DE112013003321T5 - Gasturbinenmotor (Turbomotor) - Google Patents

Gasturbinenmotor (Turbomotor) Download PDF

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Publication number
DE112013003321T5
DE112013003321T5 DE112013003321.6T DE112013003321T DE112013003321T5 DE 112013003321 T5 DE112013003321 T5 DE 112013003321T5 DE 112013003321 T DE112013003321 T DE 112013003321T DE 112013003321 T5 DE112013003321 T5 DE 112013003321T5
Authority
DE
Germany
Prior art keywords
pressure
low
combustion chamber
turbine
compressor
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.)
Withdrawn
Application number
DE112013003321.6T
Other languages
German (de)
English (en)
Inventor
Anmelder Gleich
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of DE112013003321T5 publication Critical patent/DE112013003321T5/de
Withdrawn legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/105—Final actuators by passing part of the fluid
    • 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
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • 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
    • F02C3/107—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
    • 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
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/003—Gas-turbine plants with heaters between turbine stages
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/60—Application making use of surplus or waste energy

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Supercharger (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE112013003321.6T 2012-03-30 2013-03-26 Gasturbinenmotor (Turbomotor) Withdrawn DE112013003321T5 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
BY20120506 2012-03-30
BYA20120506 2012-03-30
PCT/BY2013/000002 WO2013142941A1 (ru) 2012-03-30 2013-03-26 Газотурбинный двигатель

Publications (1)

Publication Number Publication Date
DE112013003321T5 true DE112013003321T5 (de) 2015-11-26

Family

ID=49159270

Family Applications (1)

Application Number Title Priority Date Filing Date
DE112013003321.6T Withdrawn DE112013003321T5 (de) 2012-03-30 2013-03-26 Gasturbinenmotor (Turbomotor)

Country Status (8)

Country Link
US (1) US20150135725A1 (https=)
CA (1) CA2870615A1 (https=)
CH (1) CH708180B1 (https=)
DE (1) DE112013003321T5 (https=)
GB (1) GB2515947B (https=)
RU (1) RU2012115610A (https=)
UA (1) UA103413C2 (https=)
WO (1) WO2013142941A1 (https=)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201518929D0 (en) * 2015-10-27 2015-12-09 Rolls Royce Plc Gas turbine engine
GB2547674A (en) * 2016-02-25 2017-08-30 Rolls Royce Plc Gas turbine engine
GB201619960D0 (en) * 2016-11-25 2017-01-11 Rolls Royce Plc Gas turbine engine
US20190017437A1 (en) * 2017-07-13 2019-01-17 General Electric Company Continuous detonation gas turbine engine
CH715118A2 (de) * 2018-06-21 2019-12-30 Envita Man & Development Gmbh Stationäre Gasturbinenanlage mit parallelgeschalteten Hochdruckgasturbinen.
US11859539B2 (en) * 2021-02-01 2024-01-02 General Electric Company Aircraft propulsion system with inter-turbine burner
CN113323769A (zh) * 2021-06-07 2021-08-31 北京航空航天大学 一种基于多涵道进气级间燃烧室的变循环发动机构型
CN114576013B (zh) * 2022-03-15 2024-03-26 清华大学 用于飞行器发动机的涡轮冷却方法
US12516630B1 (en) * 2025-02-03 2026-01-06 Ge Vernova Infrastructure Technology Llc System and method for fuel injection in turbine section of gas turbine engine

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3677012A (en) * 1962-05-31 1972-07-18 Gen Electric Composite cycle turbomachinery
FR2270450A1 (en) * 1974-03-29 1975-12-05 Snecma Gas turbine with split air flow - has low pressure turbine stage crossed by main and secondary flow mixture
US4068471A (en) * 1975-06-16 1978-01-17 General Electric Company Variable cycle engine with split fan section
US4054030A (en) * 1976-04-29 1977-10-18 General Motors Corporation Variable cycle gas turbine engine
US5003766A (en) * 1984-10-10 1991-04-02 Paul Marius A Gas turbine engine
US4858428A (en) * 1986-04-24 1989-08-22 Paul Marius A Advanced integrated propulsion system with total optimized cycle for gas turbines
GB2288640B (en) * 1994-04-16 1998-08-12 Rolls Royce Plc A gas turbine engine
FR2754565B1 (fr) * 1996-10-10 1999-01-08 Hispano Suiza Sa Inverseur de poussee a portes a debit de fuite controle
US6079197A (en) * 1998-01-02 2000-06-27 Siemens Westinghouse Power Corporation High temperature compression and reheat gas turbine cycle and related method
RU2146769C1 (ru) * 1998-11-23 2000-03-20 Кубанский государственный технологический университет Газотурбинная установка
US7584598B2 (en) * 2005-08-10 2009-09-08 Alstom Technology Ltd. Method for operating a gas turbine and a gas turbine for implementing the method
US7513118B2 (en) * 2005-08-10 2009-04-07 Alstom Technology Ltd. Method for operating a gas turbine and a gas turbine for implementing the method

Also Published As

Publication number Publication date
WO2013142941A1 (ru) 2013-10-03
GB201418548D0 (en) 2014-12-03
CH708180A4 (https=) 2013-10-03
CA2870615A1 (en) 2013-10-03
GB2515947B (en) 2020-07-01
CH708180B1 (de) 2018-04-13
GB2515947A (en) 2015-01-07
UA103413C2 (en) 2013-10-10
RU2012115610A (ru) 2013-08-10
US20150135725A1 (en) 2015-05-21

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Legal Events

Date Code Title Description
R012 Request for examination validly filed
R082 Change of representative

Representative=s name: JECK - FLECK - HERRMANN PATENTANWAELTE, DE

Representative=s name: JECK - FLECK PATENTANWAELTE, DE

R084 Declaration of willingness to licence
R016 Response to examination communication
R016 Response to examination communication
R016 Response to examination communication
R016 Response to examination communication
R119 Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee