CN107074345B - 用于控制飞行中的航空器周围的压力场的系统和方法 - Google Patents

用于控制飞行中的航空器周围的压力场的系统和方法 Download PDF

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Publication number
CN107074345B
CN107074345B CN201580049510.0A CN201580049510A CN107074345B CN 107074345 B CN107074345 B CN 107074345B CN 201580049510 A CN201580049510 A CN 201580049510A CN 107074345 B CN107074345 B CN 107074345B
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CN
China
Prior art keywords
pressure
aircraft
controller
pressure field
request
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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
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CN201580049510.0A
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English (en)
Chinese (zh)
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CN107074345A (zh
Inventor
T·康纳斯
M·奈特
R·科沃特
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Gulfstream Aerospace Corp
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Gulfstream Aerospace Corp
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Publication of CN107074345A publication Critical patent/CN107074345A/zh
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    • 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

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  • 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)
CN201580049510.0A 2014-08-14 2015-02-26 用于控制飞行中的航空器周围的压力场的系统和方法 Expired - Fee Related CN107074345B (zh)

Applications Claiming Priority (3)

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
US14/459,488 2014-08-14
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 (2)

Publication Number Publication Date
CN107074345A CN107074345A (zh) 2017-08-18
CN107074345B true CN107074345B (zh) 2020-01-07

Family

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Family Applications (1)

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CN201580049510.0A Expired - Fee Related CN107074345B (zh) 2014-08-14 2015-02-26 用于控制飞行中的航空器周围的压力场的系统和方法

Country Status (6)

Country Link
US (1) US9878778B2 (cg-RX-API-DMAC10.html)
EP (1) EP3180244B1 (cg-RX-API-DMAC10.html)
JP (1) JP6590419B2 (cg-RX-API-DMAC10.html)
CN (1) CN107074345B (cg-RX-API-DMAC10.html)
ES (1) ES2761648T3 (cg-RX-API-DMAC10.html)
WO (1) WO2016025029A1 (cg-RX-API-DMAC10.html)

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

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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 (cg-RX-API-DMAC10.html) * 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 (cg-RX-API-DMAC10.html) * 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
US5669582A (en) * 1995-05-12 1997-09-23 The Boeing Company Method and apparatus for reducing unwanted sideways motion in the aft cabin and roll-yaw upsets of an airplane due to atmospheric turbulence and wind gusts
US5875998A (en) * 1996-02-05 1999-03-02 Daimler-Benz Aerospace Airbus Gmbh Method and apparatus for optimizing the aerodynamic effect of an airfoil
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
US20070252035A1 (en) * 2005-11-29 2007-11-01 Hubbard James E Jr Unmanned vehicle
EP2180183A1 (en) * 2008-10-23 2010-04-28 Siemens Aktiengesellschaft Stall detection by use of pressure sensors
US20100258678A1 (en) * 2009-04-09 2010-10-14 Nicholas Jonathan Fermor Aircraft stall protection system
US10002491B2 (en) * 2009-07-07 2018-06-19 Bally Gaming, Inc. Controlling gaming effects on available presentation devices of gaming network nodes
US8320217B1 (en) * 2009-10-01 2012-11-27 Raytheon Bbn Technologies Corp. Systems and methods for disambiguating shooter locations with shockwave-only location
US20130345910A1 (en) * 2011-02-11 2013-12-26 The Board Of Trustees Of The University Of Illinois Detector function and system for predicting airfoil stall from control surface measurements
US8788122B1 (en) * 2012-08-24 2014-07-22 The Boeing Company Wing load alleviation methods and apparatus
WO2015065551A1 (en) * 2013-07-25 2015-05-07 Lam Aviation, Inc. Aircraft wing structure and control system
US9334807B2 (en) * 2014-05-13 2016-05-10 The Boeing Company Methods and apparatus to determine airflow conditions at an inlet of an engine

Also Published As

Publication number Publication date
US20160257397A1 (en) 2016-09-08
ES2761648T3 (es) 2020-05-20
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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