IT8367487A0 - Rotore per elicotteri - Google Patents

Rotore per elicotteri

Info

Publication number
IT8367487A0
IT8367487A0 IT8367487A IT6748783A IT8367487A0 IT 8367487 A0 IT8367487 A0 IT 8367487A0 IT 8367487 A IT8367487 A IT 8367487A IT 6748783 A IT6748783 A IT 6748783A IT 8367487 A0 IT8367487 A0 IT 8367487A0
Authority
IT
Italy
Prior art keywords
helicopters
rotor
Prior art date
Application number
IT8367487A
Other languages
English (en)
Other versions
IT1205404B (it
Inventor
Emilio Pariani
Original Assignee
Agusta Aeronaut Costr
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 Agusta Aeronaut Costr filed Critical Agusta Aeronaut Costr
Priority to IT67487/83A priority Critical patent/IT1205404B/it
Publication of IT8367487A0 publication Critical patent/IT8367487A0/it
Priority to DE19843415071 priority patent/DE3415071A1/de
Priority to GB08410891A priority patent/GB2139172B/en
Priority to JP59084189A priority patent/JPS6035696A/ja
Priority to US06/606,156 priority patent/US4540340A/en
Priority to FR8406997A priority patent/FR2545441B1/fr
Application granted granted Critical
Publication of IT1205404B publication Critical patent/IT1205404B/it

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/008Rotors tracking or balancing devices
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00Fluid reaction surfaces, i.e. impellers
    • Y10S416/50Vibration damping features
IT67487/83A 1983-05-05 1983-05-05 Rotore per elicotteri IT1205404B (it)

Priority Applications (6)

Application Number Priority Date Filing Date Title
IT67487/83A IT1205404B (it) 1983-05-05 1983-05-05 Rotore per elicotteri
DE19843415071 DE3415071A1 (de) 1983-05-05 1984-04-21 Hubschrauber-rotor
GB08410891A GB2139172B (en) 1983-05-05 1984-04-27 Helicopter rotor
JP59084189A JPS6035696A (ja) 1983-05-05 1984-04-27 ヘリコプター回転翼
US06/606,156 US4540340A (en) 1983-05-05 1984-05-02 Helicopter rotor
FR8406997A FR2545441B1 (fr) 1983-05-05 1984-05-04 Rotor d'helicoptere

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT67487/83A IT1205404B (it) 1983-05-05 1983-05-05 Rotore per elicotteri

Publications (2)

Publication Number Publication Date
IT8367487A0 true IT8367487A0 (it) 1983-05-05
IT1205404B IT1205404B (it) 1989-03-15

Family

ID=11302822

Family Applications (1)

Application Number Title Priority Date Filing Date
IT67487/83A IT1205404B (it) 1983-05-05 1983-05-05 Rotore per elicotteri

Country Status (6)

Country Link
US (1) US4540340A (it)
JP (1) JPS6035696A (it)
DE (1) DE3415071A1 (it)
FR (1) FR2545441B1 (it)
GB (1) GB2139172B (it)
IT (1) IT1205404B (it)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1182447B (it) * 1985-02-19 1987-10-05 Agusta Aeronaut Costr Rotore per elicotteri
EP0469510A1 (de) * 1990-07-31 1992-02-05 Androidenstiftung Lausanne Verfahren und Vorrichtung zum Ausgleich instationärer Wechselkräfte bei rotierenden Systemen
US5501434A (en) * 1994-05-10 1996-03-26 Lord Corporation Hybrid fluid and elastomer damper
US5562416A (en) * 1995-08-10 1996-10-08 Sikorsky Aircraft Corporation Helicopter rotor blade mounting assembly
US10604246B2 (en) * 2016-01-21 2020-03-31 Sikorsky Aircraft Corporation Rotorcraft rotor assemblies

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA481045A (en) * 1952-02-12 General Motors Corporation Airfoil
DE576665C (de) * 1933-05-18 Eclipse Aviat Corp Vorrichtung zum Auswuchten von Luftschrauben
US2451541A (en) * 1945-05-24 1948-10-19 United Aireraft Corp Dynamic balancer for rotor blades
US2552727A (en) * 1945-08-28 1951-05-15 United Aircraft Corp Method of balancing rotor blades
US2531598A (en) * 1946-02-04 1950-11-28 Harold T Avery Balancing means for rotating wing
US2715446A (en) * 1951-03-24 1955-08-16 Smith Corp A O Balance assembly for aircraft blades
US2947365A (en) * 1956-02-23 1960-08-02 United Aircraft Corp Means for dynamically balancing rotor blades
US2934151A (en) * 1958-02-24 1960-04-26 United Aircraft Corp Helicopter rotor
US3778189A (en) * 1972-09-05 1973-12-11 United Aircraft Corp Elastomeric helicopter rotor head with dynamic and static blade coning and droop stops
US3853426A (en) * 1972-09-05 1974-12-10 United Aircraft Corp Elastomeric helicopter rotor head with dynamic and static blade coning and droop stops
US3999888A (en) * 1975-06-25 1976-12-28 United Technologies Corporation Composite tip weight attachment
US4239455A (en) * 1978-09-11 1980-12-16 Textron, Inc. Blade-mounted centrifugal pendulum

Also Published As

Publication number Publication date
US4540340A (en) 1985-09-10
IT1205404B (it) 1989-03-15
GB2139172A (en) 1984-11-07
JPH0433679B2 (it) 1992-06-03
DE3415071A1 (de) 1984-11-08
GB8410891D0 (en) 1984-06-06
FR2545441B1 (fr) 1986-08-08
FR2545441A1 (fr) 1984-11-09
JPS6035696A (ja) 1985-02-23
GB2139172B (en) 1987-03-18

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