84 54-67-94 60-73-103 64-79-112 NC 12 21 28 33 38 42 48 54 58 Airflow(CFM) 4062 5416 6770 8124 9478 10832 13540 16248 18956 0° 36-63-117 58-84-135 70-105-151 84-117-166 98-127-179 110-135-191 124-151-214135-166-234146-179-253 48x42 Throw(ft.) 22.5° 30-49-91 43-65-105 54-81-117 65-91-128 76-98-139 86-105-148 96-117-166 105-128-182,113-139-196 45° 18-28-53 25-38-61 31-47-68 38-53-75 44-57-81 50-61-86 56-68-96 61-75-105 68-81-114 NC 13 21 28 33 38 42 49 54 59 Airflow(CFM) 4266 5699 7110 8532 9954 11376 14220 17064 19908 0° 40-64-120 57-86-139 72-107-155 86-120-170 100-130-183 113-139-196 127-155-219 139-170-240 150-183-259 46x46 Throw(ft.) 22.5° 31-50-93 44-67-107 56-83-120 67-93-132 78-101-142 88-107-152 98-120-170 107-132-186 116-142-201 45° 18-29-54 26-39-62 32-48-70 39-54-76 45-58-83 51-62-88 57-70-99 62-76-108 67-83-117 NC 13 21 28 33 38 42 49 54 59 Airflow(CFM) 4455 5940 7425 8910 10395 11880 14850 17820 20790 0° 41-66-123 59-88-142 73-110-158 88-123-174 102-133-187 116-142-200 129-158-224 142-174-245 153-187-265 48x46 Throw(ft.) Y2.5° 32-51-95 45-68-110 57-85-123 68-95-134 79-103-145 90-110-155 100-123-174 110-134-190 119-145-205 45° 18-30-55 26-40-64 33-49-71 40-55-78 46-60-84 52-64-90 58-71-101 64-78-110 69-84-119 NC 13 22 28 34 38 42 49 54 59 Airflow(CFM) 4650 6200 7750 9300 10850 12400 15500 18600 21700 0° 42-67-125 60-90-145 75-112-162 90-125-177 105-135-192 118-145-202 132-162-229 145-177-251 156-192-271 48x48 Throw(ft.) 22.5° 33-52-97 46-70-112 58-87-125 70-97-137 81-105-148 92-112-159 102-125-177 112-137-194 121-148-210 45° 19-30-56 27-40-65 34-50-73 40-56-80 47-61-86 53-65-92 59-73-103 65-80-113 70-86-122 NC 13 22 28 34 38 42 49 55 59 CD Notes: Q) • 1. Tests conducted in accordance with ANSI/ASHRAE 70-1991 at isothermal conditions. - �. 2. Tests conducted with a straight rigid inlet condition. Other inlet conditions may alter performance. 3. Performance data includes damper in the full open position. ,^ 4. 0°,22.5°and 45°represent blade deflection angles. v Id 5. Units:Face Velocity=fpm;Total Pressure=in.we 6. Throw based on terminal velocities of 150 fpm,100 fpm and 50 fpm. 7. NC is based upon 10dB room absorption(Re:10-12 watts)evaluated at 125 through 4000 Hz octave bands. 8. Dash"-"indicates NC value less than 10. www.tuttleandbailey.com 7/14 GR25 L Submittal .. . TuttleBailey® - Drawing • Double deflection with individually adjustable blades on 3/4" centers • Model T54 has horizontal front blades / Model T64 has vertical front blades • Steel construction • Standard grille finish is white (WH) • Damper option is mill finish only • Available sizes are 6x4 to 48x48 in 1" increments (larger sizes in sections) i___ Listed - 1/4 Listed - 1/4 --owl T54 2 1/16 ,I.�-1 ; 1i_1 L1i_1 L1J_ - 2 1/16 T64 HiLi- l_11f�i11f '--f--- , 9/16 9/16 ljit I ■■■■■■■■■■■■■■■ r ■■■■■■■■■■■■■■■ ■■■■■■■■■■■■■■■ ■■■■■■■■■■■■■■■ ■.■■■■■■■■■■■.■ •■■■■■■■■■■■■■■■ Listed - 1/4 ■■■■•■■■■■■■■■■ ••••••••••••••• Listed - 1/4 i ■■■■■■■■■■■■■■■ ■■■■■■■■■■■■■■■ ............... ■■■■■■■■■■■■■■. 1 1/41 1/4 Duct + 1 3/4 Duct+ 1 3/4 ■-rulli T54 w/ SOBDL- ' T64 w/ SOBD Duct- 1/4 --► 1-01-- Duct- 1/4--No--1 Concealed Mountin 3 5/16 for damper full closed g 3 11/16 for damper full open Ductwork Field supplied#8 screw Available Fastening Methods 11 Field supplied 0 01 - Screw Holes 3/4 x 1 1/4 angle 0 02 - No Screw Holes Factory welded 0 03 - Concealed 3/4 x 1 1/4 angle elm INIIIMEM Available Colors LT Frame Style 0 WH (White) ❑ML (Mill) OAP (Aluminum Paint) Module 1/4 El OW (Off-White) ❑FB (Flat Black) mu J. 1 1.1Li_f1J 1 L1.J4 0 MP (Match Paint) Moule * Max Neck Accessories 12x12 9x9 0 SOBD (Steel opposed blade damper) 24x12 21x9 0 45 (Steel mounting frame) 24x24 21x21 * - When using a module for Lay-In T-Bar ceiling, 48x24 45x21 this is the maximum neck size for specified Dimensions in inches module III Job: Tag: Location: T54 & T64 Architect: Submitted By: Supply Grille Steel Engineer: Double Deflection Contractor: SD-1761 Rev: C (08/17) These drawings do not detail every aspect of the product.This submittal demonstrates general product dimensions;drawings are not to scale. Tuttle&Bailey reserves the right to make changes without notice. Copyright©2017 Tuttle&Bailey www.tuttleandbailey.com T B ENGINEERING DATA S1200, A1200 Fixed Pattern - Horizontal Throw 12x12 Neck Neck Velocity 200 300 500 600 700 800 900 1000 1100 Size(in.)Airflow Rate (CFM) 39 59 98 118 137 157 177 196 216 Static Pressure 0.006 0.015 0.040 0.058 0.079 0.103 0.131 0.161 0.195 Total Pressure 0.009 0.020 0.056 0.081 0.110 0.143 0.181 0.224 0.271 6 Horizontal Throw 1-2-4 2-3-7 4-6-9 4-7-10 5-8-11 6-8-12 7-9-13 7-9-13 8-10-14 NC - - - - 15 20 25 30 34 Neck Neck Velocity 200 300 400 500 600 700 800 900 1000 Size(in.)Airflow Rate (CFM) 70 105 140 175 209 244 279 314 349 Static Pressure 0.018 0.040 0.071 0.111 0.160 0.218 0.285 0.361 0.446 Total Pressure 0.020 0.046 0.081 0.127 0.183 0.249 0.325 0.411 0.508 8 Horizontal Throw 2-3-6 3-4-9 4-6-11 5-7-13 6-9-14 7-10-15 8-11-16 9-12-17 10-13-18 NC - - - 16 23 30 35 40 45 Notes: 1. Tests conducted in accordance with ANSI/ASHRAE 70-1991 at isothermal conditions. 2. Throw values are given for isothermal conditions. 3. Units: Neck Velocity=fpm; Static Pressure=in.wc;Total Pressure= in.wc. 4. Throw=feet. at 150 fpm, 100 fpm and 50 fpm terminal velocity. 5. NC is based on octave bands 2-7 sound power levels with a room abosorption of 10dB (Re: 10-12 watts). j 6. Dash (-) in space denotes an NC value of less than 10. - a.�e t. 0) 1 C 0 s www.tuttleandbailey.com 7/14 CD83 T B ENGINEERING DATA S1200, A1200 Fixed Pattern - Horizontal Throw 24x24 Neck Neck Velocity 200 300 500 600 700 800 900 1000 1100 Size (in.)Airflow Rate (CFM) 39 59 98 118 137 157 177 196 216 Static Pressure 0.003 0.006 0.016 0.023 0.032 0.042 0.053 0.065 0.079 Total Pressure 0.005 0.011 0.032 0.046 0.062 0.081 0.103 0.127 0.154 6 Horizontal Throw 0-1-3 1-2-4 2-4-7 3-4-8 3-5-8 4-6-9 4-6-9 5-7-10 5-7-10 NC - - - - 15 19 23 26 29 Neck Neck Velocity 200 300 500 600 700 800 900 1000 1100 Size (in.)Airflow Rate (CFM) 70 105 175 209 244 279 314 349 384 Static Pressure 0.003 0.008 0.022 0.031 0.042 0.055 0.070 0.086 0.105 Total Pressure 0.006 0.013 0.037 0.054 0.073 0.095 0.121 0.149 0.180 8 Horizontal Throw 1-1-4 1-3-6 3-5-9 4-6-10 4-7-11 5-7-12 6-8-13 6-9-13 7-10-14 NC - - - 14 19 23 27 30 33 Neck Neck Velocity 200 300 500 600 700 800 900 1000 1100 Size(in.)Airflow Rate (CFM) 109 164 273 327 382 436 491 545 600 Static Pressure 0.005 0.010 0.029 0.041 0.056 0.073 0.093 0.114 0.138 Total Pressure 0.007 0.016 0.044 0.064 0.087 0.113 0.143 0.177 0.214 10 Horizontal Throw 1-1-5 1-3-7 4-6-12 5-7-13 5-8-14 6-9-15 7-11-16 8-12-17 9-12-17 NC - - 11 17 22 26 30 33 36 Neck Neck Velocity 200 300 500 600 700 800 900 1000 1100 - Size (in.)Airflow Rate (CFM) 157 236 393 471 550 628 707 785 864 Static Pressure 0.006 0.013 0.037 0.053 0.073 0.095 0.120 0.148 0.179 Total Pressure 0.008 0.019 0.053 0.076 0.103 0.135 0.170 0.210 0.255 12 Horizontal Throw 1-2-6 2-4-8 5-7-14 6-8-15 7-10-17 7-11-18 8-13-19 9-14-20 10-15-21 NC - - 14 19 24 28 32 36 39 Neck Neck Velocity 200 300 400 500 600 700 800 900 1000 i Size (in.)Airflow Rate (CFM) 214 321 428 535 641 748 855 962 1069 0) d) Static Pressure 0.008 0.017 0.030 0.047 0.068 0.092 0.120 0.152 0.188 CO Total Pressure 0.010 0.023 0.040 0.063 0.090 0.123 0.160 0.203 0.251 -0 14 Horizontal Throw 1-2-7 2-4-10 4-7-13 5-8-16 7-10-18 8-11-19 9-13-21 10-15-2211-16-23 O 0 NC - - - 16 21 26 31 34 38 Neck Neck Velocity 200 300 400 500 600 700 800 900 1000 Size (in.)Airflow Rate (CFM) 245 368 491 614 736 859 982 1104 1227 Static Pressure 0.008 0.019 0.034 0.053 0.076 0.103 0.135 0.171 0.211 Total Pressure 0.011 0.025 0.044 0.068 0.098 0.134 0.175 0.221 0.273 15 Horizontal Throw 1-2-7 2-5-11 4-7-14 6-9-18 7-11-19 8-12-21 9-14-22 11-16-2412-18-25 NC - - - 16 22 27 31 35 39 Notes: 1. Tests conducted in accordance with ANSI/ASHRAE 70-1991 at isothermal conditions. 2. Throw values are given for isothermal conditions. 3. Units: Neck Velocity=fpm; Static Pressure= in.wc;Total Pressure= in.wc. 4. Throw=feet. at 150 fpm, 100 fpm and 50 fpm terminal velocity. 5. NC is based on octave bands 2-7 sound power levels with a room abosorption of 10dB (Re: 10-12 watts). 6. Dash (-) in space denotes an NC value of less than 10. CD84 7/14 www.tuttleandbailey.com 4jk Tuttle & Bailey. SUBMITTAL DRAWING • Steel (S1200) or Aluminum (A1200) construction • Core is non-removable • 2-cone stepdown diffuser • Optional round damper to be ordered separately • Frame SF (surface mount) includes an aluminum and field mounted mounting frame • Damper is adjustable through hole in • Standard finish is white center cone • Two earthquake tabs are standard on all frame styles Face View CEILING OPENING n FRAME SF 24-1/2" �r See specific frame details for dimensions EARTHQUAKE TAB (SEE NOTES) A B 2-7/16" { 1 \ / 25-1/4" i r ,1 U FRAME LT A---%r i i B ... I } 2-3/8" O L23-3/4" r Y \ K./.. n FRAME PL A—+ 1 B 2-7/16" + 23-31/32" 3/8" NOMINAL SERIES 1200 SERIES S1200 SERIES A1200 DROP - 7/16" NECK STEEL& STEEL ALUMINUM SIZE ALUMINUM A B B n FRAME NR I A----ir- 6 5 7/8" 1" 1 1/2" I B — I 8 7 7/8" 1" 1 1/2" 2-7/16" } A 10 9 7/8" 1 1/2" 1 1/2" 12 11 7/8" 1 1/2" 1 1/2" 5/16" - 23-13/32" 14 13 7/8" 1 1/2" 1 1/2" DROP -3/16" r 15 14 7/8" 1 1/2" 1 1/2" Dimensions are in inches, Product information subject to change without notice PROJECT: SUBMITTED BY: DATE: 9-1-00 SD-1763 ARCHITECT: S1200 & A1200 Series ENGINEER: Fixed Pattern Diffuser - CONTRACTOR: 2-Cone w/Round Neck LOCATION: 24 x 24 module