GB367122A - Radiator for aeroplanes - Google Patents
Radiator for aeroplanesInfo
- Publication number
- GB367122A GB367122A GB1506/31A GB150631A GB367122A GB 367122 A GB367122 A GB 367122A GB 1506/31 A GB1506/31 A GB 1506/31A GB 150631 A GB150631 A GB 150631A GB 367122 A GB367122 A GB 367122A
- Authority
- GB
- United Kingdom
- Prior art keywords
- outlet openings
- aircraft
- casings
- wings
- radiator
- 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
- 238000007689 inspection 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
- B64D33/10—Radiator arrangement
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Testing Of Engines (AREA)
Abstract
367,122. Engine radiators on aircraft. MESSIER, G. L. R. J., 29, Avenue Leon Gambetta, Montrouge, Seine, France. Jan. 16, 1931, No. 1506. Convention date, Jan. 25, 1930. [Class 4.] The radiators A<1>, A<2> of water-cooled aircraft engines are disposed in casings in the wings, such casings having nozzle-shaped air inlet and outlet openings c<1>, Fig. 2, and D<1>, Fig. 3, respectively. The outlet openings may be arranged either on the upper, lower or both surfaces of the wings or in the trailing edge thereof. Both the inlet and the outlet openings may be made adjustable. The Specification as open to inspection under Sect. 91 (3) (a) comprises also the arrangement of a radiator in a recess in the body of the aircraft. This subject-matter does not appear in the Specification as accepted.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR367122X | 1930-01-25 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB367122A true GB367122A (en) | 1932-02-18 |
Family
ID=8894380
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1506/31A Expired GB367122A (en) | 1930-01-25 | 1931-01-16 | Radiator for aeroplanes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB367122A (en) |
-
1931
- 1931-01-16 GB GB1506/31A patent/GB367122A/en not_active Expired
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