ES2017738B3 - Sistema de mando de vuelo electrico con proteccion en incidencia para aeronave. - Google Patents

Sistema de mando de vuelo electrico con proteccion en incidencia para aeronave.

Info

Publication number: ES2017738B3
Authority: ES; Spain
Prior art keywords: aircraft; control system; flight control; electric flight; incidence protection
Prior art date: 1986-09-15
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 - Lifetime

Application number

ES87401976T

Other languages

English (en)

Inventor

Pierre Fabre

Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

Airbus Group SAS

Aerospatiale Matra

Original Assignee

Airbus Group SAS

Aerospatiale Matra

Priority date (The priority date 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 date listed.)

1986-09-15

Filing date

1987-09-03

Publication date

1991-03-01

1987-09-03 Application filed by Airbus Group SAS, Aerospatiale Matra filed Critical Airbus Group SAS

1991-03-01 Application granted granted Critical

1991-03-01 Publication of ES2017738B3 publication Critical patent/ES2017738B3/es

2007-09-03 Anticipated expiration legal-status Critical

Status Expired - Lifetime legal-status Critical Current

Links

RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 title 1

Classifications

- 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
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
- 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
- B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors

Landscapes

Engineering & Computer Science (AREA)
Automation & Control Theory (AREA)
Aviation & Aerospace Engineering (AREA)
Radar, Positioning & Navigation (AREA)
Remote Sensing (AREA)
Physics & Mathematics (AREA)
General Physics & Mathematics (AREA)
Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Radar Systems Or Details Thereof (AREA)

ES87401976T 1986-09-15 1987-09-03 Sistema de mando de vuelo electrico con proteccion en incidencia para aeronave. Expired - Lifetime ES2017738B3 (es)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
FR8612855A FR2604001B1 (fr)	1986-09-15	1986-09-15	Systeme de commande de vol electrique avec protection en incidence pour aeronef

Publications (1)

Publication Number	Publication Date
ES2017738B3 true ES2017738B3 (es)	1991-03-01

Family

ID=9338935

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
ES87401976T Expired - Lifetime ES2017738B3 (es)	1986-09-15	1987-09-03	Sistema de mando de vuelo electrico con proteccion en incidencia para aeronave.

Country Status (6)

Country	Link
US (1)	US4829220A (es)
EP (1)	EP0261015B1 (es)
CA (1)	CA1270563A (es)
DE (1)	DE3764336D1 (es)
ES (1)	ES2017738B3 (es)
FR (1)	FR2604001B1 (es)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
JPH01185709A (ja) *	1988-01-20	1989-07-25	Teijin Seiki Co Ltd	故障検出機構付きサーボ回路
FR2661149B1 (fr) *	1990-04-24	1992-08-14	Aerospatiale	Systeme pour le pilotage d'un avion en tangage.
FR2711257B1 (fr) *	1993-10-14	1995-12-22	Aerospatiale	Système de commande de vol électrique pour avion avec protection en assiette au décollage.
US5746392A (en) †	1995-05-15	1998-05-05	The Boeing Company	Autopilot/flight director underspeed protection system
US5803408A (en) *	1995-05-15	1998-09-08	The Boeing Company	Autopilot/flight director stall protection system
FR2826469B1 (fr)	2001-06-25	2003-10-24	Eads Airbus Sa	Procede et dispositif pour commander au moins une surface aerodynamique de profondeur d'un avion lors d'un decollage
FR2866627B1 (fr) *	2004-02-24	2006-05-05	Airbus France	Procede et dispositif pour l'optimisation du braquage des volets deporteurs d'un aeronef en vol
DE102004045732A1 (de) *	2004-09-21	2006-03-30	Airbus Deutschland Gmbh	Flugzeug mit Flügeln, deren maximaler Auftrieb durch steuerbare Flügelkomponenten veränderbar ist
FR2885706B1 (fr) *	2005-05-10	2007-06-15	Airbus France Sas	Procede d'aide au decollage d'un aeronef.
CN102219051B (zh) *	2011-04-29	2013-01-09	北京工业大学	基于人机交互技术的四旋翼飞行器系统控制方法
ES2543633T3 (es) *	2011-07-28	2015-08-20	Airbus Defence and Space GmbH	Método y aparato para minimizar las cargas estructurales dinámicas de un avión
US9845146B2 (en) *	2015-10-23	2017-12-19	The Boeing Company	Zoom climb prevention system for enhanced performance
DE102016117638B4 (de) *	2016-09-19	2018-05-24	Deutsches Zentrum für Luft- und Raumfahrt e.V.	Verminderung von an einem Luftfahrzeug auftretenden Böenlasten
US11841713B2 (en) *	2020-01-07	2023-12-12	Gulfstream Aerospace Corporation	Controllers and aircraft with takeoff stall protection system

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3393380A (en) *	1966-03-15	1968-07-16	James E. Webb	Phase locked phase modulator including a voltage controlled oscillator
CH601874A5 (es) *	1976-07-07	1978-07-14	Bbc Brown Boveri & Cie
US4052672A (en) *	1976-07-22	1977-10-04	Motorola, Inc.	Extended phase-range, high fidelity modulator arrangement
US4110707A (en) *	1976-12-13	1978-08-29	Texas Instruments Incorporated	Indirect FM modulation scheme using phase locked loop
DE2807902C2 (de) *	1978-02-24	1980-04-30	Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen	Steuereinrichtung mit aktiver Kraft rückführung
US4304375A (en) *	1979-05-17	1981-12-08	Textron Inc.	Electrically controlled elevator
CA1158219A (en) *	1980-04-01	1983-12-06	Edmond D. Diamond	Multi-axis force stick, self-trimmed aircraft flight control system
WO1984001345A1 (en) *	1982-09-30	1984-04-12	Boeing Co	Total energy based flight control system
US4500857A (en) *	1983-02-24	1985-02-19	The United States Of America As Represented By The Secretary Of The Army	Frequency modulated phase locked loop
EP0152714B1 (fr) *	1984-01-09	1987-04-01	AEROSPATIALE Société Nationale Industrielle	Système de commandes de vol pour aéronef

1986
- 1986-09-15 FR FR8612855A patent/FR2604001B1/fr not_active Expired
1987
- 1987-09-03 DE DE8787401976T patent/DE3764336D1/de not_active Expired - Lifetime
- 1987-09-03 ES ES87401976T patent/ES2017738B3/es not_active Expired - Lifetime
- 1987-09-03 EP EP87401976A patent/EP0261015B1/fr not_active Expired - Lifetime
- 1987-09-15 US US07/096,481 patent/US4829220A/en not_active Expired - Lifetime
- 1987-09-15 CA CA000546947A patent/CA1270563A/fr not_active Expired - Lifetime

Also Published As

Publication number	Publication date
FR2604001B1 (fr)	1988-12-09
DE3764336D1 (de)	1990-09-20
CA1270563A (fr)	1990-06-19
EP0261015A1 (fr)	1988-03-23
EP0261015B1 (fr)	1990-08-16
FR2604001A1 (fr)	1988-03-18
US4829220A (en)	1989-05-09

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