CH258674A - Combustion turbine unit. - Google Patents

Combustion turbine unit.

Info

Publication number
CH258674A
CH258674A CH258674DA CH258674A CH 258674 A CH258674 A CH 258674A CH 258674D A CH258674D A CH 258674DA CH 258674 A CH258674 A CH 258674A
Authority
CH
Switzerland
Prior art keywords
turbine unit
combustion turbine
combustion
unit
turbine
Prior art date
Application number
Other languages
German (de)
Inventor
Limited Rolls-Royce
Original Assignee
Rolls Royce
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=9867397&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=CH258674(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Rolls Royce filed Critical Rolls Royce
Publication of CH258674A publication Critical patent/CH258674A/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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)
CH258674D 1946-03-25 1948-08-18 Combustion turbine unit. CH258674A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9203/46A GB610113A (en) 1946-03-25 1946-03-25 Improvements in or relating to gas-turbine engines

Publications (1)

Publication Number Publication Date
CH258674A true CH258674A (en) 1948-12-15

Family

ID=9867397

Family Applications (1)

Application Number Title Priority Date Filing Date
CH258674D CH258674A (en) 1946-03-25 1948-08-18 Combustion turbine unit.

Country Status (5)

Country Link
US (1) US2494821A (en)
BE (1) BE487120A (en)
CH (1) CH258674A (en)
FR (1) FR943932A (en)
GB (1) GB610113A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1218800B (en) * 1961-04-25 1966-06-08 M A N Turbo Ges Mit Beschraenk Gas turbine, in particular small gas turbine
DE102010001059A1 (en) * 2010-01-20 2011-07-21 Rolls-Royce Deutschland Ltd & Co KG, 15827 Intermediate housing for a gas turbine engine

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2711074A (en) * 1944-06-22 1955-06-21 Gen Electric Aft frame and rotor structure for combustion gas turbine
BE487768A (en) * 1947-03-14
US2789787A (en) * 1949-10-22 1957-04-23 Svenska Turbinfab Ab Guide blade device for steam or gas turbines
US2608057A (en) * 1949-12-24 1952-08-26 A V Roe Canada Ltd Gas turbine nozzle box
US2763462A (en) * 1950-01-11 1956-09-18 Gen Motors Corp Turbine casing construction
US2609176A (en) * 1950-01-21 1952-09-02 A V Roe Canada Ltd Turbine nozzle guide vane construction
US2654566A (en) * 1950-02-11 1953-10-06 A V Roe Canada Ltd Turbine nozzle guide vane construction
US2747367A (en) * 1950-03-21 1956-05-29 United Aircraft Corp Gas turbine power plant supporting structure
US2699040A (en) * 1950-05-23 1955-01-11 Gen Motors Corp Detachable combustion chamber for gas turbines
US2780174A (en) * 1951-03-19 1957-02-05 Solar Aircraft Co Pump and power plant assembly
US2702454A (en) * 1951-06-07 1955-02-22 United Aircraft Corp Transition piece providing a connection between the combustion chambers and the turbine nozzle in gas turbine power plants
US2848191A (en) * 1951-11-03 1958-08-19 A V Roe Canada Ltd Nozzle box
US2839894A (en) * 1952-12-31 1958-06-24 Gen Motors Corp Supporting arrangement for a gas turbine combustion chamber
US2825285A (en) * 1953-12-28 1958-03-04 Belton A Copp Centrifugal pump with discharge manifold
NL99435C (en) * 1957-08-22
US4573315A (en) * 1984-05-15 1986-03-04 A/S Kongsberg Vapenfabrikk Low pressure loss, convectively gas-cooled inlet manifold for high temperature radial turbine
US6116013A (en) * 1998-01-02 2000-09-12 Siemens Westinghouse Power Corporation Bolted gas turbine combustor transition coupling
GB0618991D0 (en) 2006-09-27 2006-11-08 Rolls Royce Plc A component for a gas turbine engine
US9021783B2 (en) * 2012-10-12 2015-05-05 United Technologies Corporation Pulse detonation engine having a scroll ejector attenuator
US9470422B2 (en) 2013-10-22 2016-10-18 Siemens Energy, Inc. Gas turbine structural mounting arrangement between combustion gas duct annular chamber and turbine vane carrier
US9810434B2 (en) * 2016-01-21 2017-11-07 Siemens Energy, Inc. Transition duct system with arcuate ceramic liner for delivering hot-temperature gases in a combustion turbine engine
US10465642B2 (en) 2017-03-27 2019-11-05 Kohler Co. Carburetor drain
CN113154456B (en) * 2021-04-15 2022-06-21 中国航发湖南动力机械研究所 Head structure of casing of backflow combustion chamber, manufacturing method of head structure and engine combustion chamber
CN115288804B (en) * 2022-10-10 2023-03-24 中国航发四川燃气涡轮研究院 Bird skeleton bionic force-bearing structure and design method thereof

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2432359A (en) * 1947-12-09 Internal-combustion turbine power
GB588082A (en) * 1941-08-25 1947-05-14 Power Jets Ltd Improvements relating to engines
GB579331A (en) * 1943-07-13 1946-07-31 Francis Robert Bell Improvements in combustion chambers for power-gas-generators, internal-combustion turbines and the like

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1218800B (en) * 1961-04-25 1966-06-08 M A N Turbo Ges Mit Beschraenk Gas turbine, in particular small gas turbine
DE102010001059A1 (en) * 2010-01-20 2011-07-21 Rolls-Royce Deutschland Ltd & Co KG, 15827 Intermediate housing for a gas turbine engine
US8857193B2 (en) 2010-01-20 2014-10-14 Rolls-Royce Deutschland Ltd & Co Kg Intermediate casing for a gas-turbine engine

Also Published As

Publication number Publication date
BE487120A (en)
FR943932A (en) 1949-03-22
US2494821A (en) 1950-01-17
GB610113A (en) 1948-10-12

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