ATE495101T1 - Verfahren und vorrichtung zur anzeige des betriebszustandes eines flugzeugtriebwerkes - Google Patents
Verfahren und vorrichtung zur anzeige des betriebszustandes eines flugzeugtriebwerkesInfo
- Publication number
- ATE495101T1 ATE495101T1 AT07076060T AT07076060T ATE495101T1 AT E495101 T1 ATE495101 T1 AT E495101T1 AT 07076060 T AT07076060 T AT 07076060T AT 07076060 T AT07076060 T AT 07076060T AT E495101 T1 ATE495101 T1 AT E495101T1
- Authority
- AT
- Austria
- Prior art keywords
- speed
- aircraft engine
- target idle
- idle running
- indicating
- Prior art date
Links
- 230000000007 visual effect Effects 0.000 abstract 2
- 230000003247 decreasing effect Effects 0.000 abstract 1
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
- B64D43/00—Arrangements or adaptations of instruments
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
- Instrument Panels (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/635,418 US7679529B2 (en) | 2006-12-07 | 2006-12-07 | Method and apparatus for indicating operational state of aircraft engine |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE495101T1 true ATE495101T1 (de) | 2011-01-15 |
Family
ID=39273808
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT07076060T ATE495101T1 (de) | 2006-12-07 | 2007-12-07 | Verfahren und vorrichtung zur anzeige des betriebszustandes eines flugzeugtriebwerkes |
Country Status (5)
Country | Link |
---|---|
US (1) | US7679529B2 (de) |
EP (1) | EP1930239B1 (de) |
AT (1) | ATE495101T1 (de) |
DE (1) | DE602007011877D1 (de) |
ES (1) | ES2359518T3 (de) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20100162027A1 (en) * | 2008-12-22 | 2010-06-24 | Honeywell International Inc. | Health capability determination system and method |
US20110029804A1 (en) * | 2008-12-22 | 2011-02-03 | Honeywell International Inc. | Fleet mission management system and method using health capability determination |
US8779945B2 (en) * | 2010-03-17 | 2014-07-15 | Sikorsky Aircraft Corporation | Virtual ice accretion meter display |
US9046891B2 (en) | 2010-10-22 | 2015-06-02 | Honeywell International Inc. | Control effector health capabilities determination reasoning system and method |
EP2635874B1 (de) * | 2010-12-22 | 2015-07-01 | Bell Helicopter Textron Inc. | Leistungssicherheitsinstrument |
US20180045163A1 (en) * | 2015-03-12 | 2018-02-15 | Sikorsky Aircraft Corporation | Conditional engine igniters |
CN108137160B (zh) | 2015-09-30 | 2021-10-01 | 庞巴迪公司 | 用于呈现飞机发动机的操作状态的方法和系统 |
US9950805B2 (en) * | 2015-10-26 | 2018-04-24 | The Boeing Company | Aircraft engine fan speed display improvements for enhanced monitoring and thrust setting ability |
US11225915B2 (en) | 2017-11-16 | 2022-01-18 | General Electric Company | Engine core speed reducing method and system |
US11378414B2 (en) * | 2018-02-27 | 2022-07-05 | Gulfstream Aerospace Corporation | Trend indications for avionics systems |
CN110411439B (zh) * | 2019-07-15 | 2021-07-09 | 北京控制工程研究所 | 一种根据星能量等级生成仿真星点的方法、装置及介质 |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3512128A (en) * | 1967-04-26 | 1970-05-12 | Firestone Tire & Rubber Co | Engine control warning system |
US4044709A (en) * | 1975-09-29 | 1977-08-30 | Pacer Systems, Inc. | Omnidirectional speed cockpit display |
US4060979A (en) * | 1975-11-19 | 1977-12-06 | United Technologies Corporation | Stall warning detector for gas turbine engine |
US4325123A (en) * | 1978-07-28 | 1982-04-13 | The Boeing Company | Economy performance data avionic system |
