GB538950A - Improvements in high-altitude aircraft - Google Patents
Improvements in high-altitude aircraftInfo
- Publication number
- GB538950A GB538950A GB125840A GB125840A GB538950A GB 538950 A GB538950 A GB 538950A GB 125840 A GB125840 A GB 125840A GB 125840 A GB125840 A GB 125840A GB 538950 A GB538950 A GB 538950A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blower
- cabin
- intake
- pressure
- controlled
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 239000002775 capsule Substances 0.000 abstract 3
- 230000004048 modification Effects 0.000 abstract 2
- 238000012986 modification Methods 0.000 abstract 2
- 238000006073 displacement reaction Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWERÂ PLANTSÂ OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/02—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being pressurised
- B64D13/04—Automatic control of pressure
Landscapes
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
Abstract
538,950. Aircraft cabins. BRISTOL AEROPLANE CO., Ltd., NIXON, F., and MARPLES, E. I. B. Jan. 20, 1940, No. 1258. [Class 4] A pressure cabin having an outlet valve controlled by a pressure-responsive device within the cabin in order to maintain a constant pressure above a pre-determined minimum, has means for maintaining a constant or controlled flow of air from a blower driven from a separate engine, said means acting on the throttle of the engine or the intake of the blower. In one form an outlet valve 13 on the cabin 10 is controlled by a capsule 11 and air is supplied to the cabin by a blower 16 driven by an engine 15 which is supercharged by an additional blower 25 taking air from the cabin. The output conduit 17 of the blower 16 has a restricted passage 18 and the pressure drop across this passage is utilized to control a throttle valve 24 in the engine intake. Alternatively or in addition the input to the blower 16 may be controlled by a valve 29 actuated by a capsule 27 subjected on one side to the pressure in the intake conduit of the blower. In another modification the pressure drop across the passage 18 controls the valve in the intake of the blower 16. In another modification wherein there is a varying consumption of air in the cabin a capsule subjected to the difference of pressure between the cabin and the delivery conduit of the blower actuates a throttle valve in the engine intake which is branched off the blower conduit. In this case a displacement blower may be used, but if a centrifugal blower be used its intake should also be controlled.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB125840A GB538950A (en) | 1940-01-20 | 1940-01-20 | Improvements in high-altitude aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB125840A GB538950A (en) | 1940-01-20 | 1940-01-20 | Improvements in high-altitude aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB538950A true GB538950A (en) | 1941-08-22 |
Family
ID=9718848
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB125840A Expired GB538950A (en) | 1940-01-20 | 1940-01-20 | Improvements in high-altitude aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB538950A (en) |
-
1940
- 1940-01-20 GB GB125840A patent/GB538950A/en not_active Expired
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2284984A (en) | High-altitude aircraft | |
| US2896599A (en) | Gaseous fuel feed systems, with automatic starting and idling control, for internal combustion engines | |
| US2414322A (en) | Charge forming device | |
| US2233307A (en) | Means for controlling aircraft engines | |
| US2500234A (en) | Compressor surge control for exhaust turbine driven superchargers | |
| US2447264A (en) | Carburetor | |
| GB538950A (en) | Improvements in high-altitude aircraft | |
| GB666797A (en) | Improvements in the fuel feeding of engines arranged at the ends of the blades of a rotary wing of an aircraft | |
| US2447791A (en) | Carburetor | |
| US2456605A (en) | Fuel supply system | |
| US2601975A (en) | Carburetor | |
| US2201693A (en) | Carburetor control | |
| US2935078A (en) | Fuel flow proportioners | |
| GB1180581A (en) | Cabin Air Flow Control System | |
| US2488250A (en) | Fuel feed control apparatus | |
| US2489214A (en) | Fuel supply system | |
| US2500088A (en) | Charge forming device | |
| US2868630A (en) | Gaseous fuel feed systems for internal combustion engines | |
| US2944537A (en) | Pressure carburetor | |
| US2382493A (en) | Aircraft heating system | |
| US2336424A (en) | Ignition controller | |
| US2400369A (en) | Charge forming device | |
| GB710261A (en) | Improvements in or relating to control arrangements for gas turbines and other primemovers | |
| GB760111A (en) | Improvements in or relating to mass flow control systems | |
| GB553349A (en) | Improvements in or relating to carburetters for internal combustion engines |