DE69900471D1 - Integriertes feuer- und flugsteuerungssystem mit automatischer motordrehmomentbeschränkung - Google Patents
Integriertes feuer- und flugsteuerungssystem mit automatischer motordrehmomentbeschränkungInfo
- Publication number
- DE69900471D1 DE69900471D1 DE69900471T DE69900471T DE69900471D1 DE 69900471 D1 DE69900471 D1 DE 69900471D1 DE 69900471 T DE69900471 T DE 69900471T DE 69900471 T DE69900471 T DE 69900471T DE 69900471 D1 DE69900471 D1 DE 69900471D1
- Authority
- DE
- Germany
- Prior art keywords
- control system
- engine torque
- flight control
- automatic engine
- torque limitation
- 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
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
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Feedback Control In General (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/052,628 US6012676A (en) | 1998-03-31 | 1998-03-31 | Integrated fire and flight control system with automatic engine torque limiting |
PCT/US1999/005020 WO1999050729A1 (en) | 1998-03-31 | 1999-03-09 | Integrated fire and flight control system with automatic engine torque limiting |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69900471D1 true DE69900471D1 (de) | 2001-12-20 |
DE69900471T2 DE69900471T2 (de) | 2002-08-22 |
Family
ID=21978851
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69900471T Expired - Lifetime DE69900471T2 (de) | 1998-03-31 | 1999-03-09 | Integriertes feuer- und flugsteuerungssystem mit automatischer motordrehmomentbeschränkung |
Country Status (6)
Country | Link |
---|---|
US (1) | US6012676A (de) |
EP (1) | EP1068564B1 (de) |
JP (1) | JP2002509844A (de) |
CA (1) | CA2321586A1 (de) |
DE (1) | DE69900471T2 (de) |
WO (1) | WO1999050729A1 (de) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6879885B2 (en) * | 2001-11-16 | 2005-04-12 | Goodrich Pump & Engine Control Systems, Inc. | Rotor torque predictor |
US6648269B2 (en) * | 2001-12-10 | 2003-11-18 | Sikorsky Aircraft Corporation | Trim augmentation system for a rotary wing aircraft |
IL153291A (en) * | 2002-12-05 | 2010-05-31 | Nir Padan | System and method for situation assessment and dynamic guidance to aerial vehicles for the optimal conduct of close-in maneuvering air combat |
US7970498B2 (en) * | 2007-06-01 | 2011-06-28 | Sikorsky Aircraft Corporation | Model based sensor system for loads aware control laws |
US8271151B2 (en) | 2008-03-31 | 2012-09-18 | Sikorsky Aircraft Corporation | Flight control system for rotary wing aircraft |
EP2329203A2 (de) * | 2008-10-02 | 2011-06-08 | Carrier Corporation | Kühlsystem mit adaptiver heissgasneuerhitzung |
EP2296064B1 (de) * | 2009-09-10 | 2019-04-24 | Sikorsky Aircraft Corporation | Leben verbesserndes Flugsteuerungssystem |
US8265815B2 (en) * | 2009-11-25 | 2012-09-11 | GM Global Technology Operations LLC | Method for controlling output torque in powertrains |
US8777803B2 (en) | 2011-05-25 | 2014-07-15 | GM Global Technology Operations LLC | Method of prioritizing output torque and off-going clutch torque constraints during a torque phase |
RU2486108C1 (ru) * | 2011-11-18 | 2013-06-27 | Открытое Акционерное Общество "Московский Вертолётный Завод Им. М.Л. Миля" | Система контроля оборотов несущего винта вертолета |
US9051055B2 (en) * | 2013-03-07 | 2015-06-09 | Bell Helicopter Textron Inc. | System and method of adaptively governing rotor speed for optimal performance |
US9856017B2 (en) | 2013-06-11 | 2018-01-02 | Bell Helicopter Textron Inc. | Torque based method of limiting vertical axis augmentation |
US10508887B2 (en) * | 2016-06-02 | 2019-12-17 | Sikorsky Aircraft Corporation | Attitude-coupled targeting system for rotary wing aircraft |
US10633104B2 (en) | 2017-05-17 | 2020-04-28 | General Electric Company | Hybrid-electric propulsion system for an aircraft |
US10800536B2 (en) | 2017-06-09 | 2020-10-13 | General Electric Company | Propulsion system for an aircraft |
US10006375B1 (en) | 2017-07-11 | 2018-06-26 | General Electric Company | Propulsion system for an aircraft |
US10479491B2 (en) * | 2017-08-17 | 2019-11-19 | Textron Innovations Inc. | System and method for rotorcraft collective power hold |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BR8701672A (pt) * | 1986-08-04 | 1988-01-05 | United Technologies Corp | Processo para detectar uma folha de motor em uma aeronave de motor multiplo |
US4998202A (en) * | 1989-05-19 | 1991-03-05 | United Technologies Corporation | Helicopter, high rotor load speed enhancement |
US5178307A (en) * | 1991-08-28 | 1993-01-12 | United Technologies Corporation | High speed yaw control system for rotary wing aircraft |
US5238203A (en) * | 1991-08-28 | 1993-08-24 | United Technologies Corporation | High speed turn coordination for rotary wing aircraft |
ES2099832T3 (es) * | 1991-08-28 | 1997-06-01 | United Technologies Corp | Sistema de control vertical para helicoptero. |
US5331881A (en) * | 1992-05-19 | 1994-07-26 | United Technologies Corporation | Helicopter integrated fire and flight control having azimuth and pitch control |
US5263662A (en) * | 1992-05-19 | 1993-11-23 | United Technologies Corporation | Helicopter integrated fire and flight control system having turn coordination control |
US5310136A (en) * | 1992-05-19 | 1994-05-10 | United Technologies Corporation | Helicopter integrated fire and flight control having constraint limiting control |
US5310135A (en) * | 1992-10-28 | 1994-05-10 | United Technologies Corporation | Helicopter integrated fire and flight control having coordinated area bombing control |
US5465212A (en) * | 1993-12-23 | 1995-11-07 | United Technologies Corporation | Helicopter integrated fire and flight control having a pre-launch and post-launch maneuver director |
US5850615A (en) * | 1995-12-06 | 1998-12-15 | Mcdonnell Douglas Helicopter Co. | Rotor blade swashplate-axis rotation and gyroscopic moments componsator |
-
1998
- 1998-03-31 US US09/052,628 patent/US6012676A/en not_active Expired - Lifetime
-
1999
- 1999-03-09 DE DE69900471T patent/DE69900471T2/de not_active Expired - Lifetime
- 1999-03-09 EP EP99914890A patent/EP1068564B1/de not_active Expired - Lifetime
- 1999-03-09 JP JP2000541574A patent/JP2002509844A/ja active Pending
- 1999-03-09 WO PCT/US1999/005020 patent/WO1999050729A1/en active IP Right Grant
- 1999-03-09 CA CA002321586A patent/CA2321586A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
WO1999050729A1 (en) | 1999-10-07 |
JP2002509844A (ja) | 2002-04-02 |
EP1068564A1 (de) | 2001-01-17 |
EP1068564B1 (de) | 2001-11-14 |
DE69900471T2 (de) | 2002-08-22 |
CA2321586A1 (en) | 1999-10-07 |
US6012676A (en) | 2000-01-11 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |