AR224118A1 - Un metodo para manufacturar una paleta de rotor principal de helicoptero y una paleta obtenida por dicho metodo - Google Patents

Un metodo para manufacturar una paleta de rotor principal de helicoptero y una paleta obtenida por dicho metodo

Info

Publication number
AR224118A1
AR224118A1 AR275312A AR27531279A AR224118A1 AR 224118 A1 AR224118 A1 AR 224118A1 AR 275312 A AR275312 A AR 275312A AR 27531279 A AR27531279 A AR 27531279A AR 224118 A1 AR224118 A1 AR 224118A1
Authority
AR
Argentina
Prior art keywords
pallet
manufacturing
main rotor
helicopter main
helicopter
Prior art date
Application number
AR275312A
Other languages
English (en)
Original Assignee
Textron Inc
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 Textron Inc filed Critical Textron Inc
Application granted granted Critical
Publication of AR224118A1 publication Critical patent/AR224118A1/es

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Wind Motors (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
AR275312A 1978-04-03 1979-01-26 Un metodo para manufacturar una paleta de rotor principal de helicoptero y una paleta obtenida por dicho metodo AR224118A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/893,050 US4275994A (en) 1978-04-03 1978-04-03 Roll formed blade structure

Publications (1)

Publication Number Publication Date
AR224118A1 true AR224118A1 (es) 1981-10-30

Family

ID=25400942

Family Applications (1)

Application Number Title Priority Date Filing Date
AR275312A AR224118A1 (es) 1978-04-03 1979-01-26 Un metodo para manufacturar una paleta de rotor principal de helicoptero y una paleta obtenida por dicho metodo

Country Status (12)

Country Link
US (1) US4275994A (es)
JP (1) JPS54131298A (es)
AR (1) AR224118A1 (es)
AU (1) AU521499B2 (es)
BR (1) BR7901815A (es)
CA (1) CA1101817A (es)
DE (1) DE2900834A1 (es)
ES (1) ES479237A1 (es)
FR (1) FR2421798A1 (es)
GB (1) GB2017615B (es)
IL (1) IL56979A (es)
IT (1) IT1114058B (es)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU576968B2 (en) * 1985-08-01 1988-09-08 Vergola Pty Ltd Louvre blade forming machine
SU1539865A1 (ru) * 1986-07-14 1990-01-30 Предприятие П/Я В-8803 Электрический разъем с нулевым усилием стыковки
US5782607A (en) * 1996-12-11 1998-07-21 United Technologies Corporation Replaceable ceramic blade insert
DE102007013291B4 (de) * 2007-03-16 2010-04-15 Eurocopter Deutschland Gmbh Rotorblatt für einen lagerlosen Rotor eines Drehflügelflugzeugs
JP4402160B1 (ja) * 2009-03-02 2010-01-20 山田 正明 模型回転翼航空機の回転翼、及びその回転翼の製造方法
US7976275B2 (en) * 2010-08-30 2011-07-12 General Electric Company Wind turbine rotor blade assembly having an access window and related methods
US8057189B2 (en) * 2010-12-15 2011-11-15 General Electric Company Wind turbine blade with modular leading edge
US20130199934A1 (en) * 2012-02-06 2013-08-08 United Technologies Corporation Electroformed sheath
US20160010468A1 (en) * 2013-03-01 2016-01-14 General Electric Company Composite airfoil metal leading edge assembly
EP3374262B1 (en) * 2015-11-09 2021-02-24 Sikorsky Aircraft Corporation Rotor blade structures
CN105775124A (zh) * 2016-03-08 2016-07-20 哈尔滨飞机工业集团有限责任公司 直升机主桨叶动平衡特殊调整方法
FR3070371B1 (fr) * 2017-08-31 2022-09-23 Airbus Helicopters Pale, rotor muni de cette pale et aeronef muni de ce rotor
US11046420B2 (en) * 2019-10-23 2021-06-29 The Boeing Company Trailing edge flap having a waffle grid interior structure
US11725524B2 (en) 2021-03-26 2023-08-15 General Electric Company Engine airfoil metal edge
US11767607B1 (en) 2022-07-13 2023-09-26 General Electric Company Method of depositing a metal layer on a component

