BR9702390A - Sistema para comando de um compensador de aeronave - Google Patents
Sistema para comando de um compensador de aeronaveInfo
- Publication number
- BR9702390A BR9702390A BR9702390A BR9702390A BR9702390A BR 9702390 A BR9702390 A BR 9702390A BR 9702390 A BR9702390 A BR 9702390A BR 9702390 A BR9702390 A BR 9702390A BR 9702390 A BR9702390 A BR 9702390A
- Authority
- BR
- Brazil
- Prior art keywords
- compensator
- aircraft
- controlling
- aircraft compensator
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/10—Adjustable control surfaces or members, e.g. rudders one surface adjusted by movement of another, e.g. servo tabs
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Mechanical Control Devices (AREA)
- Transmission Devices (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9606144A FR2748720B1 (fr) | 1996-05-17 | 1996-05-17 | Systeme pour la commande d'un volet compensateur de gouverne d'aeronef |
Publications (1)
Publication Number | Publication Date |
---|---|
BR9702390A true BR9702390A (pt) | 1998-09-01 |
Family
ID=9492219
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR9702390A BR9702390A (pt) | 1996-05-17 | 1997-05-19 | Sistema para comando de um compensador de aeronave |
Country Status (9)
Country | Link |
---|---|
US (1) | US5913492A (pt) |
EP (1) | EP0807573B1 (pt) |
CN (1) | CN1080226C (pt) |
BR (1) | BR9702390A (pt) |
CA (1) | CA2204445C (pt) |
DE (1) | DE69707196T2 (pt) |
ES (1) | ES2165001T3 (pt) |
FR (1) | FR2748720B1 (pt) |
ID (1) | ID16899A (pt) |
Families Citing this family (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE508672C2 (sv) * | 1997-12-30 | 1998-10-26 | Saab Ab | Anordning och metod för styrkraftreglering vid ett mekaniskt styrsystem för ett flygplan |
US6257528B1 (en) * | 1999-07-20 | 2001-07-10 | The Boeing Company | Vehicle control system and method employing control surface and geared tab |
GB9918289D0 (en) | 1999-08-03 | 2000-05-24 | British Aerospace | Actuator system for aerospace controls and functions |
US7424988B2 (en) * | 2001-05-24 | 2008-09-16 | Mcdonnell Helicopter Company Llc | Use of aerodynamic forces to assist in the control and positioning of aircraft control surfaces and variable geometry systems |
US6672540B1 (en) | 2002-12-03 | 2004-01-06 | Rockwell Collins, Inc. | Actuator for aircraft stabilizers with a failure responsive lock control mechanism |
US7182297B2 (en) * | 2003-01-17 | 2007-02-27 | The Insitu Group, Inc. | Method and apparatus for supporting aircraft components, including actuators |
US6827311B2 (en) * | 2003-04-07 | 2004-12-07 | Honeywell International, Inc. | Flight control actuation system |
US7770842B2 (en) * | 2004-08-24 | 2010-08-10 | Honeywell International Inc. | Aircraft flight control surface actuation system communication architecture |
US7549605B2 (en) * | 2005-06-27 | 2009-06-23 | Honeywell International Inc. | Electric flight control surface actuation system for aircraft flaps and slats |
US20070007385A1 (en) * | 2005-06-27 | 2007-01-11 | Honeywell International, Inc. | Electric flight control surface actuation system electronic architecture |
US7622818B2 (en) * | 2005-12-19 | 2009-11-24 | Vertical Power, Inc. | Backup electrical power system for solid-state aircraft power distribution systems |