DE3315386A1 (de) | 1983-04-28 | 1984-10-31 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Anzeigegeraet zur bildlichen darstellung von messwerten |
US4750127A (en) * | 1985-10-31 | 1988-06-07 | The Boeing Company | Energy compensated target speed for aircraft descent |
US5353022A (en) * | 1987-08-06 | 1994-10-04 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Airplane takeoff and landing performance monitoring system |
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 |
US5404766A (en) * | 1992-10-01 | 1995-04-11 | Honeywell Inc. | Rotating round dial aircraft engine instruments |
US5422625A (en) * | 1993-04-16 | 1995-06-06 | Moriyama Kogyo Kabushiki Kaisha | Control system for engine speed meter |
US5668542A (en) * | 1995-07-03 | 1997-09-16 | The United States Of America As Represented By The Secretary Of The Air Force | Color cockpit display for aircraft systems |
US6112141A (en) * | 1997-10-15 | 2000-08-29 | Dassault Aviation | Apparatus and method for graphically oriented aircraft display and control |
US6085129A (en) * | 1997-11-14 | 2000-07-04 | Rockwell Collins, Inc. | Integrated vertical profile display |
US6118385A (en) * | 1998-09-09 | 2000-09-12 | Honeywell Inc. | Methods and apparatus for an improved control parameter value indicator |
US6188937B1 (en) * | 1998-09-30 | 2001-02-13 | Honeywell International Inc. | Methods and apparatus for annunciation of vehicle operational modes |
US6505594B1 (en) * | 1999-08-23 | 2003-01-14 | Toyota Jidosha Kabushiki Kaisha | Control apparatus for internal combustion engine and method of controlling internal combustion engine |
US6735505B2 (en) * | 2002-01-17 | 2004-05-11 | Cubic Defense Systems, Inc. | Aircraft flight and voice data recorder system and method |
US7088264B2 (en) * | 2002-03-14 | 2006-08-08 | Honeywell International Inc. | Flight safety system monitoring combinations of state values |
US7142131B2 (en) * | 2002-07-03 | 2006-11-28 | The Boeing Company | Method and apparatus for displaying aircraft engine characteristics |
EP1378446B1 (de) | 2002-07-03 | 2017-08-09 | The Boeing Company | Verfahren und Vorrichtung zum Anzeigen Flugzeugmotorparametern |
JP4087686B2 (ja) * | 2002-11-21 | 2008-05-21 | ヤマハマリン株式会社 | 船外機用エンジンの回転変動制御システム |
US7053796B1 (en) * | 2003-02-27 | 2006-05-30 | Rockwell Collins, Inc. | Multi-dimensional instruments for monitoring engine and system parameters |
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 |
FR2871437B1 (fr) * | 2004-06-15 | 2006-08-18 | Eurocopter France | Indicateur de pilotage permettant de predire l'evolution du regime de rotation du rotor principal d'un giravion |
US7414544B2 (en) * | 2005-01-28 | 2008-08-19 | Bell Helicopter Textron, Inc. | Power situation indicator |
-
2006
- 2006-12-07 US US11/635,418 patent/US7679529B2/en active Active
-
2007
- 2007-12-07 ES ES07076060T patent/ES2359518T3/es active Active
- 2007-12-07 AT AT07076060T patent/ATE495101T1/de not_active IP Right Cessation
- 2007-12-07 EP EP07076060A patent/EP1930239B1/de active Active
- 2007-12-07 DE DE602007011877T patent/DE602007011877D1/de active Active
Also Published As
Publication number | Publication date |
---|---|
EP1930239B1 (de) | 2011-01-12 |
DE602007011877D1 (de) | 2011-02-24 |
US7679529B2 (en) | 2010-03-16 |
ES2359518T3 (es) | 2011-05-24 |
US20080136677A1 (en) | 2008-06-12 |
EP1930239A1 (de) | 2008-06-11 |
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Legal Events
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RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |