GB504423A - Improvements in or relating to lightweight structural members, more particularly for aircraft construction - Google Patents
Improvements in or relating to lightweight structural members, more particularly for aircraft constructionInfo
- Publication number
- GB504423A GB504423A GB15748/38A GB1574838A GB504423A GB 504423 A GB504423 A GB 504423A GB 15748/38 A GB15748/38 A GB 15748/38A GB 1574838 A GB1574838 A GB 1574838A GB 504423 A GB504423 A GB 504423A
- Authority
- GB
- United Kingdom
- Prior art keywords
- structural members
- relating
- outer layers
- ribs
- aircraft construction
- 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
- B64C1/40—Sound or heat insulation, e.g. using insulation blankets
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
504,423. Aircraft - floats. DORNIERWERKE GES., and DORNIER, C. May 26, 1938, No. 15748. Convention date, June 10, 1937. [Class 113 (ii)] [Also in Group V] Structural members suitable for use in the construction of floats of aircraft consist of an inner core of sponge rubber or the like, with outer layers of hardened rubber, the outer layers being connected together by pillars or ribs of the same material. The outer layers 5, 8, which may be reinforced by fabric inserts 6, are connected by pillars or ribs 9. The rigidity may be increased by inwardly projecting ribs 7.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE504423X | 1937-06-10 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB504423A true GB504423A (en) | 1939-04-25 |
Family
ID=6546194
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15748/38A Expired GB504423A (en) | 1937-06-10 | 1938-05-26 | Improvements in or relating to lightweight structural members, more particularly for aircraft construction |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB504423A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2509494A (en) * | 1944-02-16 | 1950-05-30 | Louis A Gruenwald | Art of lamination |
-
1938
- 1938-05-26 GB GB15748/38A patent/GB504423A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2509494A (en) * | 1944-02-16 | 1950-05-30 | Louis A Gruenwald | Art of lamination |
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