GB329613A - Improvements in aeroplane fuselage construction - Google Patents
Improvements in aeroplane fuselage constructionInfo
- Publication number
- GB329613A GB329613A GB5967/30A GB596730A GB329613A GB 329613 A GB329613 A GB 329613A GB 5967/30 A GB5967/30 A GB 5967/30A GB 596730 A GB596730 A GB 596730A GB 329613 A GB329613 A GB 329613A
- Authority
- GB
- United Kingdom
- Prior art keywords
- members
- bulkhead
- fuselage construction
- aeroplane fuselage
- 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)
- Refrigerator Housings (AREA)
- Body Structure For Vehicles (AREA)
Abstract
329,613. Burnelli, V. J. Feb. 4, 1929, [Convention date]. Divided on 329,489. Fuselages; cars.-A fuselage bulkhead situated opposite the front spars of the wings and separating the pilot's compartment from the passenger compartment comprises upper and lower horizontal members 21, 21a and vertical members 22 - - 26, windows 29 being formed above the member 21 and doors 30 between the members 21, 21<a> as shown. Recesses 42 are formed in the lower edge of the bulkhead to accommodate retractible landing wheels. Specification. 329.489 is referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US329613XA | 1929-02-04 | 1929-02-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB329613A true GB329613A (en) | 1930-05-22 |
Family
ID=21867810
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5967/30A Expired GB329613A (en) | 1929-02-04 | 1929-05-01 | Improvements in aeroplane fuselage construction |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB329613A (en) |
-
1929
- 1929-05-01 GB GB5967/30A patent/GB329613A/en not_active Expired
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