FR943932A - Perfectionnements aux turbines à combustion interne - Google Patents

Perfectionnements aux turbines à combustion interne

Info

Publication number
FR943932A
FR943932A FR943932DA FR943932A FR 943932 A FR943932 A FR 943932A FR 943932D A FR943932D A FR 943932DA FR 943932 A FR943932 A FR 943932A
Authority
FR
France
Prior art keywords
internal combustion
combustion turbines
turbines
internal
combustion
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
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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=FR943932(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR943932A publication Critical patent/FR943932A/fr
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)
FR943932D 1946-03-25 1947-03-24 Perfectionnements aux turbines à combustion interne Expired FR943932A (fr)

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
FR943932A true FR943932A (fr) 1949-03-22

Family

ID=9867397

Family Applications (1)

Application Number Title Priority Date Filing Date
FR943932D Expired FR943932A (fr) 1946-03-25 1947-03-24 Perfectionnements aux turbines à combustion interne

Country Status (5)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113154456A (zh) * 2021-04-15 2021-07-23 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

Families Citing this family (25)

* 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 (fr) * 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
NL230456A (fr) * 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
GB0618991D0 (en) 2006-09-27 2006-11-08 Rolls Royce Plc A component for a gas turbine engine
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
US10465642B2 (en) 2017-03-27 2019-11-05 Kohler Co. Carburetor drain
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 (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113154456A (zh) * 2021-04-15 2021-07-23 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
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

Also Published As

Publication number Publication date
GB610113A (en) 1948-10-12
BE487120A (fr)
US2494821A (en) 1950-01-17
CH258674A (de) 1948-12-15

Similar Documents

Publication Publication Date Title
FR943932A (fr) Perfectionnements aux turbines à combustion interne
FR942325A (fr) Perfectionnements aux turbines à combustion interne
FR944168A (fr) Perfectionnements aux chambres de combustion pour turbines à combustion interne
CH268647A (fr) Turbine à combustion interne.
FR992440A (fr) Perfectionnements apportés aux moteurs à combustion interne
FR924012A (fr) Perfectionnement apporté aux turbines à combustion
FR946056A (fr) Perfectionnements aux aubes de turbines à combustion interne
FR943203A (fr) Perfectionnements aux turbo-moteurs à combustion interne destinés à la propulsion
FR937311A (fr) Turbine à combustion interne
FR1010954A (fr) Perfectionnements aux turbomoteurs
FR994935A (fr) Perfectionnements apportés aux machines avec turbines à combustion interne
FR937915A (fr) Perfectionnements apportés aux moteurs à combustion interne
FR57751E (fr) Perfectionnements aux moteurs à combustion interne
FR1108703A (fr) Perfectionnements aux moteurs à combustion
FR947832A (fr) Moteur à combustion interne
FR928351A (fr) Turbine à combustion
FR939576A (fr) Perfectionnements aux moteurs à combustion interne
FR995417A (fr) Perfectionnements apportés aux moteurs à combustion interne
FR57688E (fr) Turbine à combustion interne
FR951819A (fr) Perfectionnements aux moteurs à combustion interne
FR57654E (fr) Perfectionnements aux moteurs à combustion interne
FR57901E (fr) Perfectionnements aux moteurs à combustion interne
FR948671A (fr) Perfectionnements apportés aux moteurs à combustion interne
FR950774A (fr) Moteur à combustion interne
FR1001549A (fr) Turbo-moteur à combustion interne