US20070142980A1 (en) * | 2005-12-19 | 2007-06-21 | Marc Ausman | Avionics method and apparatus |
US8340842B2 (en) | 2005-12-19 | 2012-12-25 | Vertical Power, Inc. | Aircraft emergency handling |
US8346409B2 (en) | 2005-12-19 | 2013-01-01 | Vertical Power, Inc. | Variable speed flap retraction and notification |
US8103393B2 (en) * | 2005-12-19 | 2012-01-24 | Vertical Power, Inc. | Aircraft exhaust gas temperature monitor |
US20080237402A1 (en) * | 2005-12-19 | 2008-10-02 | Marc Ausman | Aircraft trim safety system and backup controls |
US7796054B2 (en) * | 2005-12-19 | 2010-09-14 | Vertical Power, Inc. | Aircraft electrical system evaluation |
US7883059B2 (en) * | 2007-05-17 | 2011-02-08 | Insitu, Inc. | Actuator systems and associated methods for unmanned air vehicles and other applications |
US8876063B2 (en) * | 2007-12-10 | 2014-11-04 | The Boeing Company | Flight control using multiple actuators on primary control surfaces with tabs |
FR2927308B1 (fr) * | 2008-02-08 | 2010-10-22 | Airbus France | Systeme distribue de commande de vol. |
US7973533B2 (en) | 2008-02-27 | 2011-07-05 | Vertical Power, Inc. | In-circuit testing for integrity of solid-state switches |
DE102008022092A1 (de) * | 2008-05-05 | 2009-11-19 | Airbus Deutschland Gmbh | Fehlertolerantes Stellsystem zur Verstellung von Klappen eines Flugzeugs mit einer Verstell-Kinematik mit feststehender Drehachse |
DE102008034444B4 (de) * | 2008-05-14 | 2013-09-05 | Diehl Aerospace Gmbh | Eingabesystem für eine Landeklappensteuerung eines Flugzeugs |
US8235327B2 (en) * | 2009-03-18 | 2012-08-07 | Insitu, Inc. | Adjustable servomechanism assemblies and associated systems and methods |
DE102009002435A1 (de) * | 2009-04-16 | 2010-10-21 | Airbus Deutschland Gmbh | Hochauftriebssystem für ein Flugzeug und Verfahren zum Detektieren von Fehlern in einem Hochauftriebssystem für ein Flugzeug |
CN107992033A (zh) * | 2012-02-10 | 2018-05-04 | 默林科技股份有限公司 | 自动驾驶仪及其方法 |
CN103043209B (zh) * | 2012-12-11 | 2016-04-20 | 江西洪都航空工业集团有限责任公司 | 一种农林飞机升降舵配平机构 |
US9180961B2 (en) * | 2013-01-28 | 2015-11-10 | The Boeing Company | Control surface for creating variable camber along a wing |
EP2805879B1 (en) * | 2013-05-22 | 2017-07-05 | Airbus Operations GmbH | Flap arrangement for a wing of an aircraft and an aircraft with a wing comprising such a flap arrangement |
CN104648657A (zh) * | 2013-11-22 | 2015-05-27 | 中国航空工业集团公司西安飞机设计研究所 | 一种可抑制振动的带调整片操纵面 |
CN103761899B (zh) * | 2013-12-31 | 2017-01-11 | 中国人民解放军空军航空大学军事仿真技术研究所 | 飞行模拟器可逆式操纵负荷系统力感仿真方法 |
CN106184713B (zh) * | 2015-04-29 | 2018-07-24 | 陕西飞机工业(集团)有限公司 | 一种飞机升降舵调整片自动配平方法 |
CN106184715B (zh) * | 2015-04-29 | 2018-07-24 | 陕西飞机工业(集团)有限公司 | 一种飞机驾驶杆配平系统 |
CN109070996A (zh) * | 2016-04-25 | 2018-12-21 | 庞巴迪公司 | 具有电传动升降舵的飞行器俯仰控制系统 |
CN109747813B (zh) * | 2017-11-07 | 2021-09-28 | 中国科学院沈阳自动化研究所 | 一种大载荷无人机尾翼驱动系统 |
CN110450940B (zh) * | 2019-06-24 | 2022-09-20 | 陕西飞机工业(集团)有限公司 | 一种飞机的升降舵配平控制电路 |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2383779A (en) * | 1942-05-14 | 1945-08-28 | Bell Aircraft Corp | Aircraft control means |
US2563757A (en) * | 1945-07-23 | 1951-08-07 | Lockheed Aircraft Corp | All-movable horizontal tail |
US2568719A (en) * | 1947-04-09 | 1951-09-25 | Sperry Corp | Control system for aircraft control surface and tab |
