GB329614A - Improvements in aeroplane fuselage construction - Google Patents
Improvements in aeroplane fuselage constructionInfo
- Publication number
- GB329614A GB329614A GB5968/30A GB596830A GB329614A GB 329614 A GB329614 A GB 329614A GB 5968/30 A GB5968/30 A GB 5968/30A GB 596830 A GB596830 A GB 596830A GB 329614 A GB329614 A GB 329614A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aeroplane fuselage
- fuselage construction
- aeroplane
- construction
- burnelli
- 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
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/10—Bulkheads
-
- 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
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
329,614. Burnelli, V., J. Feb. 4, 1929, [Convention date]. Divided on 329,489. Fuselages; cars.-An aeroplane fuselage has a bulkhead 10 opposite the rear spars of the wings, which has a central member 10<a>, this member and the frame having strengthening ribs 33, 33<a> which merge into a structure 34 forming couches for passengers. The webs are shaped to provide clearance spaces 35. 36 and are strengthened by flanges 33<b>. Specification 329,489 is referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US329614XA | 1929-02-04 | 1929-02-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB329614A true GB329614A (en) | 1930-05-22 |
Family
ID=21867811
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5968/30A Expired GB329614A (en) | 1929-02-04 | 1929-05-01 | Improvements in aeroplane fuselage construction |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB329614A (en) |
-
1929
- 1929-05-01 GB GB5968/30A patent/GB329614A/en not_active Expired
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