ES2761648T3 - Sistema y método para controlar un campo de presión alrededor de un avión en vuelo - Google Patents

Sistema y método para controlar un campo de presión alrededor de un avión en vuelo Download PDF

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Publication number
ES2761648T3
ES2761648T3 ES15766673T ES15766673T ES2761648T3 ES 2761648 T3 ES2761648 T3 ES 2761648T3 ES 15766673 T ES15766673 T ES 15766673T ES 15766673 T ES15766673 T ES 15766673T ES 2761648 T3 ES2761648 T3 ES 2761648T3
Authority
ES
Spain
Prior art keywords
controller
pressure
aircraft
pressure field
instruction
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.)
Active
Application number
ES15766673T
Other languages
English (en)
Spanish (es)
Inventor
Timothy Conners
Michael Knight
Robert Cowart
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.)
Gulfstream Aerospace Corp
Original Assignee
Gulfstream Aerospace 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 Gulfstream Aerospace Corp filed Critical Gulfstream Aerospace Corp
Application granted granted Critical
Publication of ES2761648T3 publication Critical patent/ES2761648T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/04—Influencing air flow over aircraft surfaces, not otherwise provided for by generating shock waves
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C30/00—Supersonic type aircraft
    • 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
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02—Initiating means
    • B64D31/06—Initiating means actuated automatically
    • 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
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • 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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L19/00—Details of, or accessories for, apparatus for measuring steady or quasi-steady pressure of a fluent medium insofar as such details or accessories are not special to particular types of pressure gauges
    • G01L19/0061—Electrical connection means
    • G01L19/0084—Electrical connection means to the outside of the housing
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L19/00—Details of, or accessories for, apparatus for measuring steady or quasi-steady pressure of a fluent medium insofar as such details or accessories are not special to particular types of pressure gauges
    • G01L19/14—Housings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Automation & Control Theory (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Feedback Control In General (AREA)
  • Measuring Fluid Pressure (AREA)
  • Traffic Control Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
ES15766673T 2014-08-14 2015-02-26 Sistema y método para controlar un campo de presión alrededor de un avión en vuelo Active ES2761648T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/459,488 US9878778B2 (en) 2014-08-14 2014-08-14 System and method for controlling a pressure field around an aircraft in flight
PCT/US2015/017660 WO2016025029A1 (en) 2014-08-14 2015-02-26 System and method for controlling a pressure field around an aircraft in flight

Publications (1)

Publication Number Publication Date
ES2761648T3 true ES2761648T3 (es) 2020-05-20

Family

ID=54148608

Family Applications (1)

Application Number Title Priority Date Filing Date
ES15766673T Active ES2761648T3 (es) 2014-08-14 2015-02-26 Sistema y método para controlar un campo de presión alrededor de un avión en vuelo

Country Status (6)

Country Link
US (1) US9878778B2 (enExample)
EP (1) EP3180244B1 (enExample)
JP (1) JP6590419B2 (enExample)
CN (1) CN107074345B (enExample)
ES (1) ES2761648T3 (enExample)
WO (1) WO2016025029A1 (enExample)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3460436A1 (en) 2017-09-22 2019-03-27 Rosemount Aerospace Inc. Low profile sensor
EP3462178B1 (en) 2017-09-22 2021-05-26 Rosemount Aerospace Inc. Low profile air data architecture
CN108382565B (zh) * 2018-03-22 2024-03-22 北航（四川）西部国际创新港科技有限公司 襟翼自动调节飞行器
US20200385133A1 (en) * 2019-06-06 2020-12-10 Gulfstream Aerospace Corporation Engine and thrust control of aircraft in no dwell zone
EP3808655B1 (de) * 2019-10-16 2022-08-31 Aircraft Cabin Modification GmbH System zur nutzlastüberwachung, flugzeug und verfahren
JP7458052B2 (ja) * 2019-11-14 2024-03-29 国立研究開発法人宇宙航空研究開発機構 乱気流センシングシステム、航空機及び乱気流センシング方法
CN111156995A (zh) * 2020-01-22 2020-05-15 南京航空航天大学 一种基于飞行状态感知的智能飞行器及飞行方法
US20210233413A1 (en) * 2020-01-23 2021-07-29 Aerion Intellectual Property Management Corporation Real-time automated method and system enabling continuous supersonic flight while preventing ground level sonic boom
CN117760681B (zh) * 2024-02-22 2024-05-31 中国空气动力研究与发展中心高速空气动力研究所 一种适用于大型超声速风洞的组合式声爆试验装置及方法

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FR1071234A (fr) * 1952-11-19 1954-08-27 Sncase Procédé et dispositif d'adaptation des profils aérodynamiques à bord d'attaque aigu à une vitesse quelconque, subsonique ou supersonique
US2997843A (en) * 1958-04-23 1961-08-29 Bendix Corp Inlet control system for supersonic aircraft
IT699976A (enExample) * 1959-02-17 1900-01-01
US3221549A (en) * 1962-11-09 1965-12-07 Joseph W Wetmore Aircraft instrument
US3181818A (en) * 1964-05-15 1965-05-04 United Aircraft Corp Shock wave position controller
US4114842A (en) * 1977-03-28 1978-09-19 Sperry Rand Corporation Acceleration limited preselect altitude capture and control
US4648569A (en) * 1985-10-23 1987-03-10 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Airplane automatic control force trimming device for asymmetric engine failures
JPS6385500U (enExample) * 1986-11-21 1988-06-03
JPH01254491A (ja) * 1988-04-04 1989-10-11 Mitsubishi Heavy Ind Ltd 前縁フラップ装置
US5186415A (en) * 1990-05-14 1993-02-16 Qun Li Aircraft having means for controlling the ground effect flying altitude by sensing air pressure on the surface of the wing
CN1064016C (zh) * 1992-07-16 2001-04-04 李群 弱地效飞行器
US5448881A (en) * 1993-06-09 1995-09-12 United Technologies Corporation Gas turbine engine control based on inlet pressure distortion
DE4422152C2 (de) * 1994-06-27 2000-02-03 Daimler Chrysler Aerospace Verfahren und Anordnung zum Optimieren der aerodynamischen Wirkung eines Tragflügels
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JP2000227048A (ja) * 1999-02-05 2000-08-15 Ishikawajima Harima Heavy Ind Co Ltd ジェット騒音低減方法及び機構
US6905091B2 (en) * 2003-07-14 2005-06-14 Supersonic Aerospace International, Llc System and method for controlling the acoustic signature of a device
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EP2180183A1 (en) * 2008-10-23 2010-04-28 Siemens Aktiengesellschaft Stall detection by use of pressure sensors
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Also Published As

Publication number Publication date
US20160257397A1 (en) 2016-09-08
CN107074345B (zh) 2020-01-07
EP3180244A1 (en) 2017-06-21
EP3180244B1 (en) 2019-09-11
CN107074345A (zh) 2017-08-18
JP6590419B2 (ja) 2019-10-16
WO2016025029A1 (en) 2016-02-18
US9878778B2 (en) 2018-01-30
JP2017523089A (ja) 2017-08-17

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