FR2434079A1 - Dispositif pour limiter les battements des pales d'un rotor principal de giravion - Google Patents

Dispositif pour limiter les battements des pales d'un rotor principal de giravion

Info

Publication number
FR2434079A1
FR2434079A1 FR7824480A FR7824480A FR2434079A1 FR 2434079 A1 FR2434079 A1 FR 2434079A1 FR 7824480 A FR7824480 A FR 7824480A FR 7824480 A FR7824480 A FR 7824480A FR 2434079 A1 FR2434079 A1 FR 2434079A1
Authority
FR
France
Prior art keywords
blades
limiting
main rotor
giravion
beats
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.)
Granted
Application number
FR7824480A
Other languages
English (en)
Other versions
FR2434079B1 (fr
Inventor
Marc Declercq
Declercq Et Gerard Margant Marc
Gerard Margant
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR7824480A priority Critical patent/FR2434079A1/fr
Priority to IT24969/79A priority patent/IT1122719B/it
Priority to GB7928229A priority patent/GB2028749B/en
Priority to JP54102867A priority patent/JPS5950559B2/ja
Priority to IN592/DEL/79A priority patent/IN154324B/en
Priority to US06/068,797 priority patent/US4289448A/en
Publication of FR2434079A1 publication Critical patent/FR2434079A1/fr
Application granted granted Critical
Publication of FR2434079B1 publication Critical patent/FR2434079B1/fr
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/322—Blade travel limiting devices, e.g. droop stops

Abstract

L'invention concerne un dispositif pour limiter les battements des pales d'un rotor principal de giravion. Ce dispositif comporte, comme butée inférieure commune, un anneau réciproque 8, et une butée supérieure pour chaque pale, comprenant par exemple un premier bras 22A1 d'un levier pivotant 22A ou 22B, rappelé, à l'arrêt du rotor, par un ressort 23A ou 23B, en appui contre une couronne fixe; en rotation rapide, la force centrifuge agissant sur une masselotte MA, portée par le second bras, 22a2, du levier 22A, le fait pivoter sur son axe 21A, dans un sens tel que la butée 22A1 est escamotée. Le dispositif selon l'invention est applicable en particulier aux rotors ayant des moyeux à bras souples.
FR7824480A 1978-08-23 1978-08-23 Dispositif pour limiter les battements des pales d'un rotor principal de giravion Granted FR2434079A1 (fr)

Priority Applications (6)

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
IT24969/79A IT1122719B (it) 1978-08-23 1979-08-07 Dispositivo per limitare glisbattimenti delle pale di un rotore principale di giroplano
GB7928229A GB2028749B (en) 1978-08-23 1979-08-14 Helicopter main rotor hub construction to limit blade flapping
JP54102867A JPS5950559B2 (ja) 1978-08-23 1979-08-14 ヘリコプタ主回転翼の羽ばたき運動制限装置
IN592/DEL/79A IN154324B (fr) 1978-08-23 1979-08-17
US06/068,797 US4289448A (en) 1978-08-23 1979-08-22 Device for limiting the flapping movements of a rotary-wing aircraft main rotor

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 (2)

Publication Number Publication Date
FR2434079A1 true FR2434079A1 (fr) 1980-03-21
FR2434079B1 FR2434079B1 (fr) 1983-01-07

Family

ID=9212027

Family Applications (1)

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

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)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2447856A1 (fr) * 1979-02-02 1980-08-29 Agusta Aeronaut Costr Rotor articule pour helicoptere
FR2523071A1 (fr) * 1982-03-11 1983-09-16 Agusta Aeronaut Costr Rotor d'helicoptere
FR2551723A1 (fr) * 1983-09-08 1985-03-15 Aerospatiale Dispositif a butees escamotables pour limiter les battements des pales d'un rotor principal de giravion
EP0706935A1 (fr) 1994-10-12 1996-04-17 Eurocopter France Dispositif de butées de battement, à anneau escamotable de butées hautes, et tête de rotor le comportant
EP2910470A1 (fr) 2014-02-21 2015-08-26 Airbus Helicopters Rotor pour giravion comportant un mécanisme de butée en battement, et giravion