Family Cites Families (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2596818A (en) * 1947-05-08 1952-05-13 Piasecki Helicopter Corp Rotor blade
US2574980A (en) * 1947-06-05 1951-11-13 Piasecki Helicopter Corp Rotary wing blade
FR1009798A (fr) * 1948-06-25 1952-06-03 Const Aeronautiques Du Ct Soc Perfectionnements à la construction des pales de voilures tournantes
US2884078A (en) * 1953-10-21 1959-04-28 Parsons Corp Rotor blade structure having spanwise reinforcing members
US3002567A (en) * 1953-10-21 1961-10-03 Parsons Corp Spar for sustaining rotors
US2884077A (en) * 1953-10-21 1959-04-28 Parsons Corp Rotor blade having a gap-bonded aft structure and method of fabricating same
FR1113837A (fr) * 1953-10-21 1956-04-04 Parsons Corp Voilure rotative sustentatrice, notamment pour hélicoptères
GB744437A (en) * 1953-10-29 1956-02-08 Bristol Aeroplane Co Ltd Improvements in or relating to rotor blades for helicopters and like rotary wing aircraft
US2965530A (en) * 1954-08-18 1960-12-20 Parsons Corp Method for joining dissimilar materials
US2828531A (en) * 1955-06-21 1958-04-01 Cyril Bath Co Method of making a helicopter blade
US2863513A (en) * 1955-12-12 1958-12-09 Bell Aircraft Corp Helicopter rotor blade
US3200477A (en) * 1962-11-21 1965-08-17 Enstrom Corp Helicopter tail rotor structure and method of construction
US3217807A (en) * 1964-08-28 1965-11-16 Bell Aerospace Corp Rotor blade
GB1150123A (en) * 1967-02-08 1969-04-30 Westland Aircraft Ltd Improvements in or relating to the Construction of Rotor Blades for Rotary Wing Aircraft
GB1214858A (en) * 1968-05-20 1970-12-09 Westland Aircraft Ltd Improvements in or relating to the construction of rotor blades for rotary wing aircraft
US3528753A (en) * 1968-06-14 1970-09-15 United Aircraft Corp Helicopter blade with non-homogeneous structural spar
US3674379A (en) * 1969-01-30 1972-07-04 Siai Marchetti Spa Helicopter rotor blade
US3829240A (en) * 1971-05-17 1974-08-13 Textron Inc Advanced geometry main rotor blade
US3799700A (en) * 1971-05-17 1974-03-26 Textron Inc Main rotor blade construction
AU459383B2 (en) * 1971-05-17 1975-03-27 Textron Inc. Advanced geometry main rotor blade
US3813186A (en) * 1972-10-10 1974-05-28 Textron Inc Rotor blade shear reinforcement
FR2234130B1 (es) * 1973-05-14 1976-04-30 Kamov Nikolai
JPS5016298A (es) * 1973-05-30 1975-02-20
US4022546A (en) * 1974-01-03 1977-05-10 Textron, Inc. Helicopter rotor blade
US3874820A (en) * 1974-04-08 1975-04-01 United Aircraft Corp Hingeless in-plane rotor blade design
GB1537380A (en) * 1976-05-06 1978-12-29 Westland Aircraft Ltd Fibre-reinforced plastics structures
US4095322A (en) * 1976-08-30 1978-06-20 The Boeing Company Method of fabricating a composite aerodynamic rotorblade assembly
US4150920A (en) * 1977-12-02 1979-04-24 The United States Of America As Represented By The Secretary Of The Army Rotor blade tipweight assembly

Also Published As

Publication number Publication date
GB2017615A (en) 1979-10-10
DE2900834C2 (es) 1988-05-19
GB2017615B (en) 1982-04-21
AU4329979A (en) 1979-10-18
BR7901815A (pt) 1979-11-20
IT1114058B (it) 1986-01-27
FR2421798A1 (fr) 1979-11-02
ES479237A1 (es) 1979-12-01
FR2421798B1 (es) 1983-10-21
DE2900834A1 (de) 1979-10-04
AU521499B2 (en) 1982-04-08
JPS54131298A (en) 1979-10-12
CA1101817A (en) 1981-05-26
US4275994A (en) 1981-06-30
IL56979A (en) 1983-10-31
IT7947859A0 (it) 1979-02-01

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