BE608937A - Rotor for turbo-fan - Google Patents

Rotor for turbo-fan

Info

Publication number
BE608937A
BE608937A BE608937A BE608937A BE608937A BE 608937 A BE608937 A BE 608937A BE 608937 A BE608937 A BE 608937A BE 608937 A BE608937 A BE 608937A BE 608937 A BE608937 A BE 608937A
Authority
BE
Belgium
Prior art keywords
turbo
rotor
fan
Prior art date
Application number
BE608937A
Other languages
French (fr)
Inventor
Harry Josiah Kent
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 BE608937A publication Critical patent/BE608937A/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • 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
    • F01D5/022—Blade-carrying members, e.g. rotors with concentric rows of axial blades
    • 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
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE608937A 1960-10-07 1961-10-06 Rotor for turbo-fan BE608937A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US61248A US3070284A (en) 1960-10-07 1960-10-07 Turbo-fan rotor

Publications (1)

Publication Number Publication Date
BE608937A true BE608937A (en) 1962-02-01

Family

ID=22034583

Family Applications (1)

Application Number Title Priority Date Filing Date
BE608937A BE608937A (en) 1960-10-07 1961-10-06 Rotor for turbo-fan

Country Status (3)

Country Link
US (1) US3070284A (en)
BE (1) BE608937A (en)
GB (1) GB950527A (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3404831A (en) * 1966-12-07 1968-10-08 Gen Electric Turbine bucket supporting structure
GB1118898A (en) * 1967-04-03 1968-07-03 Rolls Royce Fluid flow machine
GB2192237B (en) * 1986-07-02 1990-05-16 Rolls Royce Plc Gas turbine engine power turbine
US5108259A (en) * 1988-12-19 1992-04-28 General Electric Company Flexible connector for use in aircraft
US6454535B1 (en) 2000-10-31 2002-09-24 General Electric Company Blisk
US20160245087A1 (en) * 2013-10-03 2016-08-25 Franco Tosi Meccanica S.P.A. Rotor stage of axial turbine with improved chord/pitch ratio
US10119403B2 (en) 2014-02-13 2018-11-06 United Technologies Corporation Mistuned concentric airfoil assembly and method of mistuning same
GB2571176B (en) * 2017-12-14 2022-07-20 Safran Aircraft Engines Damping device
CN110439623B (en) * 2019-08-14 2024-05-14 上海两擎机电科技合伙企业(有限合伙) Metal edging for aircraft engine fan blade, machining tool and machining method

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA584125A (en) * 1959-09-29 E. Moss Charles Blading for gas turbine engines
US2429681A (en) * 1942-02-27 1947-10-28 Griffith Alan Arnold Thrust balancing construction for turbines, compressors, and the like
US2391623A (en) * 1943-12-08 1945-12-25 Armstrong Siddeley Motors Ltd Bladed rotor
US2518660A (en) * 1944-09-07 1950-08-15 Wright Aeronautical Corp Internal-combustion engine and exhaust gas turbine therefor
US2625365A (en) * 1949-02-26 1953-01-13 Curtiss Wright Corp Shrouded impeller
US2868439A (en) * 1954-05-07 1959-01-13 Goodyear Aircraft Corp Plastic axial-flow compressor for gas turbines
US2819870A (en) * 1955-04-18 1958-01-14 Oleh A Wayne Sheet metal blade base

Also Published As

Publication number Publication date
GB950527A (en) 1964-02-26
US3070284A (en) 1962-12-25

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