IN154324B - - Google Patents

Info

Publication number
IN154324B
IN154324B IN592/DEL/79A IN592DE1979A IN154324B IN 154324 B IN154324 B IN 154324B IN 592DE1979 A IN592DE1979 A IN 592DE1979A IN 154324 B IN154324 B IN 154324B
Authority
IN
India
Application number
IN592/DEL/79A
Other languages
English (en)
Inventor
Marc Auguste Declercq
Gerard Margant
Original Assignee
Aerospatiale
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 Aerospatiale filed Critical Aerospatiale
Publication of IN154324B publication Critical patent/IN154324B/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/322Blade travel limiting devices, e.g. droop stops

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Motorcycle And Bicycle Frame (AREA)
IN592/DEL/79A 1978-08-23 1979-08-17 IN154324B (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7824480A FR2434079A1 (fr) 1978-08-23 1978-08-23 Dispositif pour limiter les battements des pales d'un rotor principal de giravion

Publications (1)

Publication Number Publication Date
IN154324B true IN154324B (fr) 1984-10-20

Family

ID=9212027

Family Applications (1)

Application Number Title Priority Date Filing Date
IN592/DEL/79A IN154324B (fr) 1978-08-23 1979-08-17

Country Status (6)

Country Link
US (1) US4289448A (fr)
JP (1) JPS5950559B2 (fr)
FR (1) FR2434079A1 (fr)
GB (1) GB2028749B (fr)
IN (1) IN154324B (fr)
IT (1) IT1122719B (fr)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1117626B (it) * 1979-02-02 1986-02-17 Aereonautiche Giovanni Augusta Rotore articolato per elicotteri
IT1155133B (it) * 1982-03-11 1987-01-21 Agusta Aeronaut Costr Rotore per elicotteri
FR2551723B1 (fr) * 1983-09-08 1985-12-13 Aerospatiale Dispositif a butees escamotables pour limiter les battements des pales d'un rotor principal de giravion
FR2584995B1 (fr) * 1985-07-22 1987-11-13 Aerospatiale Mat-moyeu integre et tete de rotor de giravion le comportant
JP2608710B2 (ja) * 1986-12-29 1997-05-14 株式会社マキタ 電動工具用整流子電動機における配線装置
FR2725687B1 (fr) 1994-10-12 1996-12-27 Eurocopter France Dispositif de butees de battement, a anneau escamotable de butees hautes, et tete de rotor le comportant
FR2742725B1 (fr) * 1995-12-21 1998-03-06 Eurocopter France Dispositif a double anneau escamotable de butees hautes de battement, et tete de rotor le comportant
US7039220B2 (en) * 2002-08-14 2006-05-02 C-Scan, L.L.P. Methods and apparatus for the dimensional measurement of livestock using a single camera
US7744349B1 (en) * 2006-09-11 2010-06-29 Davis Aircraft Products Co., Inc. Blade flap locking for out-of-use helicopters
EP2367718B1 (fr) 2008-12-09 2018-07-11 Sikorsky Aircraft Corporation Butée d'avance pour système de rotor comprenant un amortisseur d'avance/de retard fluide élastomère
JPWO2011007850A1 (ja) * 2009-07-14 2012-12-27 豊和鋳機株式会社 ローター・ヘッド
FR3017855B1 (fr) 2014-02-21 2016-04-29 Airbus Helicopters Rotor pour giravion comportant un mecanisme de butee en battement, et giravion
FR3046778B1 (fr) * 2016-01-20 2018-01-12 Airbus Helicopters Dispositif de butee inferieur d'un rotor pour giravion, rotor de giravion et giravion
US11235870B2 (en) 2018-06-28 2022-02-01 Textron Innovations Inc. Droop ring with removable wear elements

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2151215A (en) * 1938-04-30 1939-03-21 Autogiro Co Of America Aircraft sustaining rotor
US2465674A (en) * 1945-08-07 1949-03-29 United Aircraft Corp Automatic blade droop stop
US2493869A (en) * 1946-05-30 1950-01-10 Bristol Aeroplane Co Ltd Control means for the blades of the sustaining rotor of a rotary-wing aircraft
US2742098A (en) * 1951-10-06 1956-04-17 Mcculloch Motors Corp Movement limiting means for blades of aircraft sustaining rotors
US2928478A (en) * 1955-08-03 1960-03-15 Doman Helicopters Inc Freely tilting rotor for self sustaining aircraft with erecting mechanism and the erecting mechanism
US2961051A (en) * 1955-11-17 1960-11-22 Wilford Edward Burke Rotor hub and drive system
US2946391A (en) * 1955-12-29 1960-07-26 Boeing Co Rotor blade flapping control mechanism
US2906348A (en) * 1956-12-05 1959-09-29 John W Lovegrove Anti-gust stop
US3147810A (en) * 1962-09-12 1964-09-08 Boeing Co Restraining mechanism
FR1590166A (fr) * 1968-09-27 1970-04-13
FR2041762B1 (fr) * 1969-05-28 1973-11-16 Aerospatiale
US3853426A (en) * 1972-09-05 1974-12-10 United Aircraft Corp Elastomeric helicopter rotor head with dynamic and static blade coning and droop stops
GB1514347A (en) * 1976-03-05 1978-06-14 Westland Aircraft Ltd Helicopter rotors
US4203708A (en) * 1978-06-26 1980-05-20 United Technologies Corporation Elastomeric rotor load reaction system

Also Published As

Publication number Publication date
IT1122719B (it) 1986-04-23
IT7924969A0 (it) 1979-08-07
US4289448A (en) 1981-09-15
GB2028749A (en) 1980-03-12
GB2028749B (en) 1982-06-30
JPS5531686A (en) 1980-03-06
FR2434079B1 (fr) 1983-01-07
JPS5950559B2 (ja) 1984-12-08
FR2434079A1 (fr) 1980-03-21

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