GB462904A - Improvements in spars for the wings of aircraft - Google Patents
Improvements in spars for the wings of aircraftInfo
- Publication number
- GB462904A GB462904A GB2556935A GB2556935A GB462904A GB 462904 A GB462904 A GB 462904A GB 2556935 A GB2556935 A GB 2556935A GB 2556935 A GB2556935 A GB 2556935A GB 462904 A GB462904 A GB 462904A
- Authority
- GB
- United Kingdom
- Prior art keywords
- spars
- shells
- spar
- aircraft
- strips
- 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
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/185—Spars
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Abstract
462,904. Aircraft wing spars. VOGT, R. Sept. 14, 1935, No. 25569. [Class 4] A conical tubular spar a, Figs. 1 and 2, tor single-spar aircraft wings consists of two approximately semicircular shells d, the abutting edges of which are overlapped by cover strips e. Shells d are of uniform thickness, but the breadth of strips e is varied along the span. In a modification, Fig. 3, shells g rolled into the sections shown from sheet metal are welded together along the neutral plane of the spar. The spars may be employed as fuel containers.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2556935A GB462904A (en) | 1935-09-14 | 1935-09-14 | Improvements in spars for the wings of aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2556935A GB462904A (en) | 1935-09-14 | 1935-09-14 | Improvements in spars for the wings of aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB462904A true GB462904A (en) | 1937-03-15 |
Family
ID=10229809
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2556935A Expired GB462904A (en) | 1935-09-14 | 1935-09-14 | Improvements in spars for the wings of aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB462904A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2619301A (en) * | 1948-02-02 | 1952-11-25 | Theodore P Hall | Flight component for ground vehicles adapted to be airborne |
US2681778A (en) * | 1950-09-29 | 1954-06-22 | Landrum L Hughes | Fuel storage system for aircraft |
GB2315054A (en) * | 1996-07-10 | 1998-01-21 | Christos Rugeris | Wing with inflatable spars and rigid ribs |
WO2009080736A1 (en) * | 2007-12-21 | 2009-07-02 | Airbus España S.L. | Aircraft control surface |
CN102317154B (en) * | 2007-04-05 | 2015-09-09 | 波音公司 | A kind of method and system of composite structural truss |
-
1935
- 1935-09-14 GB GB2556935A patent/GB462904A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2619301A (en) * | 1948-02-02 | 1952-11-25 | Theodore P Hall | Flight component for ground vehicles adapted to be airborne |
US2681778A (en) * | 1950-09-29 | 1954-06-22 | Landrum L Hughes | Fuel storage system for aircraft |
GB2315054A (en) * | 1996-07-10 | 1998-01-21 | Christos Rugeris | Wing with inflatable spars and rigid ribs |
CN102317154B (en) * | 2007-04-05 | 2015-09-09 | 波音公司 | A kind of method and system of composite structural truss |
EP2139761B1 (en) * | 2007-04-05 | 2017-01-18 | The Boeing Company | Methods and systems for composite structural truss |
WO2009080736A1 (en) * | 2007-12-21 | 2009-07-02 | Airbus España S.L. | Aircraft control surface |
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