IT1161533B - HELICOPTER SHOVEL - Google Patents

HELICOPTER SHOVEL

Info

Publication number
IT1161533B
IT1161533B IT68111/83A IT6811183A IT1161533B IT 1161533 B IT1161533 B IT 1161533B IT 68111/83 A IT68111/83 A IT 68111/83A IT 6811183 A IT6811183 A IT 6811183A IT 1161533 B IT1161533 B IT 1161533B
Authority
IT
Italy
Prior art keywords
helicopter
shovel
helicopter shovel
Prior art date
Application number
IT68111/83A
Other languages
Italian (it)
Other versions
IT8368111A0 (en
Inventor
Fiorenzo Mussi
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 IT68111/83A priority Critical patent/IT1161533B/en
Publication of IT8368111A0 publication Critical patent/IT8368111A0/en
Priority to DE3437942A priority patent/DE3437942C2/en
Priority to GB08426453A priority patent/GB2148820B/en
Priority to JP59222294A priority patent/JPS60166592A/en
Priority to FR8416451A priority patent/FR2554077B1/en
Application granted granted Critical
Publication of IT1161533B publication Critical patent/IT1161533B/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/473—Constructional features
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/473—Constructional features
    • B64C2027/4733—Rotor blades substantially made from particular materials
    • B64C2027/4736—Rotor blades substantially made from particular materials from composite materials
IT68111/83A 1983-10-26 1983-10-26 HELICOPTER SHOVEL IT1161533B (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
IT68111/83A IT1161533B (en) 1983-10-26 1983-10-26 HELICOPTER SHOVEL
DE3437942A DE3437942C2 (en) 1983-10-26 1984-10-17 Helicopter rotor blade
GB08426453A GB2148820B (en) 1983-10-26 1984-10-19 Helicopter rotor blades
JP59222294A JPS60166592A (en) 1983-10-26 1984-10-24 Helicopter blade
FR8416451A FR2554077B1 (en) 1983-10-26 1984-10-26 HELICOPTER BLADE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT68111/83A IT1161533B (en) 1983-10-26 1983-10-26 HELICOPTER SHOVEL

Publications (2)

Publication Number Publication Date
IT8368111A0 IT8368111A0 (en) 1983-10-26
IT1161533B true IT1161533B (en) 1987-03-18

Family

ID=11307927

Family Applications (1)

Application Number Title Priority Date Filing Date
IT68111/83A IT1161533B (en) 1983-10-26 1983-10-26 HELICOPTER SHOVEL

Country Status (5)

Country Link
JP (1) JPS60166592A (en)
DE (1) DE3437942C2 (en)
FR (1) FR2554077B1 (en)
GB (1) GB2148820B (en)
IT (1) IT1161533B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2942276B1 (en) * 2009-02-17 2017-02-10 Airbus France DAWN FOR RECEIVER OF AIRCRAFT TURBOMACHINE, THE SOUL OF WHICH IS COVERED WITH SHOCK ABSORBER MATERIAL
US10239604B2 (en) 2016-05-21 2019-03-26 Bell Helicopter Textron Inc. Structurally biased proprotor blade assembly

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2234130B1 (en) * 1973-05-14 1976-04-30 Kamov Nikolai
GB1438184A (en) * 1973-05-25 1976-06-03 Kamov N I Method of manufacturing load-carrying elements of stabilizing and steering components of aircraft
JPS5016298A (en) * 1973-05-30 1975-02-20
US3891490A (en) * 1974-06-06 1975-06-24 Raychem Corp Welded polymeric articles and process
US4083656A (en) * 1975-03-21 1978-04-11 Textron, Inc. Composite rotor blade
US4095322A (en) * 1976-08-30 1978-06-20 The Boeing Company Method of fabricating a composite aerodynamic rotorblade assembly
JPS5330599A (en) * 1976-08-30 1978-03-22 Boeing Co Aerodynamic rotary wing composite construction and method of manufacturing thereof
US4188171A (en) * 1977-08-02 1980-02-12 The Boeing Company Rotor blade internal damper

Also Published As

Publication number Publication date
DE3437942C2 (en) 1998-02-19
IT8368111A0 (en) 1983-10-26
DE3437942A1 (en) 1985-05-09
FR2554077A1 (en) 1985-05-03
GB2148820A (en) 1985-06-05
GB2148820B (en) 1987-03-25
FR2554077B1 (en) 1987-01-16
GB8426453D0 (en) 1984-11-28
JPS60166592A (en) 1985-08-29

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Legal Events

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Effective date: 19971029