GB642621A - Improvements in or relating to an internal combustion turbine - Google Patents

Improvements in or relating to an internal combustion turbine

Info

Publication number
GB642621A
GB642621A GB10225/48A GB1022548A GB642621A GB 642621 A GB642621 A GB 642621A GB 10225/48 A GB10225/48 A GB 10225/48A GB 1022548 A GB1022548 A GB 1022548A GB 642621 A GB642621 A GB 642621A
Authority
GB
United Kingdom
Prior art keywords
relating
internal combustion
combustion turbine
gas turbine
turbine plant
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
GB10225/48A
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.)
Lockheed Corp
Original Assignee
Lockheed Aircraft Corp
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 Lockheed Aircraft Corp filed Critical Lockheed Aircraft Corp
Publication of GB642621A publication Critical patent/GB642621A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18—Lubricating arrangements
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)

Abstract

642,621. Centrifugal compressors, gas turbine plant LOCKHEED AIRCRAFT CORPORATION. Feb. 10, 1947, No. 10225/48. Convention date, June 2, 1945. Divided out of 642,585. Drawings to Specification. [Classes 110(i) and 110(iii)] In a gas turbine plant as described in Specification 642,585 the bladed compressor rotor is provided with axially extending passages through which lubricating oil or other fluid is circulated for cooling the rotor.
GB10225/48A 1945-06-02 1947-02-10 Improvements in or relating to an internal combustion turbine Expired GB642621A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US642585XA 1945-06-02 1945-06-02

Publications (1)

Publication Number Publication Date
GB642621A true GB642621A (en) 1950-09-06

Family

ID=22054658

Family Applications (2)

Application Number Title Priority Date Filing Date
GB3824/47A Expired GB642585A (en) 1945-06-02 1947-02-10 Improvements in or relating to an internal combustion turbine power plant
GB10225/48A Expired GB642621A (en) 1945-06-02 1947-02-10 Improvements in or relating to an internal combustion turbine

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB3824/47A Expired GB642585A (en) 1945-06-02 1947-02-10 Improvements in or relating to an internal combustion turbine power plant

Country Status (1)

Country Link
GB (2) GB642585A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0272151A2 (en) * 1986-12-19 1988-06-22 AlliedSignal Inc. Turbocharger bearing and lubrication system
EP3564510A1 (en) * 2018-05-03 2019-11-06 Rolls-Royce plc Oil tank including a de-aerator

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2744899C3 (en) * 1977-10-06 1982-02-11 Kernforschungsanlage Jülich GmbH, 5170 Jülich Gas turbine system for driving vehicles
GB0315894D0 (en) 2003-07-08 2003-08-13 Rolls Royce Plc Aircraft engine arrangement
FR2924188B1 (en) * 2007-11-27 2010-09-03 Thales Sa FLUID SEALED ROTATION GUIDING DEVICE
CN102979624A (en) * 2012-11-21 2013-03-20 江苏华强电力设备有限公司 Control device for baffle door of air inlet channel of combustion engine
US10036503B2 (en) * 2015-04-13 2018-07-31 United Technologies Corporation Shim to maintain gap during engine assembly
CN109404060B (en) * 2018-12-10 2024-02-02 重庆江增船舶重工有限公司 Variable geometry mixed flow turbocharger sealing structure
CN113202967B (en) * 2021-04-30 2022-10-04 中国空气动力研究与发展中心设备设计与测试技术研究所 Ultralow temperature switch valve for low temperature wind tunnel
CN114645848B (en) * 2022-03-10 2024-07-09 三门拓展真空设备有限公司 Roots vacuum pump
CN116146348B (en) * 2023-04-04 2023-06-27 成都中科翼能科技有限公司 Front pivot structure of gas generator

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0272151A2 (en) * 1986-12-19 1988-06-22 AlliedSignal Inc. Turbocharger bearing and lubrication system
EP0272151A3 (en) * 1986-12-19 1990-01-03 Allied-Signal Inc. Turbocharger bearing and lubrication system
EP3564510A1 (en) * 2018-05-03 2019-11-06 Rolls-Royce plc Oil tank including a de-aerator
US11174787B2 (en) 2018-05-03 2021-11-16 Rolls-Royce Plc Oil tank

Also Published As

Publication number Publication date
GB642585A (en) 1950-09-06

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