GB243168A - Improvements in or relating to engine-mountings for aircraft - Google Patents
Improvements in or relating to engine-mountings for aircraftInfo
- Publication number
- GB243168A GB243168A GB28669/24A GB2866924A GB243168A GB 243168 A GB243168 A GB 243168A GB 28669/24 A GB28669/24 A GB 28669/24A GB 2866924 A GB2866924 A GB 2866924A GB 243168 A GB243168 A GB 243168A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- aircraft
- frame
- connects
- length
- 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
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/04—Aircraft characterised by the type or position of power plants of piston type
- B64D27/06—Aircraft characterised by the type or position of power plants of piston type within, or attached to, wings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
243,168. Supermarine Aviation Works, Ltd., and Mitchell, R. J. Nov. 29, 1924. Propelling.-An engine is detachably mounted outside the hull or fuselage of a flying boat or like aircraft by means of a pyramidal frame detachably secured at its apex to the aircraft and braced by two additional strut members which may be adjustable in length. The Figure shows in plan two engine bearers 13, 14 connected togethe'd and supported on four downwardly convergent struts 15 - - 18 secured by a pin joint at 19 to the front spar of the lower wing of a biplane. A longitudinally disposed V-shaped bracing member 21, 22 connects the end of the pyramidal frame to the rear spar of the wing at 23, and a similar member 25, 26 connects the side of the frame to the front spar at 27. The members 21, 22, 25, 26 may be variable in length to adjust the alignment of the engine.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB28669/24A GB243168A (en) | 1924-11-29 | 1924-11-29 | Improvements in or relating to engine-mountings for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB28669/24A GB243168A (en) | 1924-11-29 | 1924-11-29 | Improvements in or relating to engine-mountings for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB243168A true GB243168A (en) | 1925-11-26 |
Family
ID=10279251
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB28669/24A Expired GB243168A (en) | 1924-11-29 | 1924-11-29 | Improvements in or relating to engine-mountings for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB243168A (en) |
-
1924
- 1924-11-29 GB GB28669/24A patent/GB243168A/en not_active Expired
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2434068A (en) | Roadable airplane with folding and detachable wings | |
GB243168A (en) | Improvements in or relating to engine-mountings for aircraft | |
US1887411A (en) | Aircraft construction | |
GB376634A (en) | Elastic seaplane undercarriages | |
GB470650A (en) | Improvements in or relating to aircraft | |
US1801418A (en) | Flying machine | |
GB404963A (en) | Improvements in and connected with the construction and arrangement of aeroplane wings | |
GB283980A (en) | Improvements in or relating to aeroplanes | |
US1921428A (en) | Aircraft structure | |
GB556478A (en) | Improvements in or relating to aircraft wings | |
US1745749A (en) | Flying machine | |
US1557790A (en) | Motor arrangement for aircraft | |
US1804790A (en) | Aircraft | |
GB381270A (en) | Improvements relating to the wings of aeroplanes | |
US1858726A (en) | Airplane engine arrangement | |
US2114606A (en) | Airplane | |
US1934678A (en) | Airplane motor mounting | |
GB346244A (en) | Improvements in or relating to collapsible or folding aeroplane wings | |
GB471946A (en) | Improvements in or relating to aircraft | |
GB199005A (en) | Improvements in the construction of flying machines | |
GB598813A (en) | Improvements in or relating to transport-planes | |
GB329097A (en) | Improvements in or relating to aircraft | |
GB218043A (en) | Improvements in aeroplane flying machines or hydroaeroplanes | |
GB338783A (en) | Improvements in and relating to aircraft | |
GB429186A (en) | Improvements in or connected with biplane wing systems for aircraft |