GB632732A - Improvements relating to high-pressure compressed air systems for aircraft - Google Patents
Improvements relating to high-pressure compressed air systems for aircraftInfo
- Publication number
- GB632732A GB632732A GB1972047A GB1972047A GB632732A GB 632732 A GB632732 A GB 632732A GB 1972047 A GB1972047 A GB 1972047A GB 1972047 A GB1972047 A GB 1972047A GB 632732 A GB632732 A GB 632732A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pressure
- compressor
- air
- compressed air
- aircraft
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS 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
632,732. Compressed air systems. HYMATIC ENGINEERING CO., Ltd., HUNT, J. A., HAERLE, H. R., and JAY, J.B. July 23,1947, No. 19720. [Class 8(i)] In a high-pressure compressed air system for aircraft a high-pressure air,compressor 5 is supplied with air from a source of low pressure air 1 through a cooler 2 and a valve 9 which is controlled by the temperature; through a -thermostat 8, and if desired the pressure of the air delivered by the high-pressure compressor or an interstage thereof, by means of a spring-loaded piston 10. The compressor 5 may be driven by, and cooled by the exhaust 20 of; a turbine 18 driven by low-pressure air supplied through valves 13 and 16 controlled by the delivery pressure and speed respectively of the compressor 5. If the compressor is driven by an electric motor the latter is controlled by a pressure switch which stops the motor when the high-pressure air storage pressure 12 exceeds a predetermined maximum.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1972047A GB632732A (en) | 1947-07-23 | 1947-07-23 | Improvements relating to high-pressure compressed air systems for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1972047A GB632732A (en) | 1947-07-23 | 1947-07-23 | Improvements relating to high-pressure compressed air systems for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB632732A true GB632732A (en) | 1949-12-05 |
Family
ID=10134090
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1972047A Expired GB632732A (en) | 1947-07-23 | 1947-07-23 | Improvements relating to high-pressure compressed air systems for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB632732A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4684081A (en) * | 1986-06-11 | 1987-08-04 | Lockheed Corporation | Multifunction power system for an aircraft |
-
1947
- 1947-07-23 GB GB1972047A patent/GB632732A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4684081A (en) * | 1986-06-11 | 1987-08-04 | Lockheed Corporation | Multifunction power system for an aircraft |
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