[go: up one dir, main page]

AUMAN, 1993 - Google Patents

Wind tunnel investigation with an operational turbojet engine

AUMAN, 1993

Document ID
6719154700086834226
Author
AUMAN L
Publication year
Publication venue
31st Aerospace Sciences Meeting

External Links

Snippet

ABSTRACT A wind tunnel test of a turbojet powered missile with the engine installed and operating was conducted in Calspan's Transonic Wind Tunnel in Buffalo, New York from 20 May to 3 June 1991. The primary model corrfguration consisted of a bifurcated inlet and …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies
    • Y02T50/67Relevant aircraft propulsion technologies
    • Y02T50/671Measures to reduce the propulsor weight
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162Bearing supports
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • 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
    • F02C7/26Starting; Ignition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants 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
    • F02K7/10Plants 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
    • F02K7/16Composite ram-jet/turbo-jet engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • 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
    • F05D2260/00Function
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02Aircraft characterised by the type or position of power plant
    • B64D27/16Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • 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
    • F05D2270/00Control

Similar Documents

Publication Publication Date Title
US8215580B2 (en) Attachment of a multiflow turbojet engine to an aircraft
US12345205B2 (en) Hydrogen-fuelled gas turbine engine with fuel-to-air turbocharger
US20190178106A1 (en) Fairings for power generation machines
AUMAN Wind tunnel investigation with an operational turbojet engine
Meher-Homji et al. Pioneering Turbojet Developments of Dr. Hans Von Ohain—From the HeS 1 to the HeS 011
Lu et al. Performance analysis of stovl aircraft nozzle in hover
RU2162957C2 (en) Aircraft gas-turbine engine
Barbeau A family of small, low cost turbojet engines for short life applications
Greatrix Gas turbine engines: Fundamentals
Gentry Jr et al. Effect of pylon wake with and without pylon blowing on propeller thrust
Meher-Homji The development of the junkers jumo 004b—The world’s first production turbojet
Esterly Ground test facilities for aircraft airbreathing propulsion system development
Lederer et al. Hypersonic airbreathing propulsion activities for Saenger
Moult The development of the Goblin engine
Taguchi et al. Conceptual study on hypersonic turbojet experimental vehicle (hytex)
Brown J58/SR-71 Propulsion Integration
Briggs et al. Synthesis and performance of an Air-TurboRamjet-propelled supersonictarget vehicle
Edefur et al. Design of an air-launched tactical missile for three different propulsion systems: ATR, rocket and turbojet
Lopez-Diez et al. Front end optimization of high speed turboprop engines
Coalson Development of the F110-GE-100 engine
DUE Development of the model 373 turbojet engine
Chuslo et al. LARZAC: A Small Turbofan Engine for Military and General Aviation Aircraft
Ricco The heart of the SR-71" Blackbird": The mighty J-58 engine
Kress Afterburners and variable nozzles
Mandle Twenty Year Evolution of the WR2/WR24 Series of Small Turbojet Engines