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
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
WO2010068194A1 (fr) 2008-12-09 2010-06-17 Sikorsky Aircraft Corporation Butée d'avance pour système de rotor comprenant un amortisseur d'avance/de retard fluide élastomère
WO2011007850A1 (fr) * 2009-07-14 2011-01-20 豊和鋳機株式会社 Tête de rotor
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

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US2961051A (en) * 1955-11-17 1960-11-22 Wilford Edward Burke Rotor hub and drive system
FR2041762A1 (fr) * 1969-05-28 1971-02-05 Sud Aviation
FR2342892A1 (fr) * 1976-03-05 1977-09-30 Westland Aircraft Ltd Rotor d'helicoptere

Family Cites Families (9)

* 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
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
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
US3853426A (en) * 1972-09-05 1974-12-10 United Aircraft Corp Elastomeric helicopter rotor head with dynamic and static blade coning and droop stops
US4203708A (en) * 1978-06-26 1980-05-20 United Technologies Corporation Elastomeric rotor load reaction system

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US2961051A (en) * 1955-11-17 1960-11-22 Wilford Edward Burke Rotor hub and drive system
FR2041762A1 (fr) * 1969-05-28 1971-02-05 Sud Aviation
FR2342892A1 (fr) * 1976-03-05 1977-09-30 Westland Aircraft Ltd Rotor d'helicoptere

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2447856A1 (fr) * 1979-02-02 1980-08-29 Agusta Aeronaut Costr Rotor articule pour helicoptere
FR2523071A1 (fr) * 1982-03-11 1983-09-16 Agusta Aeronaut Costr Rotor d'helicoptere
FR2551723A1 (fr) * 1983-09-08 1985-03-15 Aerospatiale Dispositif a butees escamotables pour limiter les battements des pales d'un rotor principal de giravion
EP0145512A1 (fr) * 1983-09-08 1985-06-19 AEROSPATIALE Société Nationale Industrielle Dispositif à butées escamotables pour limiter les battements des pales d'un rotor principal de giravion
US4652210A (en) * 1983-09-08 1987-03-24 Societe Nationale Industrielle Aerospatiale Device incorporating retractable stops for limiting the flappings of the blades of the main rotor of a rotorcraft
EP0706935A1 (fr) 1994-10-12 1996-04-17 Eurocopter France Dispositif de butées de battement, à anneau escamotable de butées hautes, et tête de rotor le comportant
FR2725687A1 (fr) * 1994-10-12 1996-04-19 Eurocopter France Dispositif de butees de battement, a anneau escamotable de butees hautes, et tete de rotor le comportant
US5588801A (en) * 1994-10-12 1996-12-31 Eurocopter France Flap stops device with retractable upper stops ring, and rotor head including it
EP2910470A1 (fr) 2014-02-21 2015-08-26 Airbus Helicopters Rotor pour giravion comportant un mécanisme de butée en battement, et giravion
US9682775B2 (en) 2014-02-21 2017-06-20 Airbus Helicopters Rotorcraft rotor including a flapping abutment mechanism, and a rotorcraft

Also Published As

Publication number Publication date
IT1122719B (it) 1986-04-23
FR2434079B1 (fr) 1983-01-07
GB2028749B (en) 1982-06-30
IN154324B (fr) 1984-10-20
IT7924969A0 (it) 1979-08-07
JPS5950559B2 (ja) 1984-12-08
US4289448A (en) 1981-09-15
GB2028749A (en) 1980-03-12
JPS5531686A (en) 1980-03-06

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Legal Events

Date Code Title Description
CD Change of name or company name
ST Notification of lapse
CD Change of name or company name
TP Transmission of property