GB586551A - Improvements in or relating to internal combustion power turbine plant for propulsion in air - Google Patents

Improvements in or relating to internal combustion power turbine plant for propulsion in air

Info

Publication number
GB586551A
GB586551A GB13247/41A GB1324741A GB586551A GB 586551 A GB586551 A GB 586551A GB 13247/41 A GB13247/41 A GB 13247/41A GB 1324741 A GB1324741 A GB 1324741A GB 586551 A GB586551 A GB 586551A
Authority
GB
United Kingdom
Prior art keywords
air
blades
turbine
propulsion
rings
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
GB13247/41A
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.)
Metropolitan Vickers Electrical Co Ltd
Original Assignee
Metropolitan Vickers Electrical Co Ltd
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 Metropolitan Vickers Electrical Co Ltd filed Critical Metropolitan Vickers Electrical Co Ltd
Priority to GB13247/41A priority Critical patent/GB586551A/en
Publication of GB586551A publication Critical patent/GB586551A/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
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/072—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with counter-rotating, e.g. fan rotors
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-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
    • F02C3/067—Gas-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 having counter-rotating rotors
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

586,551. Gas turbines. BAUMANN, K. and METROPOLITAN-VICKERS ELECTRICAL CO., Ltd. Oct. 14, 1941, No. 13247. [Class 110 (iii)] [Also in Group XXXIII] In a gas turbine jet propulsion plant for aircraft, the exhaust of the turbine driving the air-compressor, before reaching the propulsion jet, passes through oppositely rotating rings of turbine blades on rotors which also carry aircompressor blades or air-screws. Air energized by these blades is added to the propulsion jet stream. The number of rings of turbine blades is greater than the number of rings of compressor blades or air-screws. Fig. 1 shows one of the many arrangements described which uses air-compressor blades Ia, IIa. When air-screws are used the outer casing 5 is omitted. The guiding cone 1a, which may be continued as indicated by the dotted line, may rotate with the turbine rotor III. The driving gases may be caused to pass two or three times through each rotor disc concentric rings of blades being provided for this purpose. Specifications 459,365 and 583,111 are referred to.
GB13247/41A 1941-10-14 1941-10-14 Improvements in or relating to internal combustion power turbine plant for propulsion in air Expired GB586551A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB13247/41A GB586551A (en) 1941-10-14 1941-10-14 Improvements in or relating to internal combustion power turbine plant for propulsion in air

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB13247/41A GB586551A (en) 1941-10-14 1941-10-14 Improvements in or relating to internal combustion power turbine plant for propulsion in air

Publications (1)

Publication Number Publication Date
GB586551A true GB586551A (en) 1947-03-24

Family

ID=10019485

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13247/41A Expired GB586551A (en) 1941-10-14 1941-10-14 Improvements in or relating to internal combustion power turbine plant for propulsion in air

Country Status (1)

Country Link
GB (1) GB586551A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1403485A2 (en) * 2002-09-24 2004-03-31 General Electric Company Gas turbine engine with low pressure turbine comprising counter rotatable low pressure inner and outer shaft turbines
EP1799989A1 (en) * 2004-10-07 2007-06-27 Volvo Aero Corporation Gas turbine intermediate structure and a gas turbine engine comprising the intermediate structure
EP2538020A3 (en) * 2011-06-22 2014-09-03 Kevork Nercessian Gas Turbines
CN108988573A (en) * 2017-09-27 2018-12-11 武汉宏海兴民科技有限公司 Turbine outer rotor physical power source on a kind of bullet
CN109505664A (en) * 2019-01-25 2019-03-22 中国船舶重工集团公司第七0三研究所 A kind of marine gas turbine with the double-deck adjustable guide vane can reverse power turbine
CN114211665A (en) * 2021-12-30 2022-03-22 扬州和创新材料科技有限公司 Processing equipment of imine membrane

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1403485A2 (en) * 2002-09-24 2004-03-31 General Electric Company Gas turbine engine with low pressure turbine comprising counter rotatable low pressure inner and outer shaft turbines
EP1403485A3 (en) * 2002-09-24 2005-03-16 General Electric Company Gas turbine engine with low pressure turbine comprising counter rotatable low pressure inner and outer shaft turbines
EP1799989A1 (en) * 2004-10-07 2007-06-27 Volvo Aero Corporation Gas turbine intermediate structure and a gas turbine engine comprising the intermediate structure
EP1799989A4 (en) * 2004-10-07 2014-07-09 Gkn Aerospace Sweden Ab Gas turbine intermediate structure and a gas turbine engine comprising the intermediate structure
EP2538020A3 (en) * 2011-06-22 2014-09-03 Kevork Nercessian Gas Turbines
CN108988573A (en) * 2017-09-27 2018-12-11 武汉宏海兴民科技有限公司 Turbine outer rotor physical power source on a kind of bullet
CN108988573B (en) * 2017-09-27 2024-02-27 武汉宏海兴民科技有限公司 Physical power supply of outer rotor of turbine on bullet
CN109505664A (en) * 2019-01-25 2019-03-22 中国船舶重工集团公司第七0三研究所 A kind of marine gas turbine with the double-deck adjustable guide vane can reverse power turbine
CN109505664B (en) * 2019-01-25 2023-09-08 中国船舶重工集团公司第七0三研究所 Marine gas turbine power turbine that can reverse with double-deck rotatable stator
CN114211665A (en) * 2021-12-30 2022-03-22 扬州和创新材料科技有限公司 Processing equipment of imine membrane

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