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时间:2011-02-24 09:22来源:蓝天飞行翻译 作者:admin
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 1. All cases are nominal values.
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (1) Total Fresh Air Quantities (Table 1)
 ----------------------------------------------------------------------------
| f * Qvs * Pc | |
 | - Q = ----------------| |
 | 2.87 * Tc | |
 | | |
 | - Q = mass flow | kg/s |
 | - f = selected flow factor | (0.8/1.0/1.2) |
 | - Pc = cabin pressure | mbar |
 | - Tc = cabin temperature | 297 K |
 | - Qvs = normal volumetric flow at sea level | 0.928 cbm/s |
 | - 2.87 = constant factor | |
 ----------------------------------------------------------------------------The nominal values from the use of the above formula:
 ----------------------------------------------------------------------------
| ground kg/s cruise kg/s |
 |----------------------------------------------------------------------------|
 | normal flow (100%) | 1.102 | 0.817 |
 | minimum flow | 80 % of norm. | 80 % of norm. |
 | maximum flow | 120 % of norm. | 120 % of norm. |
 | one pack off | 60 % of norm. | 60 % of norm. |
 ----------------------------------------------------------------------------These nominal flows can vary by plus 5 % or minus 2 %.
 ----------------------------------------------------------------------------
| Total fresh air required from the APU: |
 |----------------------------------------------------------------------------|
 | hot day | +38 DEG.C (100.4 DEG.F) | 1.00 kg/s |
 | cold day | -23 DEG.C (-9.4 DEG.F) | 1.28 kg/s |
 | normal day | - 5 DEG.C (+23 DEG.F) to +30 DEG.C (86 DEG.F) | 0.82 kg/s |
 ---------------------------------------------------------------------------- **ON A/C 301-399,


 (1) Total Fresh Air Quantities:
 ----------------------------------------------------------------------------
| f * Qvs * Pc | |
 | - Q = ----------------| |
 | 2.87 * Tc | |
 | | |
 | - Q = mass flow | kg/s |
 | - f = selected flow factor | (0.8/1.0) |
 | - Pc = cabin pressure | mbar |
 | - Tc = cabin temperature | 297 K |
 | - Qvs = normal volumetric flow at sea level | 1.088 cbm/s |
 | - 2.87 = constant factor | |
 ----------------------------------------------------------------------------The nominal values from the use of the above formula:
 ----------------------------------------------------------------------------
| ground kg/s cruise kg/s |
 |----------------------------------------------------------------------------|
 | normal flow (100%) | 1.293 | 0.96 |
 | minimum flow | 80 % of norm. | 80 % of norm. |
 | one pack off | 60 % of norm. | 60 % of norm. |
 ----------------------------------------------------------------------------These nominal flows can vary by plus 5 % or minus 2 %.
 ----------------------------------------------------------------------------
| Total fresh air required from the APU: |
 |----------------------------------------------------------------------------|
 | hot day | +38 DEG.C (100.4 DEG.F) | 1.00 kg/s (Garrett) |
 | hot day | +38 DEG.C (100.4 DEG.F) | 1.09 kg/s (APIC) |
 | cold day | -23 DEG.C (-9.4 DEG.F) | 1.28 kg/s (Garrett) |
 | cold day | -23 DEG.C (-9.4 DEG.F) | 1.49 kg/s (APIC) |
 ----------------------------------------------------------------------------
**ON A/C ALL
 (2) Distribution Data
R **ON A/C 001-049, 051-099, 101-149, 201-299,
 (Ref. Fig. 002)


 AIR flows and cabin temperatures for normal operating and 1 pack failure cases

 Figure 002 
R 1EFF : 1 1 1CES  001-049, 051-099, 101-149, 201-299,  1 111 21-00-00 Page 5 May 01/05

 


R **ON A/C 151-199, 401-499,
 (Ref. Fig. 002A)
 **ON A/C 301-399,
 (Ref. Fig. 002B)
 **ON A/C ALL
 Distribution data for all normal operational cases and important failure cases are shown in table 1. For each case the following data is given:
 -Qt = total fresh airflow to the pressurized fuselage,
 -QFD = fresh airflow to the cockpit,
 -Qc = fresh airflow to the passenger cabin,
 -Qr = recirculation airflow from two recirculation fans,
 -number of cabin occupants,
 -mixed blown air per cabin occupant,
 -fresh air per flight crew member,
 -mixed blown air per flight crew member.
 3.
 Power Supply

____________
 (Ref. Fig. 003)


 4.
 Interface
 
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