AU2003266099A1 - Jet motor or turbine motor - Google Patents

Jet motor or turbine motor

Info

Publication number
AU2003266099A1
AU2003266099A1 AU2003266099A AU2003266099A AU2003266099A1 AU 2003266099 A1 AU2003266099 A1 AU 2003266099A1 AU 2003266099 A AU2003266099 A AU 2003266099A AU 2003266099 A AU2003266099 A AU 2003266099A AU 2003266099 A1 AU2003266099 A1 AU 2003266099A1
Authority
AU
Australia
Prior art keywords
motor
jet
turbine
turbine motor
jet motor
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
AU2003266099A
Inventor
Cestmir Havranek
Zdenek Katolick
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.)
PRVNI BRNENSKA STROJIRNA VELKA BITES AS
Original Assignee
PRVNI BRNENSKA STROJIRNA VELKA
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 PRVNI BRNENSKA STROJIRNA VELKA filed Critical PRVNI BRNENSKA STROJIRNA VELKA
Publication of AU2003266099A1 publication Critical patent/AU2003266099A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/18—Structural association of electric generators with mechanical driving motors, e.g. with turbines
    • H02K7/1807—Rotary generators
    • H02K7/1823—Rotary generators structurally associated with turbines or similar engines
    • 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
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
AU2003266099A 2002-09-06 2003-09-03 Jet motor or turbine motor Abandoned AU2003266099A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CZ200213449U CZ12724U1 (en) 2002-09-06 2002-09-06 Jet or turbine engine
CZPUV2002-13449 2002-09-06
PCT/CZ2003/000050 WO2004022948A1 (en) 2002-09-06 2003-09-03 Jet motor or turbine motor

Publications (1)

Publication Number Publication Date
AU2003266099A1 true AU2003266099A1 (en) 2004-03-29

Family

ID=5476593

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2003266099A Abandoned AU2003266099A1 (en) 2002-09-06 2003-09-03 Jet motor or turbine motor

Country Status (4)

Country Link
CN (1) CN100447388C (en)
AU (1) AU2003266099A1 (en)
CZ (1) CZ12724U1 (en)
WO (1) WO2004022948A1 (en)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1614855A1 (en) * 2004-07-05 2006-01-11 Siemens Aktiengesellschaft Turbomachine and method to operate such a turbomachine
US7937927B2 (en) 2004-12-01 2011-05-10 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
WO2006060004A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Combustor for turbine engine
DE602004019710D1 (en) 2004-12-01 2009-04-09 United Technologies Corp REMOTE CONTROL FOR AN ADJUSTABLE STAGE OF A COMPRESSOR FOR A TURBINE ENGINE
WO2006110123A2 (en) 2004-12-01 2006-10-19 United Technologies Corporation Vectoring transition duct for turbine engine
US8096753B2 (en) 2004-12-01 2012-01-17 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
WO2006059985A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Axial compressor for tip turbine engine
WO2006060013A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Seal assembly for a fan rotor of a tip turbine engine
DE602004016065D1 (en) 2004-12-01 2008-10-02 United Technologies Corp VARIABLE BULB INLET BUCKET ASSEMBLY, TURBINE ENGINE WITH SUCH AN ARRANGEMENT AND CORRESPONDING STEERING PROCEDURE
WO2006110122A2 (en) 2004-12-01 2006-10-19 United Technologies Corporation Inflatable bleed valve for a turbine engine and a method of operating therefore
EP1825116A2 (en) 2004-12-01 2007-08-29 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
US8757959B2 (en) 2004-12-01 2014-06-24 United Technologies Corporation Tip turbine engine comprising a nonrotable compartment
EP1825170B1 (en) 2004-12-01 2009-03-18 United Technologies Corporation Gearbox lubrication supply system for a tip turbine engine
US7883314B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Seal assembly for a fan-turbine rotor of a tip turbine engine
WO2006060014A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Starter generator system for a tip turbine engine
DE602004027766D1 (en) 2004-12-01 2010-07-29 United Technologies Corp HYDRAULIC SEAL FOR A GEARBOX OF A TOP TURBINE ENGINE
EP1828591B1 (en) 2004-12-01 2010-07-21 United Technologies Corporation Peripheral combustor for tip turbine engine
EP1825117B1 (en) 2004-12-01 2012-06-13 United Technologies Corporation Turbine engine with differential gear driven fan and compressor
DE602004029950D1 (en) 2004-12-01 2010-12-16 United Technologies Corp SLIDED GEAR ASSEMBLY FOR A TOP TURBINE ENGINE
US7475545B2 (en) 2005-04-29 2009-01-13 General Electric Company Fladed supersonic missile turbojet
US7424805B2 (en) 2005-04-29 2008-09-16 General Electric Company Supersonic missile turbojet engine
US7509797B2 (en) 2005-04-29 2009-03-31 General Electric Company Thrust vectoring missile turbojet
US7448199B2 (en) 2005-04-29 2008-11-11 General Electric Company Self powdered missile turbojet
US8015828B2 (en) * 2007-04-03 2011-09-13 General Electric Company Power take-off system and gas turbine engine assembly including same
CN103967535A (en) * 2013-02-01 2014-08-06 中国航空工业集团公司西安飞机设计研究所 Refrigeration and electricitygeneration integrated device driven by air turbine
CN106703993A (en) * 2015-11-14 2017-05-24 熵零股份有限公司 Engine
DE102016207517A1 (en) * 2016-05-02 2017-11-02 Siemens Aktiengesellschaft Propulsion system for aircraft with electric generator
GB2567674B (en) * 2017-10-20 2022-04-06 Rolls Royce Plc Motor Generator System for a Gas Turbine Engine
CN109113803A (en) * 2018-11-09 2019-01-01 上海尚实能源科技有限公司 Rotor startup structure for turbogenerator
CN109268168A (en) * 2018-11-26 2019-01-25 北京金朋达航空科技有限公司 Height pushes away the small-size turbojet engine of ratio
CN111828375A (en) * 2020-06-30 2020-10-27 中国航发南方工业有限公司 Split-flow centrifugal impeller and aircraft engine with same
CN115324660A (en) * 2022-08-19 2022-11-11 上海翠日航空科技有限公司 Miniature turbine power generation all-in-one machine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3187188A (en) * 1959-07-21 1965-06-01 Curtiss Wright Corp High speed turbo-generator
US3071691A (en) * 1960-05-31 1963-01-01 Curtiss Wright Corp Shaft support
GB1041587A (en) * 1962-08-27 1966-09-07 Bristol Siddeley Engines Ltd Improvements in gas turbine engines
GB1147730A (en) * 1967-12-19 1969-04-02 Rolls Royce Improvements in or relating to gas turbine engines
US3859785A (en) * 1973-12-17 1975-01-14 Curtiss Wright Corp Turbine engine with integral compressor and alternator rotor
DE2967669D1 (en) * 1979-05-14 1987-12-17 Norbert L Osborn A bearing assembly structure
US4482303A (en) * 1982-01-27 1984-11-13 Ray Acosta Turbo-compressor apparatus
US5237817A (en) * 1992-02-19 1993-08-24 Sundstrand Corporation Gas turbine engine having low cost speed reduction drive

Also Published As

Publication number Publication date
CN1682023A (en) 2005-10-12
WO2004022948A1 (en) 2004-03-18
CN100447388C (en) 2008-12-31
CZ12724U1 (en) 2002-10-23

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase