ULA Supply air Tuloilma Soufflage Zuluft Tilluft Приток 20/CG/1500/0611 ø 125 360° ø 125 180° A k A k 3 1,61 6 3,52 9 5,39 12 8,25 ø 125 360° 3 1,04 6 1,98 9 2,82 12 4,45 ø 125 180° A k A k 3 1,60 6 3,51 9 5,33 12 8,07 ø 125 360° 3 1,03 6 1,95 9 2,84 12 4,46 ø 125 180° A k A k 3 1,60 6 3,51 9 5,33 12 8,07 3 1,03 6 1,95 9 2,84 12 4,46 q v = k x p m 18
ULA Supply air Tuloilma Soufflage Zuluft Tilluft Приток 20/CG/1500/0611 ø 160 360° ø 160 180° A k A k 3 2,00 6 4,11 9 6,61 12 8,78 18 12,92 ø 160 360° A k 3 2,01 6 4,13 9 6,78 12 8,86 18 12,85 ø 160 360° 3 1,18 6 2,41 9 3,47 12 4,55 18 6,65 ø 160 180° A k 3 1,23 6 2,42 9 3,41 12 4,39 18 6,68 ø 160 180° A k A k 3 2,01 6 4,13 9 6,78 12 8,86 18 12,85 3 1,23 6 2,42 9 3,41 12 4,39 18 6,68 q v = k x p m 19
- Page 1 and 2: Testing and Balancing Guide 2011 Ha
- Page 3 and 4: SLL+PLL SLL+ PLD SLN+PLL SLN+PLD Su
- Page 5 and 6: VHB / VHD VHB/VHD ø D k 160 15,9 2
- Page 7 and 8: TCV, DRV ∆p m (Pa) TCV DRV ø D k
- Page 9 and 10: N (N = Nozzle, N = Suutin, N = Buse
- Page 11 and 12: DSS C (C = Conical, C = Kartio, C =
- Page 13 and 14: TRI / S TRI ø D k 100 6,0 7,5 125
- Page 15 and 16: PRI / E Exhaust air Poistoilma Extr
- Page 17: ULA Supply air Tuloilma Soufflage Z
- Page 21 and 22: ULA Exhaust air Poistoilma Extracti
- Page 23 and 24: URH, FRH Exhaust air Poistoilma Ext
- Page 25 and 26: URH, FRH Exhaust air Poistoilma Ext
- Page 27 and 28: CBD CBD k / m CBD/A 0,71 CBD/B 0,99
- Page 29 and 30: CCC dp m HAQ & CCC q v1 = k x l eff
- Page 31 and 32: PRA 20/CG/1500/0611 ø 100 ø 125 A
- Page 33 and 34: PRA 20/CG/1500/0611 ø 500 ø 630 A
- Page 35 and 36: HFR, HFD 20/CG/1500/0611 HFR/HFD k
- Page 37 and 38: HFL 20/CG/1500/0611 Unit size Posit
- Page 39 and 40: UVF (Canopies) H = 555 mm ∆PTAB
- Page 41 and 42: ∆PTAB ∆PTAB KVF / UVF (Canopies
- Page 43 and 44: UVI (Canopies) H = 555 mm ∆PTAB
- Page 45 and 46: KVL Capture Jets Sieppausilma Jets
- Page 47 and 48: ∆PTAB KCF ∆PTAB ∆PTAB Exhaust
- Page 49 and 50: KCE ∆PTAB ∆PTAB ∆PTAB Exhaust
- Page 51 and 52: KVV / KVD H = 555 mm ∆PTAB ∆PTA
- Page 53 and 54: Notes
- Page 55 and 56: Notes