NL71631C - - Google Patents

Info

Publication number
NL71631C
NL71631C NL71631DA NL71631C NL 71631 C NL71631 C NL 71631C NL 71631D A NL71631D A NL 71631DA NL 71631 C NL71631 C NL 71631C
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 NL71631C publication Critical patent/NL71631C/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/16Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
    • F01D11/18Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • 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
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06Gas-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
    • 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, e.g. for aircraft
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S60/00Power plants
    • Y10S60/909Reaction motor or component composed of specific material

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
NL71631D 1946-07-30 NL71631C (US07122603-20061017-C00045.png)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US687178A US2574190A (en) 1946-07-30 1946-07-30 Turbine apparatus

Publications (1)

Publication Number Publication Date
NL71631C true NL71631C (US07122603-20061017-C00045.png)

Family

ID=24759402

Family Applications (1)

Application Number Title Priority Date Filing Date
NL71631D NL71631C (US07122603-20061017-C00045.png) 1946-07-30

Country Status (5)

Country Link
US (1) US2574190A (US07122603-20061017-C00045.png)
CH (1) CH271481A (US07122603-20061017-C00045.png)
FR (1) FR946928A (US07122603-20061017-C00045.png)
GB (1) GB624830A (US07122603-20061017-C00045.png)
NL (1) NL71631C (US07122603-20061017-C00045.png)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2994472A (en) * 1958-12-29 1961-08-01 Gen Electric Tip clearance control system for turbomachines
US3122883A (en) * 1959-11-20 1964-03-03 Thompson Ramo Wooldridge Inc Heat resistant wall structure for rocket motor nozzles and the like
US3129560A (en) * 1960-06-13 1964-04-21 Stanley P Prosen Convectively cooled rocket nozzle
US3182448A (en) * 1960-06-22 1965-05-11 Thiokol Chemical Corp Rocket motor construction
US3113429A (en) * 1961-02-14 1963-12-10 Cievite Corp Steering and speed control for jet propelled vehicles
US3137132A (en) * 1961-11-15 1964-06-16 Space Age Materials Corp Internally cooled rocket nozzle
US3251554A (en) * 1962-01-29 1966-05-17 Aerojet General Co Rocket motor nozzle
US3222862A (en) * 1962-04-12 1965-12-14 Aerojet General Co High temperature nozzle for rocket motor
US3157026A (en) * 1962-10-19 1964-11-17 Super Temp Corp Composite nozzle structure
US3210933A (en) * 1963-10-11 1965-10-12 John P Crews Nozzle
GB1089572A (en) * 1965-03-18 1967-11-01 Gen Electric Improvements in stator casing for rotating machinery
CH425341A (de) * 1965-07-23 1966-11-30 Bbc Brown Boveri & Cie Gasturbine mit Kühlung der Schaufelträger
US3754398A (en) * 1971-12-27 1973-08-28 Gen Motors Corp Thermal engine exhaust reactor with over-temperature protection
GB1548836A (en) * 1977-03-17 1979-07-18 Rolls Royce Gasturbine engine
FR2589520B1 (fr) * 1985-10-30 1989-07-28 Snecma Carter de turbomachine muni d'un accumulateur de chaleur
EP2194235A1 (de) * 2008-12-05 2010-06-09 Siemens Aktiengesellschaft Gehäusekomponente für eine Axialturbomaschine mit passiver Spaltkontrolle, Gasturbine mit der Gehäusekomponente und Verfahren zum Nachrüsten einer bestehenden Gehäusekomponente
US8726663B2 (en) * 2010-01-05 2014-05-20 General Electric Company Combined cycle system employing phase change material
GB201003634D0 (en) * 2010-03-05 2010-04-21 Rolls Royce Plc Containment casing
RU2500894C1 (ru) * 2012-04-27 2013-12-10 Николай Борисович Болотин Турбина газотурбинного двигателя
RU2519127C1 (ru) * 2013-04-24 2014-06-10 Николай Борисович Болотин Турбина газотурбинного двигателя и способ регулирования радиального зазора в турбине

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1294416A (en) * 1918-01-02 1919-02-18 Pfanstiehl Company Inc Valve and method of making the same.
US1823454A (en) * 1927-03-18 1931-09-15 Rich Tool Company Method of making a valve
US1699273A (en) * 1928-02-08 1929-01-15 Thompson Prod Inc Method of making valves
US2157610A (en) * 1937-06-29 1939-05-09 Eaton Mfg Co Valve for internal combustion engines
US2427845A (en) * 1941-07-08 1947-09-23 Fairey Aviat Co Ltd Periodically actuated jet motor
US2407164A (en) * 1944-04-15 1946-09-03 Leo B Kimball Internal-combustion turbine
FR907059A (fr) * 1946-09-20 1946-02-28 Turbine à gaz à haute température

Also Published As

Publication number Publication date
CH271481A (de) 1950-10-31
GB624830A (en) 1949-06-16
FR946928A (fr) 1949-06-17
US2574190A (en) 1951-11-06

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