GB307620A - Improvements in aeroplanes - Google Patents
Improvements in aeroplanesInfo
- Publication number
- GB307620A GB307620A GB6455/28A GB645528A GB307620A GB 307620 A GB307620 A GB 307620A GB 6455/28 A GB6455/28 A GB 6455/28A GB 645528 A GB645528 A GB 645528A GB 307620 A GB307620 A GB 307620A
- Authority
- GB
- United Kingdom
- Prior art keywords
- compartment
- fuselage
- longerons
- doors
- seats
- 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
- 239000006096 absorbing agent Substances 0.000 abstract 1
- 239000000446 fuel Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Types And Forms Of Lifts (AREA)
Abstract
307,620. Burnelli, V. J. March 1, 1928. Aeroplanes; fuselages ; propelling ; tanks, arrangement of.-An aeroplane fuselage is made of aerofoil form in longitudinal section and of sufficient width to accommodate two engines driving two tractor propellers at its forward end. The fuselage is supported directly by landing gear of the same track width. Planes 15, 16 of small span are connected thereto and the rear edge carries an elevator 57 and two rudders 56. The fuselage is built around six longerons, two in the plane of symmetry of the machine and has transverse bulkheads dividing it into an engine compartment 31, nassenger compartment 32 and a luggage and lavatory compartment 44. The passenger compartment has seats 39 and 40, the latter serving as sleeping berths, and additional berths 41, Fig. 1, may be suspended from the central framework. Doors are formed in the bulkheads and doors 30 at the sides give access to the interior. Fuel may be stored in tanks beneath the seats 40. Skids ; shock-absorbers, applications of. - A skid 50 hinged to a strut 51 adjoining the central longerons is sprung by an elastic element 55 in a tie 54.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB6455/28A GB307620A (en) | 1928-03-01 | 1928-03-01 | Improvements in aeroplanes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB6455/28A GB307620A (en) | 1928-03-01 | 1928-03-01 | Improvements in aeroplanes |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB307620A true GB307620A (en) | 1929-03-14 |
Family
ID=9814769
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB6455/28A Expired GB307620A (en) | 1928-03-01 | 1928-03-01 | Improvements in aeroplanes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB307620A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2293809A1 (en) * | 2005-01-24 | 2008-03-16 | Reiner Eads Deutschland Gmbh | Rear fuselage section for airfreighter, has vertical tail segment with end frames having reinforcement bars that are connected with nodal points of frames by space bars which are bent in course |
| US8729912B2 (en) | 2008-10-02 | 2014-05-20 | Cellnovo Limited | Displacement sensor |
-
1928
- 1928-03-01 GB GB6455/28A patent/GB307620A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2293809A1 (en) * | 2005-01-24 | 2008-03-16 | Reiner Eads Deutschland Gmbh | Rear fuselage section for airfreighter, has vertical tail segment with end frames having reinforcement bars that are connected with nodal points of frames by space bars which are bent in course |
| US8729912B2 (en) | 2008-10-02 | 2014-05-20 | Cellnovo Limited | Displacement sensor |
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