AU2001260966A1 - Propulsion module - Google Patents

Propulsion module

Info

Publication number
AU2001260966A1
AU2001260966A1 AU2001260966A AU6096601A AU2001260966A1 AU 2001260966 A1 AU2001260966 A1 AU 2001260966A1 AU 2001260966 A AU2001260966 A AU 2001260966A AU 6096601 A AU6096601 A AU 6096601A AU 2001260966 A1 AU2001260966 A1 AU 2001260966A1
Authority
AU
Australia
Prior art keywords
propulsion module
propulsion
module
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.)
Abandoned
Application number
AU2001260966A
Inventor
Von David Baker
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.)
Rolls Royce North American Technologies Inc
Original Assignee
Allison Advanced Development Co Inc
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 Allison Advanced Development Co Inc filed Critical Allison Advanced Development Co Inc
Publication of AU2001260966A1 publication Critical patent/AU2001260966A1/en
Abandoned 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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plant of jet type within or attached to fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements 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
    • F02C7/00—Features, 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
    • F02K7/04—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet with resonant combustion chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
    • F02K7/06—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet with combustion chambers having valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/20—Composite ram-jet/pulse-jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/78—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with an air-breathing jet-propulsion plant
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/002—Launch systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/401—Liquid propellant rocket engines
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]
AU2001260966A 2000-01-12 2001-01-12 Propulsion module Abandoned AU2001260966A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US17580800P 2000-01-12 2000-01-12
US60175808 2000-01-12
PCT/US2001/000931 WO2001054981A2 (en) 2000-01-12 2001-01-12 Propulsion module

Publications (1)

Publication Number Publication Date
AU2001260966A1 true AU2001260966A1 (en) 2001-08-07

Family

ID=22641711

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001260966A Abandoned AU2001260966A1 (en) 2000-01-12 2001-01-12 Propulsion module

Country Status (3)

Country Link
US (1) US6584764B2 (en)
AU (1) AU2001260966A1 (en)
WO (1) WO2001054981A2 (en)

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US9436667B2 (en) * 2000-05-19 2016-09-06 Renderx, Inc. Techniques for rendering media as layers
US7137243B2 (en) * 2002-07-03 2006-11-21 Rolls-Royce North American Technologies, Inc. Constant volume combustor
US7621118B2 (en) 2002-07-03 2009-11-24 Rolls-Royce North American Technologies, Inc. Constant volume combustor having a rotating wave rotor
US7055308B2 (en) 2003-05-30 2006-06-06 General Electric Company Detonation damper for pulse detonation engines
US6846208B1 (en) 2003-11-03 2005-01-25 Lockheed Martin Corporation Wave rotor based power and propulsion generation for a marine vessel
US6983586B2 (en) 2003-12-08 2006-01-10 General Electric Company Two-stage pulse detonation system
US7216474B2 (en) 2004-02-19 2007-05-15 Aerojet-General Corporation Integrated air inlet system for multi-propulsion aircraft engines
EP1812688B1 (en) * 2004-11-12 2016-04-13 Board of Trustees of Michigan State University Composite turbomachine impeller and method of manufacture
US7555891B2 (en) 2004-11-12 2009-07-07 Board Of Trustees Of Michigan State University Wave rotor apparatus
US7784265B2 (en) * 2006-02-07 2010-08-31 General Electric Company Multiple tube pulse detonation engine turbine apparatus and system
EP2102355B1 (en) 2006-12-14 2016-03-02 Bolder Biotechnology, Inc. Long acting proteins and peptides and methods of making and using the same
US9404441B2 (en) * 2008-08-18 2016-08-02 Aerojet Rocketdyne Of De, Inc. Low velocity injector manifold for hypergolic rocket engine
CN101956631B (en) * 2010-09-30 2013-04-03 西北工业大学 Air inlet channel of air-breathing type pulse detonation engine
WO2012116285A2 (en) 2011-02-25 2012-08-30 Board Of Trustees Of Michigan State University Wave disc engine apparatus
US9957060B2 (en) 2012-03-21 2018-05-01 Hamilton Sundstrand Corporation Deployable inlet scoop for an inboard ram air turbine
RU2503590C1 (en) * 2012-10-25 2014-01-10 Юлия Алексеевна Щепочкина Aircraft
US9920689B2 (en) * 2013-03-15 2018-03-20 Indiana University Research And Technology Corporation Hybrid wave rotor propulsion system
CN106499516B (en) * 2016-10-26 2018-12-07 南京航空航天大学 Internal combustion wave rotor mixes gas and forms device
RU174498U1 (en) * 2017-04-28 2017-10-17 Федеральное государственное унитарное предприятие Тушинское машиностроительное конструкторское бюро "Союз" ФГУП ТМКБ "Союз" POWER INSTALLATION OF A HYPERSONIC AIRCRAFT
US10969107B2 (en) 2017-09-15 2021-04-06 General Electric Company Turbine engine assembly including a rotating detonation combustor
US11591101B2 (en) 2020-01-15 2023-02-28 Raytheon Technologies Corporation Diffuser for rotating detonation engine
CN112627905B (en) * 2020-12-18 2022-05-03 常州工学院 Internal combustion wave rotor exhaust mixing device based on blade diversion pressure relief
CN113236424B (en) * 2021-06-22 2022-07-05 西安航天动力研究所 Double-lower-side rear supersonic air inlet
US20230123752A1 (en) * 2021-10-20 2023-04-20 Innoveering, LLC Deployable inlet assembly for aerial vehicle
IL294415B2 (en) 2022-06-29 2023-10-01 Israel Aerospace Ind Ltd Air intake module for a projectile

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Also Published As

Publication number Publication date
US20030029162A1 (en) 2003-02-13
US6584764B2 (en) 2003-07-01
WO2001054981A3 (en) 2002-03-07
WO2001054981A2 (en) 2001-08-02

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