DE2309404C2 - Laufschaufel für Turbotriebwerksverdichter - Google Patents

Laufschaufel für Turbotriebwerksverdichter

Info

Publication number
DE2309404C2
DE2309404C2 DE2309404A DE2309404A DE2309404C2 DE 2309404 C2 DE2309404 C2 DE 2309404C2 DE 2309404 A DE2309404 A DE 2309404A DE 2309404 A DE2309404 A DE 2309404A DE 2309404 C2 DE2309404 C2 DE 2309404C2
Authority
DE
Germany
Prior art keywords
blade
shaft
profile
rotor
blade root
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
DE2309404A
Other languages
German (de)
English (en)
Other versions
DE2309404A1 (de
Inventor
Kenneth Ronald Bristol Guy
Robert Burns Hood
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
Publication of DE2309404A1 publication Critical patent/DE2309404A1/de
Application granted granted Critical
Publication of DE2309404C2 publication Critical patent/DE2309404C2/de
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
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • 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)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE2309404A 1972-03-09 1973-02-24 Laufschaufel für Turbotriebwerksverdichter Expired DE2309404C2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1107872A GB1419381A (en) 1972-03-09 1972-03-09 Fan for gas turbine engines

Publications (2)

Publication Number Publication Date
DE2309404A1 DE2309404A1 (de) 1973-09-13
DE2309404C2 true DE2309404C2 (de) 1982-07-22

Family

ID=9979625

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2309404A Expired DE2309404C2 (de) 1972-03-09 1973-02-24 Laufschaufel für Turbotriebwerksverdichter

Country Status (6)

Country Link
US (1) US3871791A (US20050271598A1-20051208-C00001.png)
JP (1) JPS5430123B2 (US20050271598A1-20051208-C00001.png)
DE (1) DE2309404C2 (US20050271598A1-20051208-C00001.png)
FR (1) FR2175429A5 (US20050271598A1-20051208-C00001.png)
GB (1) GB1419381A (US20050271598A1-20051208-C00001.png)
IT (1) IT977572B (US20050271598A1-20051208-C00001.png)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1513338A (en) * 1976-03-26 1978-06-07 Rolls Royce Rotor blade for a gas turbine engine
US4621979A (en) * 1979-11-30 1986-11-11 United Technologies Corporation Fan rotor blades of turbofan engines
US4326836A (en) * 1979-12-13 1982-04-27 United Technologies Corporation Shroud for a rotor blade
US4682935A (en) * 1983-12-12 1987-07-28 General Electric Company Bowed turbine blade
US4595340A (en) * 1984-07-30 1986-06-17 General Electric Company Gas turbine bladed disk assembly
FR2615254A1 (fr) * 1987-05-13 1988-11-18 Snecma Aube mobile de soufflante comportant une depouille en extremite
FR2643940B1 (fr) * 1989-03-01 1991-05-17 Snecma Aube mobile de turbomachine a moment de pied compense
US5067876A (en) * 1990-03-29 1991-11-26 General Electric Company Gas turbine bladed disk
US5108261A (en) * 1991-07-11 1992-04-28 United Technologies Corporation Compressor disk assembly
US5435694A (en) * 1993-11-19 1995-07-25 General Electric Company Stress relieving mount for an axial blade
US5480284A (en) * 1993-12-20 1996-01-02 General Electric Company Self bleeding rotor blade
US6375419B1 (en) 1995-06-02 2002-04-23 United Technologies Corporation Flow directing element for a turbine engine
US6299412B1 (en) * 1999-12-06 2001-10-09 General Electric Company Bowed compressor airfoil
FR3025553B1 (fr) * 2014-09-08 2019-11-29 Safran Aircraft Engines Aube a becquet amont

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1772876A (en) * 1927-11-17 1930-08-12 Parsons Billet or blank suitable for the production of turbine blades
US1981392A (en) * 1932-12-03 1934-11-20 Manganese Bronze & Brass Compa Propeller and the like
US2193616A (en) * 1937-07-10 1940-03-12 Baumann Werner Screw propeller
US2327453A (en) * 1941-10-04 1943-08-24 Eric A F Presser Helical marine propeller
US2391623A (en) * 1943-12-08 1945-12-25 Armstrong Siddeley Motors Ltd Bladed rotor
US2421890A (en) * 1944-11-27 1947-06-10 Goetaverken Ab Turbine blade
US3012709A (en) * 1955-05-18 1961-12-12 Daimler Benz Ag Blade for axial compressors
US2974728A (en) * 1957-10-21 1961-03-14 Lennox Ind Inc Fan construction
US2999668A (en) * 1958-08-28 1961-09-12 Curtiss Wright Corp Self-balanced rotor blade
US3294364A (en) * 1962-01-02 1966-12-27 Gen Electric Rotor assembly
US3173490A (en) * 1962-07-25 1965-03-16 Hiller Aircraft Company Inc Propeller blade for vtol aircraft
US3334685A (en) * 1965-08-18 1967-08-08 Gen Electric Fluid boiling and condensing heat transfer system
GB1121194A (en) * 1967-05-01 1968-07-24 Rolls Royce Bladed rotor for a fluid flow machine
US3490852A (en) * 1967-12-21 1970-01-20 Gen Electric Gas turbine rotor bucket cooling and sealing arrangement
GB1186240A (en) * 1967-12-22 1970-04-02 Rolls Royce Improvements in Blades for Fluid Flow Machines.

Also Published As

Publication number Publication date
GB1419381A (en) 1975-12-31
FR2175429A5 (US20050271598A1-20051208-C00001.png) 1973-10-19
IT977572B (it) 1974-09-20
DE2309404A1 (de) 1973-09-13
JPS5430123B2 (US20050271598A1-20051208-C00001.png) 1979-09-28
US3871791A (en) 1975-03-18
JPS48101603A (US20050271598A1-20051208-C00001.png) 1973-12-21

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Legal Events

Date Code Title Description
OGA New person/name/address of the applicant
OD Request for examination
8125 Change of the main classification
D2 Grant after examination
8327 Change in the person/name/address of the patent owner

Owner name: ROLLS-ROYCE PLC, LONDON, GB

8339 Ceased/non-payment of the annual fee