GB212993A - Improvements in the construction of supporting planes for flying machines - Google Patents
Improvements in the construction of supporting planes for flying machinesInfo
- Publication number
- GB212993A GB212993A GB34838/22A GB3483822A GB212993A GB 212993 A GB212993 A GB 212993A GB 34838/22 A GB34838/22 A GB 34838/22A GB 3483822 A GB3483822 A GB 3483822A GB 212993 A GB212993 A GB 212993A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- girder
- construction
- central part
- tips
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
212,993. Invernairn, (W. Beardmore), Lord, and Chorlton, A. E. L. Dec. 21. 1922. Planes, construction of.-In a wing built up in three parts with the central part constituted by a box girder, the stressed upper and lower metal surfaces of the girder are laminated, the number of superposed metal plates being decreased towards the wing tips as shown A, A<1>, A<2> and B, B<1> B<2>. The depth of the flanges D, E may also decrease towards the tips. The joints in the superposed layers may be arranged out of line as shown in Fig. 5. The innermost plates may be stiffened on the inner side by light metal trays. The front and rear former parts L, M of the wing may be hinged to the central part at their lower edges and be formed with open frames sufficiently elastic to be accommodated t'o the girder and fixed thereto at the upper edges by bolts passing through extensions N.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB34838/22A GB212993A (en) | 1922-12-21 | 1922-12-21 | Improvements in the construction of supporting planes for flying machines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB34838/22A GB212993A (en) | 1922-12-21 | 1922-12-21 | Improvements in the construction of supporting planes for flying machines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB212993A true GB212993A (en) | 1924-03-21 |
Family
ID=10370517
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB34838/22A Expired GB212993A (en) | 1922-12-21 | 1922-12-21 | Improvements in the construction of supporting planes for flying machines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB212993A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3093219A (en) * | 1961-04-06 | 1963-06-11 | Monte Copter Inc | Plural-section airfoils |
US4749155A (en) * | 1985-09-30 | 1988-06-07 | The Boeing Company | Method of making wing box cover panel |
EP3421355A1 (en) * | 2017-06-29 | 2019-01-02 | Airbus Operations GmbH | Aerofoil structure and method of assembly |
CN111605716A (en) * | 2019-02-22 | 2020-09-01 | 空中客车运营简化股份公司 | Main structure of aircraft hanging rack and aircraft |
-
1922
- 1922-12-21 GB GB34838/22A patent/GB212993A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3093219A (en) * | 1961-04-06 | 1963-06-11 | Monte Copter Inc | Plural-section airfoils |
US4749155A (en) * | 1985-09-30 | 1988-06-07 | The Boeing Company | Method of making wing box cover panel |
EP3421355A1 (en) * | 2017-06-29 | 2019-01-02 | Airbus Operations GmbH | Aerofoil structure and method of assembly |
CN111605716A (en) * | 2019-02-22 | 2020-09-01 | 空中客车运营简化股份公司 | Main structure of aircraft hanging rack and aircraft |
CN111605716B (en) * | 2019-02-22 | 2024-02-20 | 空中客车运营简化股份公司 | Main structure of aircraft hanging frame and aircraft |
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