DE69210193T2 - Methode und Vorrichtung zur Regelung des Schubes eines Flugzeuges während des Steigfluges - Google Patents
Methode und Vorrichtung zur Regelung des Schubes eines Flugzeuges während des SteigflugesInfo
- Publication number
- DE69210193T2 DE69210193T2 DE69210193T DE69210193T DE69210193T2 DE 69210193 T2 DE69210193 T2 DE 69210193T2 DE 69210193 T DE69210193 T DE 69210193T DE 69210193 T DE69210193 T DE 69210193T DE 69210193 T2 DE69210193 T2 DE 69210193T2
- Authority
- DE
- Germany
- Prior art keywords
- climb
- thrust
- controlling
- aircraft during
- aircraft
- 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 - Fee Related
Links
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- 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
- G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
- G05D1/0661—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/811,724 US5299765A (en) | 1991-12-23 | 1991-12-23 | Apparatus and methods for controlling aircraft thrust during a climb |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69210193D1 DE69210193D1 (de) | 1996-05-30 |
DE69210193T2 true DE69210193T2 (de) | 1996-09-05 |
Family
ID=25207376
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69210193T Expired - Fee Related DE69210193T2 (de) | 1991-12-23 | 1992-11-26 | Methode und Vorrichtung zur Regelung des Schubes eines Flugzeuges während des Steigfluges |
Country Status (3)
Country | Link |
---|---|
US (1) | US5299765A (de) |
EP (1) | EP0549014B1 (de) |
DE (1) | DE69210193T2 (de) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6691004B2 (en) * | 1995-07-31 | 2004-02-10 | Honeywell International, Inc. | Method for determining a currently obtainable climb gradient of an aircraft |
US6062513A (en) * | 1998-09-14 | 2000-05-16 | The Boeing Company | Total energy based flight control system |
US6885340B2 (en) * | 2000-02-29 | 2005-04-26 | Rannoch Corporation | Correlation of flight track data with other data sources |
US6633259B1 (en) * | 1999-03-05 | 2003-10-14 | Rannuch Corporation | Method and apparatus for improving utility of automatic dependent surveillance |
FR2854128B1 (fr) * | 2003-04-22 | 2006-04-07 | Airbus France | Indicateur de pilotage pour un aeronef, en particulier un avion de transport, destine a fournir la poussee engendree par au moins un moteur de l'aeronef |
US6880784B1 (en) * | 2003-05-08 | 2005-04-19 | Supersonic Aerospace International, Llc | Automatic takeoff thrust management system |
US6945500B2 (en) * | 2003-08-15 | 2005-09-20 | Skycorp, Inc. | Apparatus for a geosynchronous life extension spacecraft |
US6886786B1 (en) * | 2003-10-10 | 2005-05-03 | The Boeing Company | Engine thrust management—new design architecture |
GB0415618D0 (en) * | 2004-07-13 | 2004-08-18 | Rolls Royce Plc | Aircraft takeoff |
US20070260424A1 (en) * | 2006-05-05 | 2007-11-08 | Harold Brown | Methods and apparatus for estimating engine thrust |
US7788013B2 (en) * | 2006-07-03 | 2010-08-31 | Textron System Corporation | Techniques for remotely adjusting a portion of an airplane engine |
US7584028B2 (en) * | 2006-11-14 | 2009-09-01 | The Boeing Company | Methods and systems for implementing location based noise abatement procedures |
US8380371B2 (en) * | 2007-03-14 | 2013-02-19 | General Electric Company | Method of generating variable thrust cutback during aircraft departure |
US8670881B2 (en) * | 2007-03-14 | 2014-03-11 | General Electric Company | Flight management system for generating variable thrust cutback during aircraft departure |
US8131410B2 (en) * | 2007-06-15 | 2012-03-06 | The Boeing Company | Quiet climb crew interface |
US7861578B2 (en) * | 2008-07-29 | 2011-01-04 | General Electric Company | Methods and systems for estimating operating parameters of an engine |
FR2946017B1 (fr) * | 2009-05-29 | 2012-09-28 | Airbus France | Systeme pour la commande d'au moins un moteur d'aeronef et aeronef comportant un tel systeme de commande. |
FR2946016B1 (fr) * | 2009-05-29 | 2012-09-28 | Airbus France | Systeme pour la commande d'au moins un moteur d'aeronef et aeronef comportant un tel systeme de commande. |
EP3038921B1 (de) | 2013-08-28 | 2020-07-01 | United Technologies Corporation | Schubausgleich für flugzeug mit mehreren triebwerken |
US10112722B2 (en) | 2015-01-15 | 2018-10-30 | Unison Industries Llc | Power control for propeller-driven aircraft |
US10227933B2 (en) * | 2015-02-12 | 2019-03-12 | United Technologies Corporation | Aircraft power setting trims for life extension |
US9696724B1 (en) * | 2016-04-22 | 2017-07-04 | Rockwell Collins, Inc. | Takeoff automating system, device, and method |
US10399689B2 (en) | 2017-06-07 | 2019-09-03 | Ge Aviation Systems Llc | Optimizing aircraft control based on noise abatement volumes |
US10671092B2 (en) | 2017-10-20 | 2020-06-02 | The Boeing Company | Airplane climb thrust optimization |
US11216011B2 (en) | 2018-03-16 | 2022-01-04 | Embraer S.A. | Optimized trajectory to noise improvement with auto-takeoff |
US11391218B2 (en) * | 2019-03-22 | 2022-07-19 | Pratt & Whitney Canada Corp. | Method and system for setting power of an aircraft engine |
US11733712B2 (en) * | 2020-07-03 | 2023-08-22 | Honeywell International Inc. | Systems and methods for generating displays for noise abatement departure procedures |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3586268A (en) * | 1969-04-04 | 1971-06-22 | William W Melvin | Instrument flight system |
US3691356A (en) * | 1970-12-10 | 1972-09-12 | Sperry Rand Corp | Speed command and throttle control system for aircraft |
US3822047A (en) * | 1972-12-14 | 1974-07-02 | Collins Radio Co | Takeoff and go-around climb-out profile pitch command formulation for aircraft |
US3908934A (en) * | 1973-12-03 | 1975-09-30 | Sperry Rand Corp | Programmed gain control for aircraft throttle control system |
US4019702A (en) * | 1975-11-13 | 1977-04-26 | The Boeing Company | Method and apparatus for guiding a jet aircraft in a noise-abated post-takeoff climb |
US4471439A (en) * | 1982-09-20 | 1984-09-11 | The Boeing Company | Method and apparatus for aircraft pitch and thrust axes control |
US4589616A (en) * | 1984-01-24 | 1986-05-20 | Sperry Corporation | Cruise airspeed control of aircraft altitude capture |
US4662171A (en) * | 1986-03-31 | 1987-05-05 | The Boeing Company | Automatic thrust restoration system |
-
1991
- 1991-12-23 US US07/811,724 patent/US5299765A/en not_active Expired - Lifetime
-
1992
- 1992-11-26 EP EP92203661A patent/EP0549014B1/de not_active Expired - Lifetime
- 1992-11-26 DE DE69210193T patent/DE69210193T2/de not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP0549014B1 (de) | 1996-04-24 |
EP0549014A1 (de) | 1993-06-30 |
DE69210193D1 (de) | 1996-05-30 |
US5299765A (en) | 1994-04-05 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |