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WO2008093447A1 - 低騒音航空機 - Google Patents

低騒音航空機 Download PDF

Info

Publication number
WO2008093447A1
WO2008093447A1 PCT/JP2007/066761 JP2007066761W WO2008093447A1 WO 2008093447 A1 WO2008093447 A1 WO 2008093447A1 JP 2007066761 W JP2007066761 W JP 2007066761W WO 2008093447 A1 WO2008093447 A1 WO 2008093447A1
Authority
WO
WIPO (PCT)
Prior art keywords
engine
thrust
landing
ground
nozzle
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.)
Ceased
Application number
PCT/JP2007/066761
Other languages
English (en)
French (fr)
Inventor
Shigeru Horinouchi
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.)
Japan Aerospace Exploration Agency JAXA
Original Assignee
Japan Aerospace Exploration Agency JAXA
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 Japan Aerospace Exploration Agency JAXA filed Critical Japan Aerospace Exploration Agency JAXA
Priority to AT07806238T priority Critical patent/ATE530436T1/de
Priority to EP07806238A priority patent/EP2116714B1/en
Priority to US12/524,086 priority patent/US20100006697A1/en
Priority to JP2008556006A priority patent/JP4873505B2/ja
Publication of WO2008093447A1 publication Critical patent/WO2008093447A1/ja
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • 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
    • B64D33/04—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
    • 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
    • B64D33/04—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • B64D33/06—Silencing exhaust or propulsion jets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/006—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector within one plane only
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1207—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a fixed structure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/44—Nozzles having means, e.g. a shield, reducing sound radiation in a specified direction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
    • 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
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Exhaust Silencers (AREA)
  • Inorganic Insulating Materials (AREA)
  • Vehicle Waterproofing, Decoration, And Sanitation Devices (AREA)

Abstract

　公知の機構を利用することにより航空機の離着陸時の地上におけるエンジン騒音を大幅に低減することが可能な低騒音航空機を提供する。 　公知の機構で構成された推力の方向を可変にする推力偏向手段を利用して、エンジンのジェット排気騒音の最大伝播方向を地上から遠ざけるようにエンジンの排気方向を航空機の経路方向（飛行方向）に関して上側（上方）になるように偏向することにより、航空機の離着陸時の地上におけるエンジン騒音レベルを低減する。特に、推力偏向式排気ノズル２０が上部偏向ノズル２１および下部偏向ノズル２２によって構成されている場合は、着陸滑走時において、エンジンに逆推力を発生させることが出来るようになる。
PCT/JP2007/066761 2007-01-30 2007-08-29 低騒音航空機 Ceased WO2008093447A1 (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
AT07806238T ATE530436T1 (de) 2007-01-30 2007-08-29 Geräuscharmes luftfahrzeug
EP07806238A EP2116714B1 (en) 2007-01-30 2007-08-29 Low noise aircraft
US12/524,086 US20100006697A1 (en) 2007-01-30 2007-08-29 Low noise aircraft
JP2008556006A JP4873505B2 (ja) 2007-01-30 2007-08-29 低騒音航空機

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2007-019456 2007-01-30
JP2007019456 2007-01-30

Publications (1)

Publication Number Publication Date
WO2008093447A1 true WO2008093447A1 (ja) 2008-08-07

Family

ID=39673763

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2007/066761 Ceased WO2008093447A1 (ja) 2007-01-30 2007-08-29 低騒音航空機

Country Status (5)

Country Link
US (1) US20100006697A1 (ja)
EP (1) EP2116714B1 (ja)
JP (1) JP4873505B2 (ja)
AT (1) ATE530436T1 (ja)
WO (1) WO2008093447A1 (ja)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2946019A1 (fr) * 2009-05-29 2010-12-03 Airbus France Systeme propulsif multifonctions pour avion
JP2022535892A (ja) * 2019-06-07 2022-08-10 ジップエール 推進装置のための推力ユニット及び関連した推進装置

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10822076B2 (en) 2014-10-01 2020-11-03 Sikorsky Aircraft Corporation Dual rotor, rotary wing aircraft
WO2016053408A1 (en) * 2014-10-01 2016-04-07 Sikorsky Aircraft Corporation Acoustic signature variation of aircraft utilizing a clutch
CN104863749B (zh) * 2015-03-27 2017-01-18 南京航空航天大学 具有反推功能的旁路式无源双喉道矢量喷管
FR3062371B1 (fr) * 2017-01-31 2019-03-29 Airbus Nacelle d'un turboreacteur comportant un volet inverseur
EP3957560B1 (en) * 2017-12-07 2023-11-15 Zipair Improved thrust systems
CN113107706B (zh) * 2021-04-25 2022-03-22 中国航发沈阳发动机研究所 一种二元矢量喷管外罩结构及其设计方法
CN115962063A (zh) * 2023-01-06 2023-04-14 沈阳飞机设计研究所扬州协同创新研究院有限公司 一种轴对称喉道滑动调节的单边膨胀喷管

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS50135416A (ja) * 1974-04-03 1975-10-27
JPS5177712A (en) * 1974-09-19 1976-07-06 Rolls Royce 1971 Ltd Jetsutoenjinno shusuishinjetsutono shoonhohooyobi sochi
JPH07208263A (ja) 1994-01-21 1995-08-08 Ishikawajima Harima Heavy Ind Co Ltd 超音速航空機用排気ノズル
JPH08135505A (ja) 1994-09-14 1996-05-28 Mitsubishi Heavy Ind Ltd 超音速航空機用ジェット推進機関の吸音装置
JP2000205045A (ja) * 1999-01-14 2000-07-25 Soc Natl Etud Constr Mot Aviat <Snecma> 可逆一体型のタ―ボファンエンジンの排気ノズル
JP2004530078A (ja) * 2001-06-14 2004-09-30 プラット　アンド　ホイットニー　カナダ　コーポレイション ジェット騒音低減用の排気流ガイド

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS52135416A (en) * 1976-05-09 1977-11-12 Minoru Yoshida Tube for hydraulic apparatus
DE10033653A1 (de) * 2000-06-16 2002-03-07 Sandor Nagy Kombinationsantrieb
US6938408B2 (en) * 2001-04-26 2005-09-06 Propulsion Vectoring, L.P. Thrust vectoring and variable exhaust area for jet engine nozzle

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS50135416A (ja) * 1974-04-03 1975-10-27
JPS5177712A (en) * 1974-09-19 1976-07-06 Rolls Royce 1971 Ltd Jetsutoenjinno shusuishinjetsutono shoonhohooyobi sochi
JPH07208263A (ja) 1994-01-21 1995-08-08 Ishikawajima Harima Heavy Ind Co Ltd 超音速航空機用排気ノズル
JPH08135505A (ja) 1994-09-14 1996-05-28 Mitsubishi Heavy Ind Ltd 超音速航空機用ジェット推進機関の吸音装置
JP2000205045A (ja) * 1999-01-14 2000-07-25 Soc Natl Etud Constr Mot Aviat <Snecma> 可逆一体型のタ―ボファンエンジンの排気ノズル
JP2004530078A (ja) * 2001-06-14 2004-09-30 プラット　アンド　ホイットニー　カナダ　コーポレイション ジェット騒音低減用の排気流ガイド

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2946019A1 (fr) * 2009-05-29 2010-12-03 Airbus France Systeme propulsif multifonctions pour avion
JP2022535892A (ja) * 2019-06-07 2022-08-10 ジップエール 推進装置のための推力ユニット及び関連した推進装置
JP7285028B2 (ja) 2019-06-07 2023-06-01 ジップエール 推進装置のための推力ユニット及び関連した推進装置

Also Published As

Publication number Publication date
EP2116714B1 (en) 2011-10-26
ATE530436T1 (de) 2011-11-15
US20100006697A1 (en) 2010-01-14
EP2116714A4 (en) 2010-07-07
EP2116714A1 (en) 2009-11-11
JPWO2008093447A1 (ja) 2010-05-20
JP4873505B2 (ja) 2012-02-08

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