GB188650A - Improvements in aeroplane construction - Google Patents
Improvements in aeroplane constructionInfo
- Publication number
- GB188650A GB188650A GB29609/22A GB2960922A GB188650A GB 188650 A GB188650 A GB 188650A GB 29609/22 A GB29609/22 A GB 29609/22A GB 2960922 A GB2960922 A GB 2960922A GB 188650 A GB188650 A GB 188650A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plane
- fuselage
- aeroplanes
- fuselages
- pushers
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/04—Aircraft not otherwise provided for having multiple fuselages or tail booms
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Non-Deflectable Wheels, Steering Of Trailers, Or Other Steering (AREA)
- Toys (AREA)
- Catching Or Destruction (AREA)
Abstract
188,650. Soc. Anon. des Ateliers d'Aviation L. BrÚguet. Nov. 11, 1921, [Convention date]. Aeroplanes; planes, arrangement and construction of; cars; propelling; steering; skids.-Aeroplanes having the engines, tanks, goods &c. distributed as uniformly as possible within thick wings, are supported on two main fuselages b, c. having front portions formed as runners for starting and alighting, and supporting, in conjunction with a third fuselage g of smaller section, a narrow tail plane e and elevators f. The front end of the fuselage g has accommodation for the pilot. A rudder h is provided on each fuselage. Four tractor propellers i - - l and two pushers m, n are driven from separate engines arranged within the plane, or the propellers may be all pushers or all tractors. The fuel tanks are arranged in the plane a and the goods and passengers in the fuselages b, c and in the plane a. The machine may be fitted with the landing gear described in Specification 187,627.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR188650X | 1921-11-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB188650A true GB188650A (en) | 1924-01-30 |
Family
ID=8878834
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB29609/22A Expired GB188650A (en) | 1921-11-11 | 1922-10-30 | Improvements in aeroplane construction |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB188650A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010215035A (en) * | 2009-03-13 | 2010-09-30 | Global Energy Co Ltd | Three-fuselage aircraft |
-
1922
- 1922-10-30 GB GB29609/22A patent/GB188650A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010215035A (en) * | 2009-03-13 | 2010-09-30 | Global Energy Co Ltd | Three-fuselage aircraft |
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