FR816937A - Perfectionnements relatifs aux hélices d'aéronautique - Google Patents

Perfectionnements relatifs aux hélices d'aéronautique

Info

Publication number
FR816937A
FR816937A FR816937DA FR816937A FR 816937 A FR816937 A FR 816937A FR 816937D A FR816937D A FR 816937DA FR 816937 A FR816937 A FR 816937A
Authority
FR
France
Prior art keywords
improvements relating
aeronautical propellers
aeronautical
propellers
relating
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Application granted granted Critical
Publication of FR816937A publication Critical patent/FR816937A/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02—Hub construction
    • B64C11/04—Blade mountings
    • B64C11/06—Blade mountings for variable-pitch blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/008—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft characterised by vibration absorbing or balancing means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02—Hub construction
    • B64C11/04—Blade mountings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10—Suppression of vibrations in rotating systems by making use of members moving with the system
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/50—Vibration damping features

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Mechanical Engineering (AREA)
  • Transmission Devices (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
FR816937D 1936-01-28 1937-01-27 Perfectionnements relatifs aux hélices d'aéronautique Expired FR816937A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US61154A US2144428A (en) 1936-01-28 1936-01-28 Aeronautical propeller having vibration controlling features

Publications (1)

Publication Number Publication Date
FR816937A true FR816937A (fr) 1937-08-20

Family

ID=22033980

Family Applications (1)

Application Number Title Priority Date Filing Date
FR816937D Expired FR816937A (fr) 1936-01-28 1937-01-27 Perfectionnements relatifs aux hélices d'aéronautique

Country Status (3)

Country Link
US (1) US2144428A (fr)
FR (1) FR816937A (fr)
GB (1) GB489648A (fr)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2447628A (en) * 1942-06-06 1948-08-24 United Aircraft Corp Propeller vibration damping means
US2425261A (en) * 1943-12-09 1947-08-05 Curtiss Wright Corp Variable pitch propeller
US2436087A (en) * 1944-12-04 1948-02-17 Ernest H Benson Cooling fan for aircraft engines
US2457609A (en) * 1945-02-08 1948-12-28 Fairey Aviat Co Ltd Pitch changing mechanism
US2783023A (en) * 1950-04-05 1957-02-26 Stalker Dev Company Fluid rotor having damping means
US2862686A (en) * 1954-08-19 1958-12-02 Thompson Prod Inc Hollow vane with internal vibration dampener
US2933286A (en) * 1954-09-15 1960-04-19 Gen Electric Damping turbine buckets
US3007654A (en) * 1956-12-27 1961-11-07 Doman Helicopters Inc Rotor and blade for rotorcraft
US2992688A (en) * 1957-02-18 1961-07-18 Hartzell Propeller Inc Adjustable pitch propeller
GB1058817A (en) * 1964-08-07 1967-02-15 Hawker Siddeley Dynamics Ltd Improvements in roller bearings, especially for aircraft propeller blades
US3966357A (en) * 1974-09-25 1976-06-29 General Electric Company Blade baffle damper
FR2474095B1 (fr) * 1980-01-17 1986-02-28 Rolls Royce Dispositif amortisseur de vibrations pour aubes mobiles de moteur a turbine a gaz
GB2165333A (en) * 1984-09-26 1986-04-09 Steven Odobasic Laminated torsion elements
US5205714A (en) * 1990-07-30 1993-04-27 General Electric Company Aircraft fan blade damping apparatus
US7270517B2 (en) * 2005-10-06 2007-09-18 Siemens Power Generation, Inc. Turbine blade with vibration damper
US10077674B2 (en) 2015-06-23 2018-09-18 General Electric Company Trunnion retention for a turbine engine
CN106081096A (zh) * 2016-07-27 2016-11-09 上海未来伙伴机器人有限公司 桨叶装置、桨叶装置制造方法以及多旋翼飞行器

Also Published As

Publication number Publication date
US2144428A (en) 1939-01-17
GB489648A (en) 1938-07-28

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