GB482135A - Improvements relating to aeroplane wings - Google Patents
Improvements relating to aeroplane wingsInfo
- Publication number
- GB482135A GB482135A GB25962/36A GB2596236A GB482135A GB 482135 A GB482135 A GB 482135A GB 25962/36 A GB25962/36 A GB 25962/36A GB 2596236 A GB2596236 A GB 2596236A GB 482135 A GB482135 A GB 482135A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- portions
- boom
- engine
- members
- 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
- 230000004048 modification Effects 0.000 abstract 2
- 238000012986 modification Methods 0.000 abstract 2
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
- 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)
- On-Site Construction Work That Accompanies The Preparation And Application Of Concrete (AREA)
Abstract
482,135. Mounting aero - engines in wings. BRISTOL AEROPLANE CO., Ltd., FEDDEN, A. H. R., OWNER, F. M., and COPLEY, J. W. May 4, 1937, No. 25962. [Class 4] An aeroplane is provided with a wing built of two or more detachable sections, one of which contains the engine which is of the horizontally-opposed cylinder type, having its crankshaft-axis lying fore and aft of the wing and is supported near the middle and at the rear by frames which are fastened to the end of spar portions in the adjacent wing sections. In Fig. 1 a wing root section 11 is permanently attached to the fuselage 10. A middle section 12 containing the engine is adjacent the root portion 11 and a tip portion 14 completes the wing. The middle section of the wing comprises a forward and rearward frame each comprising upper and lower channelsection boom-portions 15, 16, Figs. 2 and 3, connected by vertical members 17, 18 and diagonal members 23, 24. The members 23, 24 may be arranged in the chain-and-dot position depending on the rotation of the engine and the side of the aeroplane on which the section is carried. The forward and rearward frames are connected by members 31. The engine is mounted on the frames by means of flanges 39 which enter the channels of the boom-portions and are-riveted and bolted thereto. The ends of the boom portions are formed with lugs 47-50 by means of which this section is connected to the root and tip portions of the wing. In a modification the engine crankcase is connected by blocks to the boom-portions which are connected by cross-shaped braces, or diagonal members may be connected between the boom-portions and lugs on the crankcase. In a further modification the flanges 39 form a part of the profile of the wing and are formed with lugs to which short boom-portions are attached connected together by vertical and diagonal members.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB25962/36A GB482135A (en) | 1937-05-04 | 1937-05-04 | Improvements relating to aeroplane wings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB25962/36A GB482135A (en) | 1937-05-04 | 1937-05-04 | Improvements relating to aeroplane wings |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB482135A true GB482135A (en) | 1938-03-24 |
Family
ID=10236133
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB25962/36A Expired GB482135A (en) | 1937-05-04 | 1937-05-04 | Improvements relating to aeroplane wings |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB482135A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2753140A (en) * | 1951-07-28 | 1956-07-03 | United Aircraft Corp | Engine mount |
-
1937
- 1937-05-04 GB GB25962/36A patent/GB482135A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2753140A (en) * | 1951-07-28 | 1956-07-03 | United Aircraft Corp | Engine mount |
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