BE652675A - - Google Patents
Info
- Publication number
- BE652675A BE652675A BE652675DA BE652675A BE 652675 A BE652675 A BE 652675A BE 652675D A BE652675D A BE 652675DA BE 652675 A BE652675 A BE 652675A
- Authority
- BE
- Belgium
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Control Devices (AREA)
- Transmission Devices (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US340612A US3243148A (en) | 1964-01-28 | 1964-01-28 | Aircraft horizontal tail control mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE652675A true BE652675A (US20110009641A1-20110113-C00185.png) | 1964-12-31 |
Family
ID=23334172
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE652675D BE652675A (US20110009641A1-20110113-C00185.png) | 1964-01-28 | 1964-09-04 |
Country Status (4)
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102004047008A1 (de) * | 2004-09-28 | 2006-03-30 | Liebherr-Aerospace Lindenberg Gmbh | Vorrichtung zur Einstellung von Flugzeughöhenflossen |
| JP4125311B2 (ja) * | 2005-08-30 | 2008-07-30 | 株式会社東芝 | ロボットおよびマニピュレータ |
| JP5552340B2 (ja) * | 2010-03-15 | 2014-07-16 | ナブテスコ株式会社 | アクチュエータ及びリンクの製造方法、アクチュエータ及びリンクの設計方法、アクチュエータ及びリンク |
| EP3176080B1 (en) * | 2015-12-03 | 2019-10-16 | LORD Solutions France | Gear reducer for a cockpit control device of an aircraft, and control device comprising such a gear reducer |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2191842A (en) * | 1937-03-13 | 1940-02-27 | Back William Edward | Airplane and control apparatus therefor |
| US2275692A (en) * | 1940-04-02 | 1942-03-10 | Sims Edward | Airplane aileron |
| US2667315A (en) * | 1950-10-28 | 1954-01-26 | Armstrong Whitworth Co Eng | Balancing of aircraft control columns |
| US2685422A (en) * | 1951-12-27 | 1954-08-03 | Chance Vought Aircraft Inc | Variable stop mechanism for interrelated mechanical surface control systems for aircraft |
| US2940696A (en) * | 1955-04-27 | 1960-06-14 | Bendix Aviat Corp | Differential mixer |
| US2940697A (en) * | 1955-05-02 | 1960-06-14 | Bendix Aviat Corp | Control system |
| US2903205A (en) * | 1956-11-15 | 1959-09-08 | Otto J Borngesser | Electric "g" limiter for aircraft |
| US2985408A (en) * | 1959-06-10 | 1961-05-23 | Richard M Johnson | Control linkage for airfoils |
| US3119583A (en) * | 1960-01-15 | 1964-01-28 | English Electric Co Ltd | Linkage in aircraft power control systems |
| FR1328347A (fr) * | 1962-03-28 | 1963-05-31 | English Electric Co Ltd | Tringlerie pour commande de gouverne sur un avion |
| US3138354A (en) * | 1962-08-02 | 1964-06-23 | Boeing Co | Aileron control on variable sweep wing designs |
-
1964
- 1964-01-28 US US340612A patent/US3243148A/en not_active Expired - Lifetime
- 1964-07-09 DE DE19641556940 patent/DE1556940B1/de not_active Withdrawn
- 1964-08-31 NL NL646410132A patent/NL143866B/xx unknown
- 1964-09-04 BE BE652675D patent/BE652675A/xx unknown
Also Published As
| Publication number | Publication date |
|---|---|
| NL6410132A (US20110009641A1-20110113-C00185.png) | 1965-07-29 |
| US3243148A (en) | 1966-03-29 |
| DE1556940B1 (de) | 1970-06-18 |
| NL143866B (nl) | 1974-11-15 |
