CH485946A - Strahltriebwerk - Google Patents

Strahltriebwerk

Info

Publication number
CH485946A
CH485946A CH879267A CH879267A CH485946A CH 485946 A CH485946 A CH 485946A CH 879267 A CH879267 A CH 879267A CH 879267 A CH879267 A CH 879267A CH 485946 A CH485946 A CH 485946A
Authority
CH
Switzerland
Prior art keywords
jet engine
jet
engine
Prior art date
Application number
CH879267A
Other languages
English (en)
Inventor
Tiedeman Jr Earle Roger
Edwin Sumey Ivan
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of CH485946A publication Critical patent/CH485946A/de

Links

Classifications

    • 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
    • F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH879267A 1966-09-26 1967-06-21 Strahltriebwerk CH485946A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US58198466A 1966-09-26 1966-09-26

Publications (1)

Publication Number Publication Date
CH485946A true CH485946A (de) 1970-02-15

Family

ID=24327371

Family Applications (1)

Application Number Title Priority Date Filing Date
CH879267A CH485946A (de) 1966-09-26 1967-06-21 Strahltriebwerk

Country Status (7)

Country Link
US (1) US3433020A (de)
JP (1) JPS5019681B1 (de)
BE (1) BE700428A (de)
CH (1) CH485946A (de)
DE (1) DE1601554A1 (de)
GB (1) GB1179797A (de)
NL (1) NL6708850A (de)

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3505813A (en) * 1968-05-31 1970-04-14 Rolls Royce Turbine engine with axial load balancing means for thrust bearing
GB1217807A (en) * 1969-07-19 1970-12-31 Rolls Royce Gas turbine engine
CH557952A (de) * 1972-11-08 1975-01-15 Bbc Sulzer Turbomaschinen Gasturbinenanlage.
US3844110A (en) * 1973-02-26 1974-10-29 Gen Electric Gas turbine engine internal lubricant sump venting and pressurization system
DE2728400C2 (de) * 1977-06-24 1987-02-12 Brown, Boveri & Cie Ag, 6800 Mannheim Gasturbine
US4653267A (en) * 1983-05-31 1987-03-31 United Technologies Corporation Thrust balancing and cooling system
DE3428892A1 (de) * 1984-08-04 1986-02-13 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Schaufel- und dichtspaltoptimierungseinrichtung fuer verdichter von gasturbinentriebwerken, insbesondere gasturbinenstrahltriebwerken
US4697981A (en) * 1984-12-13 1987-10-06 United Technologies Corporation Rotor thrust balancing
US4730977A (en) * 1986-12-31 1988-03-15 General Electric Company Thrust bearing loading arrangement for gas turbine engines
US4907943A (en) * 1988-05-25 1990-03-13 United Technologies Corporation Method and apparatus for assessing thrust loads on engine bearings
US5862666A (en) * 1996-12-23 1999-01-26 Pratt & Whitney Canada Inc. Turbine engine having improved thrust bearing load control
RU2224905C2 (ru) * 2001-07-27 2004-02-27 Открытое акционерное общество "Авиадвигатель" Двухконтурный газотурбинный двигатель
DE10358625A1 (de) * 2003-12-11 2005-07-07 Rolls-Royce Deutschland Ltd & Co Kg Anordnung zur Lagerentlastung in einer Gasturbine
US8235656B2 (en) * 2009-02-13 2012-08-07 General Electric Company Catenary turbine seal systems
US8182201B2 (en) * 2009-04-24 2012-05-22 Pratt & Whitney Canada Corp. Load distribution system for gas turbine engine
US8511976B2 (en) 2010-08-02 2013-08-20 General Electric Company Turbine seal system
US8984858B2 (en) * 2010-12-30 2015-03-24 Rolls-Royce Corporation Gas turbine engine
US10119476B2 (en) * 2011-09-16 2018-11-06 United Technologies Corporation Thrust bearing system with inverted non-contacting dynamic seals for gas turbine engine
US8961127B2 (en) 2011-10-24 2015-02-24 Hamilton Sundstrand Corporation Shaft cap
US9028220B2 (en) 2011-10-24 2015-05-12 Hamilton Sundstrand Corporation Tie rod
US9188136B2 (en) 2011-10-24 2015-11-17 Hamilton Sundstrand Corporation Fan rotor with cooling holes
US8887486B2 (en) 2011-10-24 2014-11-18 Hamilton Sundstrand Corporation Ram air fan inlet housing
US9140272B2 (en) 2011-10-24 2015-09-22 Hamilton Sundstrand Corporation Ram air fan outer housing
US8882454B2 (en) 2011-10-24 2014-11-11 Hamilton Sundstrand Corporation Ram air fan bearing housing
US9267512B2 (en) 2011-10-24 2016-02-23 Hamilton Sundstrand Corporation Ram air fan diffuser with perforated side walls
US9057386B2 (en) 2011-10-24 2015-06-16 Hamilton Sundstrand Corporation Ram air fan inner housing
US20130195627A1 (en) 2012-01-27 2013-08-01 Jorn A. Glahn Thrust balance system for gas turbine engine
US9228593B2 (en) 2012-08-15 2016-01-05 Hamilton Sundstrand Corporation Ram air fan outer housing
US9556885B2 (en) 2012-08-23 2017-01-31 Hamilton Sundstrand Corporation Inlet shroud assembly
US20170184027A1 (en) * 2015-12-29 2017-06-29 General Electric Company Method and system for compressor and turbine cooling
WO2018095867A1 (en) * 2016-11-22 2018-05-31 Sulzer Management Ag Shaft seal including an upstream non-contact part, e.g. a labyrinth seal, and a downstream slinger
US10982682B2 (en) 2018-03-16 2021-04-20 Hamilton Sundstrand Corporation Fan rotor for ram air fan
CN109387370B (zh) * 2018-11-14 2023-12-22 中国空空导弹研究院 一种冲压发动机直连式高空模拟试验无轴向力进气系统
CN119801661B (zh) * 2025-01-14 2025-10-28 上海交通大学 超临界co2轴流涡轮机组及其轴向力测量和调节方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2647684A (en) * 1947-03-13 1953-08-04 Rolls Royce Gas turbine engine
GB624494A (en) * 1947-06-16 1949-06-09 Bristol Aeroplane Co Ltd Improvements in or relating to compressors
US2746671A (en) * 1950-04-14 1956-05-22 United Aircraft Corp Compressor deicing and thrust balancing arrangement
US2791090A (en) * 1952-08-05 1957-05-07 Bristol Aeroplane Co Ltd Improved cooling and lubricating arrangement for bearings of a gas turbine engine
GB759037A (en) * 1953-09-07 1956-10-10 Rolls Royce Improvements in or relating to gas turbine engines
GB805330A (en) * 1954-08-13 1958-12-03 Rolls Royce Improvements in or relating to gas-turbine engines

Also Published As

Publication number Publication date
GB1179797A (en) 1970-01-28
US3433020A (en) 1969-03-18
BE700428A (de) 1967-12-01
JPS5019681B1 (de) 1975-07-09
NL6708850A (de) 1968-03-27
DE1601554A1 (de) 1971-01-21

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Legal Events

Date Code Title Description
PL Patent ceased