GB527025A - Improvements in or relating to heating apparatus for the cabins of aircraft - Google Patents
Improvements in or relating to heating apparatus for the cabins of aircraftInfo
- Publication number
- GB527025A GB527025A GB9670/39A GB967039A GB527025A GB 527025 A GB527025 A GB 527025A GB 9670/39 A GB9670/39 A GB 9670/39A GB 967039 A GB967039 A GB 967039A GB 527025 A GB527025 A GB 527025A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- cabin
- pipe
- pipes
- cabins
- 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
- 238000010438 heat treatment Methods 0.000 title abstract 3
- 239000007789 gas Substances 0.000 abstract 2
- JHIVVAPYMSGYDF-UHFFFAOYSA-N cyclohexanone Chemical compound O=C1CCCCC1 JHIVVAPYMSGYDF-UHFFFAOYSA-N 0.000 abstract 1
- 238000005192 partition 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 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
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D13/08—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned the air being heated or cooled
Landscapes
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Air-Conditioning For Vehicles (AREA)
Abstract
527,025. Heating aircraft. SULZER FRERES SOC. ANON. March 28, 1939, No. 9670. Convention date, May 4, 1938. [Classes 64 (ii) and 64 (iii)] Heat is transmitted from exhaust gases to air which in turn transmits heat to air passing into aircraft cabins. The engine exhaust pipe 8 opens at 10 into the air, and air entering at 12 passes through a jacket 11, and thence through pipes 13, 14, 15, 16, 17 to outlets 21, 22. Air for heating the cabin enters at 23 and passes through valve 25 to injector nozzle 34, which may draw air from cabin 7 through pipe 35 into space 33 and which delivers it to pipes 26, 27 surrounding pipes 16, 17. Warmed air is delivered into the cabin 7 and also through pipe 32 into the pilot's cabin 5. The inner pipes 16, 17 may be plain, or corrugated as in Fig. 3, and the annular space may be longitudinally divided by partitions 37. Outlet nozzles 28, 30 communicate with the smaller chamber 38, and nozzles 29, 31 with the larger chamber 39. The pipe 13 communicates with the air through valve-controlled pipe 46. The intermediate air may be heated to about 200‹C. by the exhaust gas, and the air entering the cabins may be heated to 35‹C. The injector 33 is employed to circulate air from the cabin when atmospheric temperature is exceptionally low. Reference has been directed by the Comptroller to Specification 305,627, [Class 64 (ii)].
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH527025X | 1938-05-04 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB527025A true GB527025A (en) | 1940-10-01 |
Family
ID=4518252
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB9670/39A Expired GB527025A (en) | 1938-05-04 | 1939-03-28 | Improvements in or relating to heating apparatus for the cabins of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB527025A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2984415A (en) * | 1957-02-16 | 1961-05-16 | Daimler Benz Ag | Heating and ventilating system for motor vehicles |
| US3168244A (en) * | 1962-05-25 | 1965-02-02 | Gospodar Reinhard | Heating systems for motor vehicles |
| GB2137331A (en) * | 1983-03-18 | 1984-10-03 | Martell Electronics Limited | Method and apparatus for heating or cooling explosive or flammable material |
| EP0223471A2 (en) * | 1985-11-05 | 1987-05-27 | British Aerospace Public Limited Company | Fluid flow distribution ducts |
-
1939
- 1939-03-28 GB GB9670/39A patent/GB527025A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2984415A (en) * | 1957-02-16 | 1961-05-16 | Daimler Benz Ag | Heating and ventilating system for motor vehicles |
| US3168244A (en) * | 1962-05-25 | 1965-02-02 | Gospodar Reinhard | Heating systems for motor vehicles |
| GB2137331A (en) * | 1983-03-18 | 1984-10-03 | Martell Electronics Limited | Method and apparatus for heating or cooling explosive or flammable material |
| EP0223471A2 (en) * | 1985-11-05 | 1987-05-27 | British Aerospace Public Limited Company | Fluid flow distribution ducts |
| EP0223471A3 (en) * | 1985-11-05 | 1989-02-22 | British Aerospace Public Limited Company | Fluid flow distribution ducts |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB704622A (en) | Fuel system for jet and rocket motors | |
| GB650608A (en) | Improvements relating to internal combustion engine systems | |
| US2458066A (en) | Combustion chamber | |
| GB1427540A (en) | Devices for prevapourising liquid fuel | |
| GB527025A (en) | Improvements in or relating to heating apparatus for the cabins of aircraft | |
| US1610825A (en) | Carburetor for internal-combustion engines | |
| US3101768A (en) | Resonant intermittent combustion devices | |
| GB899350A (en) | Air heating apparatus | |
| GB697027A (en) | Combustion chambers for prime movers | |
| GB481139A (en) | Improvements in or relating to carburettors for internal combustion engines | |
| GB491483A (en) | Improvements in or relating to exhaust systems for aircraft engines | |
| GB620073A (en) | Improvements in or relating to combustion systems for gas turbines with heat exchangers | |
| US1709032A (en) | Fuel-saving device | |
| GB302717A (en) | Improved process and an apparatus for producing a combustible charge for use in internal combustion engines | |
| GB490576A (en) | Improvements in or relating to apparatus for vapourization of fuel, especially heavy mineral oils | |
| GB531864A (en) | Improvements in and relating to the utilisation of the exhaust gases of internal combustion aircraft engines | |
| GB374220A (en) | Improvements in and relating to the supply of combustion air to internal combustion engines | |
| GB588284A (en) | New and improved liquid circulation system for cooling internal combustion engines | |
| GB595864A (en) | Improvements relating to systems for the prevention of icing in or the removal of icing from aircraft | |
| GB704124A (en) | Liquid cooling systems for internal combustion engines | |
| GB935573A (en) | Furnace for the pyrolytic production of acetylene | |
| GB515273A (en) | Improvements in or relating to the utilization of exhaust gases from internal combustion engines | |
| GB563112A (en) | Improvements relating to the heating of aircraft | |
| GB726995A (en) | Improvements in or relating to heating apparatus | |
| GB574489A (en) | Improvements in or relating to means for aeroplane propulsion |