GB366079A - Improvements in aircraft - Google Patents
Improvements in aircraftInfo
- Publication number
- GB366079A GB366079A GB25289/30A GB2528930A GB366079A GB 366079 A GB366079 A GB 366079A GB 25289/30 A GB25289/30 A GB 25289/30A GB 2528930 A GB2528930 A GB 2528930A GB 366079 A GB366079 A GB 366079A
- Authority
- GB
- United Kingdom
- Prior art keywords
- spar
- wing
- aug
- bolts
- class
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
Abstract
366,079. Aircraft wing structures. MESSERSCHMITT, W., 118A, Haunstetterstrasse, Augsburg, Germany. Aug. 25, 1930, No. 25289. Convention date, Aug. 23, 1929. [Class 4.] An aircraft structure comprises a single main spar and leading and trailing members substantially devoid of longitudinal strength but of considerable lateral rigidity detachably connected to the spar at its flanges alone. As applied to a wing, front and rear girders d, e, Fig. 1, are bolted to plates b attached to flanges of spar a. A releasable connection may be provided at f. Separate longitudinally extending strips g may be placed under each row of nuts or broad strips, Fig. 3, serving for two adjacent rows may be fitted. In a modification every third rib may be connected to. the spar web by angle-pieces i. Hinges may be employed instead of bolts. Manholes may be provided in the covering where required. The bolts are secured by screwing or welding to prevent their dropping on to the wing. Specification 315,793, [Class 4, Aeronautics], is referred to.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE366079X | 1929-08-23 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB366079A true GB366079A (en) | 1932-01-25 |
Family
ID=6317713
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB25289/30A Expired GB366079A (en) | 1929-08-23 | 1930-08-25 | Improvements in aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB366079A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2421960A (en) * | 1943-09-17 | 1947-06-10 | Budd Co | Hinge mounting |
| US2443323A (en) * | 1944-05-10 | 1948-06-15 | Universal Moulded Products Cor | Airplane control surface |
| WO2008032040A1 (en) | 2006-09-12 | 2008-03-20 | Gkn Aerospace Services Limited | Rib post |
| CN106335629A (en) * | 2015-07-06 | 2017-01-18 | 埃姆普里萨有限公司 | Airframe wing spar structures with continuous unitary and integrally fastened upper and lower chord sections |
-
1930
- 1930-08-25 GB GB25289/30A patent/GB366079A/en not_active Expired
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2421960A (en) * | 1943-09-17 | 1947-06-10 | Budd Co | Hinge mounting |
| US2443323A (en) * | 1944-05-10 | 1948-06-15 | Universal Moulded Products Cor | Airplane control surface |
| WO2008032040A1 (en) | 2006-09-12 | 2008-03-20 | Gkn Aerospace Services Limited | Rib post |
| US8393575B2 (en) | 2006-09-12 | 2013-03-12 | Gkn Aerospace Services Limited | Rib post |
| CN106335629A (en) * | 2015-07-06 | 2017-01-18 | 埃姆普里萨有限公司 | Airframe wing spar structures with continuous unitary and integrally fastened upper and lower chord sections |
| CN106335629B (en) * | 2015-07-06 | 2021-06-11 | 埃姆普里萨有限公司 | Fuselage spar structure with continuous integral fastened upper and lower chord sections |
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