NL69078C - - Google Patents

Info

Publication number
NL69078C
NL69078C NL69078DA NL69078C NL 69078 C NL69078 C NL 69078C NL 69078D A NL69078D A NL 69078DA NL 69078 C NL69078 C NL 69078C
Authority
NL
Netherlands
Application number
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.)
Publication of NL69078C publication Critical patent/NL69078C/xx

Links

Classifications

    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/073—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the compressor and turbine stages being concentric

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
NL69078D 1944-01-31 NL69078C (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2548975X 1944-01-31

Publications (1)

Publication Number Publication Date
NL69078C true NL69078C (fr)

Family

ID=10909804

Family Applications (1)

Application Number Title Priority Date Filing Date
NL69078D NL69078C (fr) 1944-01-31

Country Status (2)

Country Link
US (1) US2548975A (fr)
NL (1) NL69078C (fr)

Families Citing this family (92)

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US3861139A (en) * 1973-02-12 1975-01-21 Gen Electric Turbofan engine having counterrotating compressor and turbine elements and unique fan disposition
US6263664B1 (en) * 1996-06-28 2001-07-24 Hiroyasu Tanigawa Combined steam and gas turbine engine with magnetic transmission
US6397577B1 (en) * 2001-04-02 2002-06-04 The United States Of America As Represented By The Secretary Of The Air Force Shaftless gas turbine engine spool
EP1828573B1 (fr) * 2004-12-01 2010-06-16 United Technologies Corporation Joint hydraulique pour boite de vitesses de moteur a turbine d'extremite
WO2006059993A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Moteur à turbine en bout avec étages soufflante et turbine multiples
US8468795B2 (en) 2004-12-01 2013-06-25 United Technologies Corporation Diffuser aspiration for a tip turbine engine
DE602004019709D1 (de) * 2004-12-01 2009-04-09 United Technologies Corp Tip-turbinentriebwerk und entsprechendes betriebsverfahren
EP1825117B1 (fr) * 2004-12-01 2012-06-13 United Technologies Corporation Moteur à turbine équipé d'une soufflante et d'un compresseur entraînés par un engrenage différentiel
DE602004019710D1 (de) * 2004-12-01 2009-04-09 United Technologies Corp Fernbetätigung für eine verstellbare stufe eines verdichters für einen turbinenmotor
US8757959B2 (en) * 2004-12-01 2014-06-24 United Technologies Corporation Tip turbine engine comprising a nonrotable compartment
EP1828547B1 (fr) 2004-12-01 2011-11-30 United Technologies Corporation Turbosoufflante comprenant une pluralité d'aubes directrices d'entrée commandées individuellement et procédé de commande associé
EP1834071B1 (fr) * 2004-12-01 2013-03-13 United Technologies Corporation Inducteur de pale de ventilateur de moteur de turbine a pression d'entree
US7874163B2 (en) * 2004-12-01 2011-01-25 United Technologies Corporation Starter generator system for a tip turbine engine
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EP1825177B1 (fr) 2004-12-01 2012-01-25 United Technologies Corporation Purgeur gonflable destine a un moteur a turbine et methode de reglage d'air de purge
US7980054B2 (en) * 2004-12-01 2011-07-19 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
WO2006059988A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Moteur a turbine de bout modulaire
WO2006059978A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Moteur a turbine de bout en porte-a-faux
WO2006059987A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Séparateur de particules pour moteur à turbine en bout
WO2006060001A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Rotor de ventilateur pour moteur a turbine de bout
US20090169385A1 (en) * 2004-12-01 2009-07-02 Suciu Gabriel L Fan-turbine rotor assembly with integral inducer section for a tip turbine engine
WO2006060003A2 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Pale de ventilateur comprenant une section de diffuseur integrale et une section de pale de turbine a aube destine a une moteur a turbine a aube
WO2006059989A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Structure de support de moteur a turbine de bout
WO2006059971A2 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Logement de moteur a turbine integrant un ventilateur, un combustor, et une turbine
EP1831521B1 (fr) 2004-12-01 2008-08-20 United Technologies Corporation Ensemble aubes de guidage d'admission de soufflante variable, turbomachine dotee d'un tel ensemble et procede de commande correspondant
WO2006059985A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Compresseur axial pour moteur a turbine de bout
WO2006059996A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Ailettes de rotor de soufflante pour moteur a turbine en bout
EP1834076B1 (fr) * 2004-12-01 2011-04-06 United Technologies Corporation Groupe d'aubes de turbine d'un rotor de soufflante et procédé de montage d'un tel groupe
WO2006059973A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Moteur de turbine a aube comprenant un echangeur thermique
US7874802B2 (en) * 2004-12-01 2011-01-25 United Technologies Corporation Tip turbine engine comprising turbine blade clusters and method of assembly
EP1825111B1 (fr) * 2004-12-01 2011-08-31 United Technologies Corporation Carter de compresseur à rotation inverse pour un moteur à turbine en bout
WO2006059979A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Carter intégral, aube fixe, bâti et mélangeur d'un moteur à turbine en bout
WO2006059997A2 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Elements annulaires de rotor de turbine
WO2006059974A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Ensemble de boite de vitesses a couplage proximal pour moteur de turbine a pression d'entree
US8087885B2 (en) * 2004-12-01 2012-01-03 United Technologies Corporation Stacked annular components for turbine engines
WO2006110123A2 (fr) * 2004-12-01 2006-10-19 United Technologies Corporation Conduit de transition pour moteur a turbine
US7882695B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Turbine blow down starter for turbine engine
WO2006059968A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Boite de vitesses contre-rotative pour moteur a turbine de bout
WO2006059990A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Refroidissement regeneratif des aubes et pales de turbine pour moteur a turbine d'extremite
US9845727B2 (en) 2004-12-01 2017-12-19 United Technologies Corporation Tip turbine engine composite tailcone
WO2006059994A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Ensemble de joint pour rotor de turbine-ventilateur de moteur de turbine a pression d’entree
US8083030B2 (en) * 2004-12-01 2011-12-27 United Technologies Corporation Gearbox lubrication supply system for a tip engine
DE602004028297D1 (de) * 2004-12-01 2010-09-02 United Technologies Corp Umfangsbrennkammer für spitzenturbinenmotor
US7883315B2 (en) * 2004-12-01 2011-02-08 United Technologies Corporation Seal assembly for a fan rotor of a tip turbine engine
EP1828683B1 (fr) 2004-12-01 2013-04-10 United Technologies Corporation Dispositif de combustion pour moteur de turbine
WO2006062497A1 (fr) * 2004-12-04 2006-06-15 United Technologies Corporation Bâti moteur à turbine en bout de pale
US8356469B1 (en) 2007-04-05 2013-01-22 The United States Of America As Represented By The Secretary Of The Air Force Gas turbine engine with dual compression rotor
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
US8176725B2 (en) * 2009-09-09 2012-05-15 United Technologies Corporation Reversed-flow core for a turbofan with a fan drive gear system
US20110146289A1 (en) * 2009-12-21 2011-06-23 John Lewis Baughman Power extraction method
US20110146228A1 (en) * 2009-12-21 2011-06-23 John Lewis Baughman Power extraction system
US20120324901A1 (en) * 2011-06-23 2012-12-27 United Technologies Corporation Tandem fan-turbine rotor for a tip turbine engine
US9879694B2 (en) * 2015-02-03 2018-01-30 United Technologies Corporation Turbo-compressor with geared turbofan
US10041408B2 (en) * 2015-02-13 2018-08-07 United Technologies Corporation Turbine engine with a turbo-compressor
US10100731B2 (en) 2015-02-13 2018-10-16 United Technologies Corporation Turbine engine with a turbo-compressor
US10337401B2 (en) * 2015-02-13 2019-07-02 United Technologies Corporation Turbine engine with a turbo-compressor
US10125722B2 (en) 2015-02-13 2018-11-13 United Technologies Corporation Turbine engine with a turbo-compressor
US10378438B2 (en) * 2016-04-20 2019-08-13 Rolls-Royce North American Technologies, Inc. Reverse flow gas turbine engine with radially outward turbine
US10883424B2 (en) 2016-07-19 2021-01-05 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine architecture
US11415063B2 (en) 2016-09-15 2022-08-16 Pratt & Whitney Canada Corp. Reverse-flow gas turbine engine
US10465611B2 (en) 2016-09-15 2019-11-05 Pratt & Whitney Canada Corp. Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool
US11035293B2 (en) 2016-09-15 2021-06-15 Pratt & Whitney Canada Corp. Reverse flow gas turbine engine with offset RGB
US10815899B2 (en) 2016-11-15 2020-10-27 Pratt & Whitney Canada Corp. Gas turbine engine accessories arrangement
US10655537B2 (en) * 2017-01-23 2020-05-19 General Electric Company Interdigitated counter rotating turbine system and method of operation
US10539020B2 (en) * 2017-01-23 2020-01-21 General Electric Company Two spool gas turbine engine with interdigitated turbine section
US10544734B2 (en) * 2017-01-23 2020-01-28 General Electric Company Three spool gas turbine engine with interdigitated turbine section
US10738709B2 (en) 2017-02-09 2020-08-11 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine
US10808624B2 (en) 2017-02-09 2020-10-20 Pratt & Whitney Canada Corp. Turbine rotor with low over-speed requirements
US10746188B2 (en) 2017-03-14 2020-08-18 Pratt & Whitney Canada Corp. Inter-shaft bearing connected to a compressor boost system
US10215052B2 (en) 2017-03-14 2019-02-26 Pratt & Whitney Canada Corp. Inter-shaft bearing arrangement
US10787931B2 (en) 2017-05-25 2020-09-29 General Electric Company Method and structure of interdigitated turbine engine thermal management
US10718265B2 (en) 2017-05-25 2020-07-21 General Electric Company Interdigitated turbine engine air bearing and method of operation
US10669893B2 (en) 2017-05-25 2020-06-02 General Electric Company Air bearing and thermal management nozzle arrangement for interdigitated turbine engine
US10605168B2 (en) 2017-05-25 2020-03-31 General Electric Company Interdigitated turbine engine air bearing cooling structure and method of thermal management
US10344763B2 (en) * 2017-08-28 2019-07-09 Mustafa Rez Disc turbo charger
US20190063313A1 (en) * 2017-08-28 2019-02-28 Mustafa Rez Disc Turbine Engine
CN110529250B (zh) * 2018-05-23 2022-08-02 通用电气公司 燃气涡轮发动机
US11434831B2 (en) * 2018-05-23 2022-09-06 General Electric Company Gas turbine combustor having a plurality of angled vanes circumferentially spaced within the combustor
CN110821677A (zh) 2018-08-08 2020-02-21 普拉特 - 惠特尼加拿大公司 多发动机系统和方法
US11255266B2 (en) * 2019-05-14 2022-02-22 Raytheon Technologies Corporation Recuperated cycle engine
US12158077B2 (en) * 2020-02-19 2024-12-03 Nathan Geoffrey ANDREWS Compact turbine-compressor assembly
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly
FR3155029B1 (fr) * 2023-11-03 2025-09-26 Safran Aircraft Engines Turbomachine pour aeronef

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US2085761A (en) * 1933-02-15 1937-07-06 Milo Ab Aircraft power plant
US2162956A (en) * 1933-02-16 1939-06-20 Milo Ab Aircraft power plant
US2292288A (en) * 1937-06-02 1942-08-04 Soc Es Energie Sa Means for driving the propelling system of aircraft
US2256198A (en) * 1938-05-27 1941-09-16 Ernst Heinkel Aircraft power plant
US2360130A (en) * 1941-03-26 1944-10-10 Armstrong Siddeley Motors Ltd High-speed propulsion plant
US2426098A (en) * 1942-09-03 1947-08-19 Armstrong Siddeley Motors Ltd Compound internal-combustion turbine plant
US2430399A (en) * 1942-11-05 1947-11-04 Armstrong Siddeley Motors Ltd Jet augmenter for combustion turbine propulsion plants
US2428330A (en) * 1943-01-15 1947-09-30 Armstrong Siddeley Motors Ltd Assembly of multistage internalcombustion turbines embodying contrarotating bladed members

Also Published As

Publication number Publication date
US2548975A (en) 1951-04-17

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