GB734959A - Improvements in or relating to hinges for aircraft control surfaces - Google Patents
Improvements in or relating to hinges for aircraft control surfacesInfo
- Publication number
- GB734959A GB734959A GB466853A GB466853A GB734959A GB 734959 A GB734959 A GB 734959A GB 466853 A GB466853 A GB 466853A GB 466853 A GB466853 A GB 466853A GB 734959 A GB734959 A GB 734959A
- Authority
- GB
- United Kingdom
- Prior art keywords
- hinges
- control surface
- feb
- relating
- axis
- 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
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/02—Mounting or supporting thereof
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
Abstract
734,959. Hinges. BOULTON PAUL AIRCRAFT, Ltd. Feb. 19, 1954 [Feb. 19, 1953], No. 4668/53. Class 65(2). [Also in Group XXXIII] A control surface is hingedly connected to an aircraft wing (see Group XXXIII) by one or more conventional hinges and also by one or more hinges free to rotate about an axis chordwise of the control surface and capable of sliding movement along the said axis. As shown, an eyebolt 5 is pinned to the wing 2, and supports in its eye by means of roller bearings 12 an axle 9, extensions 10 and 11 of which are screwed into two part cylindrical members 8 which together fit into a cylindrical bore 7 in the control surface so as to be capable of sliding and rotating therein. Preferably a plurality of these hinges are disposed along the hinge line, with a conventional hinge at each end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB466853A GB734959A (en) | 1953-02-19 | 1953-02-19 | Improvements in or relating to hinges for aircraft control surfaces |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB466853A GB734959A (en) | 1953-02-19 | 1953-02-19 | Improvements in or relating to hinges for aircraft control surfaces |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB734959A true GB734959A (en) | 1955-08-10 |
Family
ID=9781535
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB466853A Expired GB734959A (en) | 1953-02-19 | 1953-02-19 | Improvements in or relating to hinges for aircraft control surfaces |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB734959A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3140066A (en) * | 1962-12-04 | 1964-07-07 | North American Aviation Inc | Multiple pivot mounting means |
| US4531417A (en) * | 1980-09-29 | 1985-07-30 | Hollman Nils David | Hinge-type angle setting device |
| DE102012006187A1 (en) * | 2012-03-27 | 2013-10-02 | Airbus Operations Gmbh | Flap assembly and aircraft with at least one flap assembly |
-
1953
- 1953-02-19 GB GB466853A patent/GB734959A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3140066A (en) * | 1962-12-04 | 1964-07-07 | North American Aviation Inc | Multiple pivot mounting means |
| US4531417A (en) * | 1980-09-29 | 1985-07-30 | Hollman Nils David | Hinge-type angle setting device |
| DE102012006187A1 (en) * | 2012-03-27 | 2013-10-02 | Airbus Operations Gmbh | Flap assembly and aircraft with at least one flap assembly |
| US9315256B2 (en) | 2012-03-27 | 2016-04-19 | Airbus Operations Gmbh | Flap arrangement and aircraft with at least one flap arrangement |
| DE102012006187B4 (en) * | 2012-03-27 | 2020-03-12 | Airbus Operations Gmbh | Flap arrangement and aircraft with at least one flap arrangement |
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