FR1111000A - Improvements to axial compressors - Google Patents

Improvements to axial compressors

Info

Publication number
FR1111000A
FR1111000A FR1111000DA FR1111000A FR 1111000 A FR1111000 A FR 1111000A FR 1111000D A FR1111000D A FR 1111000DA FR 1111000 A FR1111000 A FR 1111000A
Authority
FR
France
Prior art keywords
axial compressors
compressors
axial
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
French (fr)
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
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR1111000A publication Critical patent/FR1111000A/en
Expired legal-status Critical Current

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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
FR1111000D 1953-11-06 1954-10-27 Improvements to axial compressors Expired FR1111000A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB30854/53A GB758669A (en) 1953-11-06 1953-11-06 Improvements in or relating to axial-flow compressors

Publications (1)

Publication Number Publication Date
FR1111000A true FR1111000A (en) 1956-02-20

Family

ID=10314175

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1111000D Expired FR1111000A (en) 1953-11-06 1954-10-27 Improvements to axial compressors

Country Status (4)

Country Link
US (1) US2833463A (en)
BE (1) BE533039A (en)
FR (1) FR1111000A (en)
GB (1) GB758669A (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB799896A (en) * 1955-10-21 1958-08-13 Rolls Royce Improvements in or relating to axial-flow compressors
GB845325A (en) * 1956-12-18 1960-08-17 Gen Electric Stator vane assembly for axial flow compressors
GB938189A (en) * 1960-10-29 1963-10-02 Ruston & Hornsby Ltd Improvements in the construction of turbine and compressor blade elements
US3269702A (en) * 1964-01-13 1966-08-30 United Aircraft Corp Nozzle vane assembly
US4460315A (en) * 1981-06-29 1984-07-17 General Electric Company Turbomachine rotor assembly
US4907944A (en) * 1984-10-01 1990-03-13 General Electric Company Turbomachinery blade mounting arrangement
US4688992A (en) * 1985-01-25 1987-08-25 General Electric Company Blade platform
US5141395A (en) * 1991-09-05 1992-08-25 General Electric Company Flow activated flowpath liner seal
US8128354B2 (en) * 2007-01-17 2012-03-06 Siemens Energy, Inc. Gas turbine engine
US8894370B2 (en) * 2008-04-04 2014-11-25 General Electric Company Turbine blade retention system and method
FR2978197B1 (en) * 2011-07-22 2015-12-25 Snecma TURBINE AND TURBINE TURBINE TURBINE DISPENSER HAVING SUCH A DISPENSER

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR961133A (en) * 1947-02-17 1950-05-05
US2638743A (en) * 1949-04-29 1953-05-19 Ruston & Hornsby Ltd Construction of turbine-inlet and stator elements of gas turbines

Also Published As

Publication number Publication date
US2833463A (en) 1958-05-06
GB758669A (en) 1956-10-10
BE533039A (en)

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