JPS4840199A - - Google Patents
Info
- Publication number
- JPS4840199A JPS4840199A JP47095239A JP9523972A JPS4840199A JP S4840199 A JPS4840199 A JP S4840199A JP 47095239 A JP47095239 A JP 47095239A JP 9523972 A JP9523972 A JP 9523972A JP S4840199 A JPS4840199 A JP S4840199A
- Authority
- JP
- Japan
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
- B64D2045/001—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear for indicating symmetry of flaps deflection
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Multiple Motors (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Fluid-Pressure Circuits (AREA)
- Control Of Direct Current Motors (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB4435871A GB1400449A (en) | 1971-09-23 | 1971-09-23 | Actuating arrangements for aircraft control surfaces |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS4840199A true JPS4840199A (en) | 1973-06-13 |
| JPS5550840B2 JPS5550840B2 (en) | 1980-12-20 |
Family
ID=10432909
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9523972A Expired JPS5550840B2 (en) | 1971-09-23 | 1972-09-25 |
Country Status (5)
| Country | Link |
|---|---|
| JP (1) | JPS5550840B2 (en) |
| DE (1) | DE2246576C3 (en) |
| FR (1) | FR2157808B1 (en) |
| GB (1) | GB1400449A (en) |
| IT (1) | IT965443B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5539895A (en) * | 1978-09-12 | 1980-03-21 | Sundstrand Corp | Actuator device of aircraft steering wing surface |
| JP2009519158A (en) * | 2005-12-13 | 2009-05-14 | エアバス・ドイチュラント・ゲーエムベーハー | Method and apparatus for automatically reducing load on aircraft high lift surface system, landing flap system |
| JP4638444B2 (en) * | 2003-11-12 | 2011-02-23 | エアバス オペラツィオンス ゲゼルシャフト ミット ベシュレンクテル ハフツング | Load limiting method in drive system for aircraft high lift device |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3013774A1 (en) * | 1980-04-10 | 1981-10-15 | Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen | OPERATING ARRANGEMENT FOR FLAP VALVES |
| JPS6363234U (en) * | 1986-10-15 | 1988-04-26 | ||
| US10450055B2 (en) * | 2017-06-15 | 2019-10-22 | The Boeing Company | Methods and apparatus for a distributed aircraft actuation system |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2769603A (en) * | 1951-04-27 | 1956-11-06 | Sperry Rand Corp | Control system for aircraft surfaces |
-
1971
- 1971-09-23 GB GB4435871A patent/GB1400449A/en not_active Expired
-
1972
- 1972-09-21 IT IT52878/72A patent/IT965443B/en active
- 1972-09-22 FR FR7233723A patent/FR2157808B1/fr not_active Expired
- 1972-09-22 DE DE2246576A patent/DE2246576C3/en not_active Expired
- 1972-09-25 JP JP9523972A patent/JPS5550840B2/ja not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5539895A (en) * | 1978-09-12 | 1980-03-21 | Sundstrand Corp | Actuator device of aircraft steering wing surface |
| JPH0146359B2 (en) * | 1978-09-12 | 1989-10-06 | Sundstrand Corp | |
| JP4638444B2 (en) * | 2003-11-12 | 2011-02-23 | エアバス オペラツィオンス ゲゼルシャフト ミット ベシュレンクテル ハフツング | Load limiting method in drive system for aircraft high lift device |
| JP2009519158A (en) * | 2005-12-13 | 2009-05-14 | エアバス・ドイチュラント・ゲーエムベーハー | Method and apparatus for automatically reducing load on aircraft high lift surface system, landing flap system |
| US8256718B2 (en) | 2005-12-13 | 2012-09-04 | Airbus Operations Gmbh | Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| GB1400449A (en) | 1975-07-16 |
| DE2246576C3 (en) | 1980-03-13 |
| FR2157808B1 (en) | 1975-03-14 |
| IT965443B (en) | 1974-01-31 |
| JPS5550840B2 (en) | 1980-12-20 |
| DE2246576A1 (en) | 1973-03-29 |
| FR2157808A1 (en) | 1973-06-08 |
| DE2246576B2 (en) | 1979-07-05 |