DE602004000498D1 - Lufteinlauf und Verfahren zum Betrieb des Lufteinlaufs - Google Patents

Lufteinlauf und Verfahren zum Betrieb des Lufteinlaufs

Info

Publication number
DE602004000498D1
DE602004000498D1 DE200460000498 DE602004000498T DE602004000498D1 DE 602004000498 D1 DE602004000498 D1 DE 602004000498D1 DE 200460000498 DE200460000498 DE 200460000498 DE 602004000498 T DE602004000498 T DE 602004000498T DE 602004000498 D1 DE602004000498 D1 DE 602004000498D1
Authority
DE
Germany
Prior art keywords
air inlet
inlet
air
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
Application number
DE200460000498
Other languages
English (en)
Other versions
DE602004000498T2 (de
Inventor
Hiroaki Kobayashi
Nobuhiro Tanatsugu
Tetsuya Sato
Takayuki Kojima
Yusuke Maru
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
Publication of DE602004000498D1 publication Critical patent/DE602004000498D1/de
Application granted granted Critical
Publication of DE602004000498T2 publication Critical patent/DE602004000498T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0253Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft
    • B64D2033/026Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft for supersonic or hypersonic aircraft
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/80Application in supersonic vehicles excluding hypersonic vehicles or ram, scram or rocket propulsion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/10Two-dimensional
    • F05D2250/14Two-dimensional elliptical
    • F05D2250/141Two-dimensional elliptical circular
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/90Variable geometry
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/0536Highspeed fluid intake means [e.g., jet engine intake]
    • Y10T137/0645With condition responsive control means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Body Structure For Vehicles (AREA)
  • Jet Pumps And Other Pumps (AREA)
DE200460000498 2003-01-24 2004-01-21 Lufteinlauf und Verfahren zum Betrieb des Lufteinlaufs Expired - Lifetime DE602004000498T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2003016096 2003-01-24
JP2003016096A JP3747244B2 (ja) 2003-01-24 2003-01-24 エアインテーク、及びエアインテーク方法

Publications (2)

Publication Number Publication Date
DE602004000498D1 true DE602004000498D1 (de) 2006-05-11
DE602004000498T2 DE602004000498T2 (de) 2006-08-24

Family

ID=32588691

Family Applications (1)

Application Number Title Priority Date Filing Date
DE200460000498 Expired - Lifetime DE602004000498T2 (de) 2003-01-24 2004-01-21 Lufteinlauf und Verfahren zum Betrieb des Lufteinlaufs

Country Status (4)

Country Link
US (1) US7322179B2 (de)
EP (1) EP1441116B1 (de)
JP (1) JP3747244B2 (de)
DE (1) DE602004000498T2 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2474552C (en) 2002-01-30 2011-07-26 Gulfstream Aerospace Corporation Fuselage shaping and inclusion of spike on a supersonic aircraft for controlling and reducing sonic boom
CA3071172A1 (en) * 2005-12-15 2008-04-17 Gulfstream Aerospace Corporation Isentropic compression inlet for supersonic aircraft
US8393158B2 (en) 2007-10-24 2013-03-12 Gulfstream Aerospace Corporation Low shock strength inlet
US20100284791A1 (en) * 2009-05-11 2010-11-11 Robert Jesse Flores Apparatuses, systems, and methods for preventing foreign objects from being ingested into a jet engine
JP6016616B2 (ja) * 2012-12-21 2016-10-26 三菱重工業株式会社 ジェットエンジン
US9862482B2 (en) * 2015-09-04 2018-01-09 The Boeing Company Variable geometry flush boundary diverter
CN105523189B (zh) * 2015-12-14 2017-11-21 成都飞机设计研究所 一种滑动变体可调caret进气道
CN107605601B (zh) * 2017-09-29 2018-08-31 南京航空航天大学 一种捕获面积与喉道面积同步调节的超声速进气道及其控制方法和设计方法
CN112483256B (zh) * 2020-12-06 2022-08-23 西安长峰机电研究所 一种冲压发动机进气口自动开闭装置
CN114010953B (zh) * 2021-11-10 2024-02-06 固安翌光科技有限公司 一种光疗主体及鼻部治疗装置

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3131534A (en) * 1955-10-19 1964-05-05 Thompson Ramo Wooldridge Inc Spike control for jet engines
US2934893A (en) * 1957-05-06 1960-05-03 Westinghouse Electric Corp Air intake structure for an aircraft engine
US3067573A (en) * 1958-02-27 1962-12-11 James F Connors Telescoping-spike supersonic inlet for aircraft engines
US3374631A (en) * 1965-08-16 1968-03-26 Mcdonnell Aircraft Corp Combination subsonic and supersonic propulsion system and apparatus
US4007891A (en) 1975-09-12 1977-02-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Jet engine air intake system
DE2801119C2 (de) 1978-01-12 1982-12-02 Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5000 Köln Überschallufteinlauf fester Geometrie für luftatmende Rückstoßtriebwerke von lenkbaren Flugkörpern oder Flugzeugen, insbesondere für mit Festbrennstoffen betriebene Stauantriebe
DE3236487C2 (de) 1982-10-01 1984-07-19 Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5000 Köln Rotationssymmetrischer Überschall-Lufteinlauf für Strahltriebwerke
US5301901A (en) 1993-01-29 1994-04-12 General Electric Company Telescoping centerbody wedge for a supersonic inlet

Also Published As

Publication number Publication date
US20040144077A1 (en) 2004-07-29
EP1441116A1 (de) 2004-07-28
DE602004000498T2 (de) 2006-08-24
JP3747244B2 (ja) 2006-02-22
US7322179B2 (en) 2008-01-29
JP2004224252A (ja) 2004-08-12
EP1441116B1 (de) 2006-03-22

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition