DE69007922D1 - Dynamische Kompensation des Beschleunigungsprogrammes. - Google Patents

Dynamische Kompensation des Beschleunigungsprogrammes.

Info

Publication number
DE69007922D1
DE69007922D1 DE90630159T DE69007922T DE69007922D1 DE 69007922 D1 DE69007922 D1 DE 69007922D1 DE 90630159 T DE90630159 T DE 90630159T DE 69007922 T DE69007922 T DE 69007922T DE 69007922 D1 DE69007922 D1 DE 69007922D1
Authority
DE
Germany
Prior art keywords
dynamic compensation
acceleration program
acceleration
program
compensation
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
Application number
DE90630159T
Other languages
English (en)
Other versions
DE69007922T2 (de
Inventor
Douglas A Parsons
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE69007922D1 publication Critical patent/DE69007922D1/de
Application granted granted Critical
Publication of DE69007922T2 publication Critical patent/DE69007922T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • G05D1/08—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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2200/00—Mathematical features
    • F05D2200/10—Basic functions
    • F05D2200/11—Sum
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/04—Purpose of the control system to control acceleration (u)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/04—Purpose of the control system to control acceleration (u)
    • F05D2270/042—Purpose of the control system to control acceleration (u) by keeping it below damagingly high values
DE69007922T 1989-09-20 1990-09-20 Dynamische Kompensation des Beschleunigungsprogrammes. Expired - Fee Related DE69007922T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/409,835 US5029441A (en) 1989-09-20 1989-09-20 Dynamic compensation to n-dot schedules

Publications (2)

Publication Number Publication Date
DE69007922D1 true DE69007922D1 (de) 1994-05-11
DE69007922T2 DE69007922T2 (de) 1994-07-21

Family

ID=23622169

Family Applications (2)

Application Number Title Priority Date Filing Date
DE69007922T Expired - Fee Related DE69007922T2 (de) 1989-09-20 1990-09-20 Dynamische Kompensation des Beschleunigungsprogrammes.
DE199090630159T Pending DE419402T1 (de) 1989-09-20 1990-09-20 Dynamische kompensation des beschleunigungsprogrammes.

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE199090630159T Pending DE419402T1 (de) 1989-09-20 1990-09-20 Dynamische kompensation des beschleunigungsprogrammes.

Country Status (3)

Country Link
US (1) US5029441A (de)
EP (1) EP0419402B1 (de)
DE (2) DE69007922T2 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5231823A (en) * 1991-08-22 1993-08-03 General Electric Company Supervisory control system
US5259188A (en) * 1992-08-24 1993-11-09 General Electric Company Method and system to increase stall margin
US5361579A (en) * 1993-06-01 1994-11-08 Sundstrand Corporation Turbojet fuel control system
FR2803051B1 (fr) * 1999-12-23 2002-05-03 Turbomeca Dispositif et procede de regulation de la puissance d'un groupe motopropulseur d'entrainement de rotor d'helicoptere
US6715277B2 (en) * 2001-11-16 2004-04-06 Goodrich Pump & Engine Control Systems, Inc. Fuel control system for gas turbine engines
US6786049B2 (en) 2002-05-22 2004-09-07 Hamilton Sundstrand Fuel supply control for a gas turbine including multiple solenoid valves
US8712653B2 (en) * 2006-06-20 2014-04-29 GM Global Technology Operations LLC Deceleration dependent shift control
US8494749B2 (en) 2010-10-14 2013-07-23 Hamilton Sundstrand Corporation Method of operating an electronic engine control (EEC) to compensate for speed changes
US8720201B2 (en) 2010-11-24 2014-05-13 Hamilton Sundstrand Corporation Method of monitoring an electronic engine control (EEC) to detect a loss of fuel screen open area
EP3351771B1 (de) 2017-01-20 2021-03-17 GE Avio S.r.l. Gasturbinenmotorbrennstoffsteuerungssystem und -verfahren
US11072434B2 (en) 2018-04-24 2021-07-27 Textron Innovations Inc. Method and system for controlling rotor speeds of rotor systems

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4188781A (en) * 1978-04-25 1980-02-19 General Electric Company Non-linear dual mode regulator circuit
GB2052805B (en) * 1979-06-29 1983-03-09 Smiths Industries Ltd Gas-turbine engine control
US4423593A (en) * 1982-04-16 1984-01-03 Chandler Evans Inc. Fuel control for controlling helicopter rotor/turbine acceleration
US4470118A (en) * 1982-04-19 1984-09-04 Chandler Evans Inc. Gas turbine engine fuel control
US4543782A (en) * 1982-05-21 1985-10-01 Lucas Industries Gas turbine engine fuel control systems
GB2121986B (en) * 1982-05-21 1986-01-15 Lucas Ind Plc Gas turbine engine fuel control systems

Also Published As

Publication number Publication date
EP0419402B1 (de) 1994-04-06
DE69007922T2 (de) 1994-07-21
DE419402T1 (de) 1991-07-25
EP0419402A1 (de) 1991-03-27
US5029441A (en) 1991-07-09

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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