GB610113A - Improvements in or relating to gas-turbine engines - Google Patents

Improvements in or relating to gas-turbine engines

Info

Publication number
GB610113A
GB610113A GB9203/46A GB920346A GB610113A GB 610113 A GB610113 A GB 610113A GB 9203/46 A GB9203/46 A GB 9203/46A GB 920346 A GB920346 A GB 920346A GB 610113 A GB610113 A GB 610113A
Authority
GB
United Kingdom
Prior art keywords
ring
turbine
compressor
combustion chambers
casing
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.)
Expired
Application number
GB9203/46A
Other languages
English (en)
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
Family has litigation
Priority to BE487120D priority Critical patent/BE487120A/xx
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=GB610113(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Individual filed Critical Individual
Priority to GB9203/46A priority patent/GB610113A/en
Priority to US733912A priority patent/US2494821A/en
Priority to FR943932D priority patent/FR943932A/fr
Priority to CH258674D priority patent/CH258674A/de
Publication of GB610113A publication Critical patent/GB610113A/en
Expired legal-status Critical Current

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)
GB9203/46A 1946-03-25 1946-03-25 Improvements in or relating to gas-turbine engines Expired GB610113A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
BE487120D BE487120A (enrdf_load_stackoverflow) 1946-03-25
GB9203/46A GB610113A (en) 1946-03-25 1946-03-25 Improvements in or relating to gas-turbine engines
US733912A US2494821A (en) 1946-03-25 1947-03-11 Means for supporting the nozzles of the combustion chambers of internal-combustion turbines
FR943932D FR943932A (fr) 1946-03-25 1947-03-24 Perfectionnements aux turbines à combustion interne
CH258674D CH258674A (de) 1946-03-25 1948-08-18 Verbrennungs-Turbinenaggregat.

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
GB610113A true GB610113A (en) 1948-10-12

Family

ID=9867397

Family Applications (1)

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

Country Status (5)

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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2442300A (en) * 2006-09-27 2008-04-02 Rolls Royce Plc Sheet material gas turbine engine casing components
US10465642B2 (en) 2017-03-27 2019-11-05 Kohler Co. Carburetor drain

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
FR963256A (enrdf_load_stackoverflow) * 1947-03-14 1950-07-05
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
BE570533A (enrdf_load_stackoverflow) * 1957-08-22
DE1218800B (de) * 1961-04-25 1966-06-08 M A N Turbo Ges Mit Beschraenk Gasturbine, insbesondere Kleingasturbine
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
DE102010001059A1 (de) * 2010-01-20 2011-07-21 Rolls-Royce Deutschland Ltd & Co KG, 15827 Zwischengehäuse für ein Gasturbinentriebwerk
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
CN113154456B (zh) * 2021-04-15 2022-06-21 中国航发湖南动力机械研究所 回流燃烧室机匣头部结构及其制造方法和发动机燃烧室
CN115288804B (zh) * 2022-10-10 2023-03-24 中国航发四川燃气涡轮研究院 一种鸟类骨架仿生式承力结构及其设计方法

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 (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2442300A (en) * 2006-09-27 2008-04-02 Rolls Royce Plc Sheet material gas turbine engine casing components
GB2442300B (en) * 2006-09-27 2009-01-28 Rolls Royce Plc Casing for a gas turbine engine
US8057170B2 (en) 2006-09-27 2011-11-15 Rolls-Royce Plc Intermediate casing for a gas turbine engine
US10465642B2 (en) 2017-03-27 2019-11-05 Kohler Co. Carburetor drain

Also Published As

Publication number Publication date
US2494821A (en) 1950-01-17
FR943932A (fr) 1949-03-22
BE487120A (enrdf_load_stackoverflow)
CH258674A (de) 1948-12-15

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