FR1012335A - Perfectionnements apportés aux engins, notamment aux compresseurs axiaux, à rotor équipé de plusieurs aubages disposés en tandem - Google Patents

Perfectionnements apportés aux engins, notamment aux compresseurs axiaux, à rotor équipé de plusieurs aubages disposés en tandem

Info

Publication number
FR1012335A
FR1012335A FR1012335DA FR1012335A FR 1012335 A FR1012335 A FR 1012335A FR 1012335D A FR1012335D A FR 1012335DA FR 1012335 A FR1012335 A FR 1012335A
Authority
FR
France
Prior art keywords
tandem
machines
improvements made
blades arranged
several blades
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.)
Safran Transmission Systems SAS
Societe dExplotation des Materiels Hispano Suiza
Original Assignee
Societe dExplotation des Materiels Hispano Suiza
Hispano Suiza SA
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 Societe dExplotation des Materiels Hispano Suiza, Hispano Suiza SA filed Critical Societe dExplotation des Materiels Hispano Suiza
Application granted granted Critical
Publication of FR1012335A publication Critical patent/FR1012335A/fr
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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • F01D5/066—Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
    • 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
FR1012335D 1949-07-13 1949-07-13 Perfectionnements apportés aux engins, notamment aux compresseurs axiaux, à rotor équipé de plusieurs aubages disposés en tandem Expired FR1012335A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR833101X 1949-07-13

Publications (1)

Publication Number Publication Date
FR1012335A true FR1012335A (fr) 1952-07-08

Family

ID=9296365

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1012335D Expired FR1012335A (fr) 1949-07-13 1949-07-13 Perfectionnements apportés aux engins, notamment aux compresseurs axiaux, à rotor équipé de plusieurs aubages disposés en tandem

Country Status (5)

Country Link
US (1) US2662685A (fr)
CH (1) CH298241A (fr)
DE (1) DE833101C (fr)
FR (1) FR1012335A (fr)
GB (1) GB670942A (fr)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE507205A (fr) * 1950-12-08
GB706563A (en) * 1951-04-18 1954-03-31 Bristol Aeroplane Co Ltd Improvements in or relating to rotors for axial flow compressors or turbines
US2938705A (en) * 1955-05-26 1960-05-31 Curtiss Wright Corp Lightweight compressor or turbine structure
US2916256A (en) * 1955-09-21 1959-12-08 United Aircraft Corp Rotor construction for compressors and turbines
US2922618A (en) * 1956-03-06 1960-01-26 Gen Electric Turbo-machine rotor
US2951677A (en) * 1956-03-12 1960-09-06 Curtiss Wright Corp Turbine rotor construction
US2973938A (en) * 1958-08-18 1961-03-07 Gen Electric Cooling means for a multi-stage turbine
US3083947A (en) * 1960-03-03 1963-04-02 United Aircraft Corp Compressor spacer
US3114533A (en) * 1961-04-27 1963-12-17 Gen Electric Rotor construction
US3184153A (en) * 1962-01-18 1965-05-18 Joy Mfg Co Rotor construction
US3597110A (en) * 1969-10-23 1971-08-03 Gen Electric Joint construction
GB1291302A (en) * 1970-03-14 1972-10-04 Sec Dep For Defendence Improvements in bladed rotor assemblies
DE2140816A1 (de) * 1971-08-14 1973-03-01 Motoren Turbinen Union Rotor fuer stroemungsmaschinen
FR2607866B1 (fr) * 1986-12-03 1991-04-12 Snecma Axes de fixation de rotors de turbomachine, procede de montage et rotors ainsi montes
US4869632A (en) * 1988-03-02 1989-09-26 United Technologies Corporation Bolted connection for a turbine disk
US5388963A (en) * 1993-07-02 1995-02-14 United Technologies Corporation Flange for high speed rotors
FR2966867B1 (fr) * 2010-10-28 2015-05-29 Snecma Ensemble de disques de rotor pour une turbomachine
US9528376B2 (en) * 2012-09-13 2016-12-27 General Electric Company Compressor fairing segment
KR101872808B1 (ko) * 2017-04-28 2018-06-29 두산중공업 주식회사 길이조절구조를 포함하는 가스터빈 로터, 및 이를 포함하는 가스터빈

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US906400A (en) * 1905-12-15 1908-12-08 Sebastian Ziani De Ferranti Process for attaching turbine-blades to their carrying elements.
US852030A (en) * 1906-09-08 1907-04-30 William A Nussbaumer Elastic-fluid turbine.
US1210978A (en) * 1913-10-09 1917-01-02 Charles Algernon Parsons Construction of turbine and like rotors.
US1118361A (en) * 1914-06-19 1914-11-24 Gen Electric Wheel for elastic-fluid turbines.
US1873956A (en) * 1930-05-05 1932-08-30 Allis Chalmers Mfg Co Rotor structure
CH296109A (de) * 1941-09-08 1954-01-31 Daimler Benz Ag Trommelförmiger Schaufelträger mit mehreren Schaufelkränzen für Axialturbomaschinen.
NL66706C (fr) * 1944-10-06
US2548858A (en) * 1949-06-24 1951-04-17 Westinghouse Electric Corp Gas turbine apparatus

Also Published As

Publication number Publication date
CH298241A (fr) 1954-04-30
GB670942A (en) 1952-04-30
US2662685A (en) 1953-12-15
DE833101C (de) 1952-03-03

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