US2577439A (en) * | 1947-10-18 | 1951-12-04 | Curtiss Wright Corp | Differential spring balance tab |
US2640665A (en) * | 1948-06-02 | 1953-06-02 | Cons Vultee Aircraft Corp | Aircraft trim tab control |
FR1015687A (fr) * | 1949-03-04 | 1952-10-17 | A V Roe Canada Ltd | Dispositif de commande d'aéronefs en vol |
US2557426A (en) * | 1950-01-13 | 1951-06-19 | Lockheed Aircraft Corp | Tab actuating mechanism |
US2719684A (en) * | 1951-09-04 | 1955-10-04 | North American Aviation Inc | Aircraft control |
US2817483A (en) * | 1951-10-17 | 1957-12-24 | Glenn L Martin Co | Aircraft control force modifier |
US2721716A (en) * | 1952-03-31 | 1955-10-25 | Beadle John Charles William | Collapsible parachute |
US3149272A (en) * | 1962-04-10 | 1964-09-15 | Sperry Rand Corp | Discriminating safety monitor for servo systems |
US4595458A (en) * | 1985-05-17 | 1986-06-17 | Olin Corporation | Process for using selected fatty acid adducts of a 1,2,4-triazole as sizing or waterproofing agents for cellulosic materials |
FR2600035B1 (fr) * | 1986-06-16 | 1988-10-21 | Aerospatiale | Systeme pour la commande d'une surface aerodynamique mobile d'un aeronef. |
-
1996
- 1996-05-17 FR FR9606144A patent/FR2748720B1/fr not_active Expired - Fee Related
-
1997
- 1997-04-30 EP EP97400980A patent/EP0807573B1/fr not_active Expired - Lifetime
- 1997-04-30 DE DE69707196T patent/DE69707196T2/de not_active Expired - Lifetime
- 1997-04-30 ES ES97400980T patent/ES2165001T3/es not_active Expired - Lifetime
- 1997-05-05 CA CA002204445A patent/CA2204445C/fr not_active Expired - Fee Related
- 1997-05-12 ID IDP971579A patent/ID16899A/id unknown
- 1997-05-13 US US08/855,190 patent/US5913492A/en not_active Expired - Fee Related
- 1997-05-17 CN CN97113518A patent/CN1080226C/zh not_active Expired - Fee Related
- 1997-05-19 BR BR9702390A patent/BR9702390A/pt not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
DE69707196D1 (de) | 2001-11-15 |
US5913492A (en) | 1999-06-22 |
FR2748720B1 (fr) | 1998-07-24 |
FR2748720A1 (fr) | 1997-11-21 |
DE69707196T2 (de) | 2002-05-29 |
ID16899A (id) | 1997-11-20 |
ES2165001T3 (es) | 2002-03-01 |
EP0807573B1 (fr) | 2001-10-10 |
CN1080226C (zh) | 2002-03-06 |
CN1176208A (zh) | 1998-03-18 |
CA2204445C (fr) | 2005-07-05 |
CA2204445A1 (fr) | 1997-11-17 |
EP0807573A1 (fr) | 1997-11-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FB34 | Technical and formal requirements: requirement - article 34 of industrial property law | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] | ||
B24H | Lapse because of non-payment of annual fees (definitively: art 78 iv lpi) | ||
B24F | Patent annual fee: publication cancelled |
Free format text: ANULADA A PUBLICACAO CODIGO 24.8 NA RPI NO 2258 DE 15/04/2014 POR TER SIDO INDEVIDA. |
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B21F | Lapse acc. art. 78, item iv - on non-payment of the annual fees in time |
Free format text: REFERENTE AS 14A, 15A, 16A, 17A, 18A, 19A E 20A ANUIDADES. |
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B24J | Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12) |
Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2607 DE 22-12-2020 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |