GB571592A - Improvements in aeroplanes - Google Patents
Improvements in aeroplanesInfo
- Publication number
- GB571592A GB571592A GB3440/44A GB344044A GB571592A GB 571592 A GB571592 A GB 571592A GB 3440/44 A GB3440/44 A GB 3440/44A GB 344044 A GB344044 A GB 344044A GB 571592 A GB571592 A GB 571592A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cabin
- engine
- radiator
- petrol tank
- martin
- 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 POWERÂ PLANTSÂ OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Supercharger (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
571,592. Aeroplanes. MARTIN, J., and MARTIN-BAKER AIRCRAFT CO., Ltd. Feb. 24, 1944, No. 3440. [Class 4] A monoplane of the type in which the engine 4 is disposed to the rear of the pilot's cabin 11 and in which the airscrew is driven by. an extension shaft 6 passing through the cabin, has the radiator .and oil cooler 15 and petrol tank 5 placed between the cabin and engine, the rear of the cabin being in advance of the leading edge of the wing 2. In the arrangement shown, the petrol tank and engine are disposed between the leading and trailing edges of the wing. The driving shaft 6 extends through the petrol tank and radiator to a reduction gear-box 7, and is supported by a bearing 6a in the cabin. Air intakes 19, 21, for the radiator and engine supercharger are provided below the fuselage. The arrangement enables the engine and various accessories to be placed in line along the longitudinal axis of the machine, and to be protected by a compact arrangement of armouring. Specifications 541,506 and 547,178 are referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3440/44A GB571592A (en) | 1944-02-24 | 1944-02-24 | Improvements in aeroplanes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3440/44A GB571592A (en) | 1944-02-24 | 1944-02-24 | Improvements in aeroplanes |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB571592A true GB571592A (en) | 1945-08-31 |
Family
ID=9758363
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3440/44A Expired GB571592A (en) | 1944-02-24 | 1944-02-24 | Improvements in aeroplanes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB571592A (en) |
-
1944
- 1944-02-24 GB GB3440/44A patent/GB571592A/en not_active Expired
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