RU2018143548A3 - - Google Patents
Download PDFInfo
- Publication number
- RU2018143548A3 RU2018143548A3 RU2018143548A RU2018143548A RU2018143548A3 RU 2018143548 A3 RU2018143548 A3 RU 2018143548A3 RU 2018143548 A RU2018143548 A RU 2018143548A RU 2018143548 A RU2018143548 A RU 2018143548A RU 2018143548 A3 RU2018143548 A3 RU 2018143548A3
- Authority
- RU
- Russia
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
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/12—Dual control apparatus
-
- 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
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/042—Initiating means actuated personally operated by hand
- B64C13/0423—Initiating means actuated personally operated by hand yokes or steering wheels for primary flight controls
-
- 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
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/044—Initiating means actuated personally operated by feet, e.g. pedals
-
- 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
- B64C13/24—Transmitting means
- B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
- B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
- B64C13/341—Transmitting means without power amplification or where power amplification is irrelevant mechanical having duplication or stand-by provisions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/04—Adjustable control surfaces or members, e.g. rudders with compound dependent movements
-
- 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
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/40—Transmitting means with power amplification using fluid pressure
- B64C13/42—Transmitting means with power amplification using fluid pressure having duplication or stand-by provisions
-
- 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
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
- B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Mechanical Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Transmission Devices (AREA)
- Toys (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US15/888,957 | 2018-02-05 | ||
| US15/888,957 US10793257B2 (en) | 2018-02-05 | 2018-02-05 | Flight control systems and methods for an aerial vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2018143548A RU2018143548A (ru) | 2020-06-10 |
| RU2018143548A3 true RU2018143548A3 (ru) | 2022-04-14 |
Family
ID=65279468
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2018143548A RU2018143548A (ru) | 2018-02-05 | 2018-12-10 | Системы и способы управления полетом для воздушного транспортного средства |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US10793257B2 (ru) |
| EP (1) | EP3521157B1 (ru) |
| JP (1) | JP7231393B2 (ru) |
| CN (1) | CN110116799A (ru) |
| BR (1) | BR102019002105A2 (ru) |
| CA (1) | CA3031120C (ru) |
| RU (1) | RU2018143548A (ru) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111976955B (zh) * | 2020-07-24 | 2023-03-14 | 中国航空工业集团公司西安飞行自动控制研究所 | 民机电传飞控双驾驶杆盘的单侧卡阻故障处理方法和装置 |
| US20220194561A1 (en) * | 2020-12-17 | 2022-06-23 | The Boeing Company | Systems and Methods for Overriding Autonomous Control of a Device |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2478173A (en) * | 1943-06-03 | 1949-08-09 | William E Austin | Safety device for aircraft controls |
| US3902379A (en) * | 1973-12-03 | 1975-09-02 | Us Navy | High load, quick-disconnect link |
| US3949958A (en) * | 1973-12-07 | 1976-04-13 | Lockheed Aircraft Corporation | Pitch control system |
| US4403756A (en) * | 1980-12-22 | 1983-09-13 | The Boeing Company | Bifurcated feel simulator for aircraft |
| US5782436A (en) * | 1996-01-19 | 1998-07-21 | Mcdonnell Douglas Corporation | Torque tube breakout mechanism |
| US20030183728A1 (en) | 2002-03-29 | 2003-10-02 | The Boeing Company | Aircraft control surface controller and associated method |
| JP4691121B2 (ja) | 2008-02-20 | 2011-06-01 | 三菱重工業株式会社 | 操縦システム、操縦桿リンク切り離し方法 |
| DE102009013758A1 (de) * | 2009-03-17 | 2010-09-23 | Airbus Deutschland Gmbh | Flugzeug mit einer Vorrichtung zur Beeinflussung der Richtungsstabilität des Flugzeugs sowie Verfahren zur Beeinflussung der Richtungsstabilität des Flugzeugs |
| US9764830B2 (en) * | 2012-02-10 | 2017-09-19 | Bell Helicopter Textron Inc. | Pilot control system with adjustable pedals |
| EP2695810B1 (en) * | 2012-08-09 | 2016-10-19 | Airbus Operations GmbH | Drive system for control surfaces of an aircraft |
| US9446838B2 (en) * | 2014-08-14 | 2016-09-20 | Gulfstream Aerospace Corporation | Systems for inceptor control in fly-by-wire aircraft systems |
| US9437056B2 (en) | 2014-10-09 | 2016-09-06 | The Boeing Company | Methods and apparatus for operating flight control systems of aircrafts |
| US10913527B2 (en) * | 2016-03-22 | 2021-02-09 | The Boeing Company | Method and apparatus for latent fault detection and management for fly-by-wire flight control systems |
-
2018
- 2018-02-05 US US15/888,957 patent/US10793257B2/en active Active
- 2018-12-10 RU RU2018143548A patent/RU2018143548A/ru unknown
- 2018-12-13 JP JP2018233403A patent/JP7231393B2/ja active Active
-
2019
- 2019-01-07 CN CN201910011022.0A patent/CN110116799A/zh active Pending
- 2019-01-23 CA CA3031120A patent/CA3031120C/en active Active
- 2019-02-01 BR BR102019002105-5A patent/BR102019002105A2/pt active Search and Examination
- 2019-02-04 EP EP19155328.8A patent/EP3521157B1/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| BR102019002105A2 (pt) | 2019-09-17 |
| EP3521157B1 (en) | 2022-09-28 |
| JP7231393B2 (ja) | 2023-03-01 |
| US10793257B2 (en) | 2020-10-06 |
| CA3031120C (en) | 2023-06-20 |
| CA3031120A1 (en) | 2019-08-05 |
| EP3521157A1 (en) | 2019-08-07 |
| CN110116799A (zh) | 2019-08-13 |
| US20190241253A1 (en) | 2019-08-08 |
| JP2019135141A (ja) | 2019-08-15 |
| RU2018143548A (ru) | 2020-06-10 |