GB262511A - Improvements in or relating to built-up girders or frames more particularly of airships or other aircraft - Google Patents
Improvements in or relating to built-up girders or frames more particularly of airships or other aircraftInfo
- Publication number
- GB262511A GB262511A GB22536/25A GB2253625A GB262511A GB 262511 A GB262511 A GB 262511A GB 22536/25 A GB22536/25 A GB 22536/25A GB 2253625 A GB2253625 A GB 2253625A GB 262511 A GB262511 A GB 262511A
- Authority
- GB
- United Kingdom
- Prior art keywords
- longitudinals
- girders
- built
- airships
- aircraft
- 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
- B64C1/08—Geodetic or other open-frame structures
-
- 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)
Abstract
262,511. Airship Guarantee Co., Ltd., and Wallis, B. N. Sept. 9, 1925. Framework.-Girders of varying width or curvature are built up from longitudinals and bracing members, the latter being of one or a few standard lengths but being secured to the longitudinals so as to have the desired effective length. In one arrangement, the longitudinals are straddled by socket members 3 into which the bracing members 2 are inserted to a greater or less extent. In a modification the longitudinals are provided with side plates 5 shaped so as to allow the bracing member to be set at various angles to the axis of the longitudinal. Specification 262,512, [Class 83 (iv), Metals, Working], is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB22536/25A GB262511A (en) | 1925-09-09 | 1925-09-09 | Improvements in or relating to built-up girders or frames more particularly of airships or other aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB22536/25A GB262511A (en) | 1925-09-09 | 1925-09-09 | Improvements in or relating to built-up girders or frames more particularly of airships or other aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB262511A true GB262511A (en) | 1926-12-09 |
Family
ID=10180970
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB22536/25A Expired GB262511A (en) | 1925-09-09 | 1925-09-09 | Improvements in or relating to built-up girders or frames more particularly of airships or other aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB262511A (en) |
-
1925
- 1925-09-09 GB GB22536/25A patent/GB262511A/en not_active Expired
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