DE69602927T2 - Vorrichtung zur steuerungshilfe - Google Patents

Vorrichtung zur steuerungshilfe

Info

Publication number
DE69602927T2
DE69602927T2 DE69602927T DE69602927T DE69602927T2 DE 69602927 T2 DE69602927 T2 DE 69602927T2 DE 69602927 T DE69602927 T DE 69602927T DE 69602927 T DE69602927 T DE 69602927T DE 69602927 T2 DE69602927 T2 DE 69602927T2
Authority
DE
Germany
Prior art keywords
aircraft
propulsion system
flight
instantaneous value
power
Prior art date
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
DE69602927T
Other languages
English (en)
Other versions
DE69602927D1 (de
Inventor
Patrick Pelletier
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 Helicopters SAS
Original Assignee
Individual
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.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Application granted granted Critical
Publication of DE69602927D1 publication Critical patent/DE69602927D1/de
Publication of DE69602927T2 publication Critical patent/DE69602927T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00Arrangements or adaptations of instruments

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Control Of Turbines (AREA)
  • Massaging Devices (AREA)
  • Lifting Devices For Agricultural Implements (AREA)
  • Medicines Containing Plant Substances (AREA)
  • Traffic Control Systems (AREA)
  • Jib Cranes (AREA)
  • Revetment (AREA)
DE69602927T 1995-02-23 1996-02-22 Vorrichtung zur steuerungshilfe Expired - Lifetime DE69602927T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9502091A FR2731069B1 (fr) 1995-02-23 1995-02-23 Dispositif d'aide au pilotage
PCT/FR1996/000284 WO1996026472A1 (fr) 1995-02-23 1996-02-22 Dispositif d'aide au pilotage

Publications (2)

Publication Number Publication Date
DE69602927D1 DE69602927D1 (de) 1999-07-22
DE69602927T2 true DE69602927T2 (de) 1999-12-16

Family

ID=9476432

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69602927T Expired - Lifetime DE69602927T2 (de) 1995-02-23 1996-02-22 Vorrichtung zur steuerungshilfe

Country Status (6)

Country Link
EP (1) EP0811183B1 (de)
AT (1) ATE181430T1 (de)
DE (1) DE69602927T2 (de)
ES (1) ES2135873T3 (de)
FR (1) FR2731069B1 (de)
WO (1) WO1996026472A1 (de)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2749546B1 (fr) * 1996-06-07 1998-08-07 Eurocopter France Indicateur de pilotage pour aeronef
FR2756256B1 (fr) * 1996-11-26 1999-01-22 Eurocopter France Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere
FR2772718B1 (fr) * 1997-12-22 2000-02-11 Eurocopter France Indicateur de pilotage pour aeronef
FR2778765B1 (fr) * 1998-05-18 2001-10-05 Eurocopter France Systeme de surveillance du fonctionnement d'un aeronef, notamment d'un helicoptere
FR2809082B1 (fr) * 2000-05-17 2002-09-20 Eurocopter France Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere
FR2817831B1 (fr) 2000-12-13 2003-05-30 Eads Airbus Sa Indicateur de pilotage pour un aeronef, destine a fournir le rapport de pressions moteur
FR2871520B1 (fr) * 2004-06-15 2008-12-26 Eurocopter France Indicateur de pilotage permettant de predire l'evolution des parametres de surveillance d'un turbomoteur
US9272778B2 (en) 2009-06-04 2016-03-01 Airbus Helicopters Device for assisting in piloting hybrid helicopter, hybrid helicopter provided with such device, and method implemented by such device
FR2946322B1 (fr) * 2009-06-04 2011-06-17 Eurocopter France Dispositif d'aide au pilotage d'un helicoptere hybride, helicoptere hybride muni d'un tel dispositif et procede mis en oeuvre par ledit dispositif
FR2973340B1 (fr) 2011-03-30 2013-04-12 Eurocopter France Procede, dispositif d'aide au pilotage d'un aeronef, et aeronef
CN105425767B (zh) * 2015-11-04 2018-05-18 中国直升机设计研究所 一种维护设备自动识别不同待测机型的方法
US20200277080A1 (en) * 2019-02-28 2020-09-03 Beta Air Llc Systems and methods for in-flight operational assessment
US11964780B2 (en) 2019-02-28 2024-04-23 Beta Air, Llc Systems and methods for in-flight operational assessment
CN114476094B (zh) * 2021-12-31 2024-06-14 中国航空工业集团公司西安飞机设计研究所 一种倾转旋翼机关键动力参数超限保护方法

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3927307A (en) * 1974-03-01 1975-12-16 Textron Inc Power available indicator
US5050081A (en) * 1988-11-14 1991-09-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method and system for monitoring and displaying engine performance parameters
DE4125372C1 (en) * 1991-07-31 1992-08-13 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De Monitoring aircraft power unit esp. helicopter gas turbine drives - indicating only critical instantaneous parameters on display and warning of values outside set ranges

Also Published As

Publication number Publication date
EP0811183B1 (de) 1999-06-16
FR2731069B1 (fr) 1997-04-30
ES2135873T3 (es) 1999-11-01
WO1996026472A1 (fr) 1996-08-29
DE69602927D1 (de) 1999-07-22
EP0811183A1 (de) 1997-12-10
ATE181430T1 (de) 1999-07-15
FR2731069A1 (fr) 1996-08-30

Similar Documents

Publication Publication Date Title
DE69602927D1 (de) Vorrichtung zur steuerungshilfe
TW358918B (en) A system and method of including trap condition and rounding information in arithmetic processor instructions
DE3852059T2 (de) Verfahren zur Ausarbeitung eines statistischen Modells für die Bestimmung der Arbeitslast eines Flugzeugpiloten, daraus resultierendes Modell, Einrichtung zur Durchführung dieses Verfahrens und Anwendungen des Modells.
AP1773A (en) Airborne geophysical measurements.
WO2006136687A3 (fr) Procede et dispositif d'affichage pour un aeronef qui suit un plan de vol
ATE401551T1 (de) Vorrichtung zur darstellung von fluginformation in einem flugzeug
ATE411774T1 (de) Hautanalyse-gerät mit sprachausgabe
SE7702823L (sv) Antilasningsreglersystem
DE59401527D1 (de) Vorrichtung zur Abschwächung von Ansaugwirbeln an Turbinentriebwerken
Bukov et al. Optical surface pressure measurements: Accuracy and application field evaluation
DE69615113T2 (de) System mit einer vorrichtung und einem peripheriegerät für die vorrichtung und eine vorrichtung und ein peripheriegerät für ein solches system
GB1528581A (en) Position sensors for displays
ATE198510T1 (de) Einrichtung zur darstellung barometrischer luftdruckveränderungen mit intervallversorgung
JPS566022A (en) Engine controlling system
DE29607706U1 (de) Vorrichtung zur gleichzeitigen Messung von Schubkraft und Auftriebskraft an aerodynamischen Modellen
JPS57127808A (en) Azimuth and traveling distance finder
RU2209747C2 (ru) Пилотажный индикатор
SMART An evaluation of detail in dynamic visual displays[M. S. Thesis]
Okoemov et al. Applications of a quasi-stationary autopilot in a nonstationary aircraft-autopilot system
HUANG A PC-based measurement and test system for digital controller
DE29601834U1 (de) Vorrichtung zur Messung kleiner Kräfte und daraus abgeleiteter Größen durch Meßwertaufnahme mittels elektrischer Sensoren, z.B. Dehnungsmeßstreifen
Basile et al. Solid state device for the measurement of light aircraft roll attitude
Brummer An isentropic coordinate model used in a mesoscale data assimilation system.
WACKER Simulation system for development tasks in radar data processing
Kim Occurred Seasick Impression and Analysis of the Observer´ s Heart Rate Variability by using Ship´ s Bridge Simulator

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: EUROCOPTER, MARIGNANCE CEDEX, FR

8381 Inventor (new situation)

Inventor name: PELLETIER, PATRICK, BRETINGNY-SUR-ORGE, FR