[go: up one dir, main page]

ATE4185T1 - Rueckhaltesystem fuer zusammenenlegbare blaetter. - Google Patents

Rueckhaltesystem fuer zusammenenlegbare blaetter.

Info

Publication number
ATE4185T1
ATE4185T1 AT80901086T AT80901086T ATE4185T1 AT E4185 T1 ATE4185 T1 AT E4185T1 AT 80901086 T AT80901086 T AT 80901086T AT 80901086 T AT80901086 T AT 80901086T AT E4185 T1 ATE4185 T1 AT E4185T1
Authority
AT
Austria
Prior art keywords
blade
retention system
restraint
elastomeric bearing
foldable sheets
Prior art date
Application number
AT80901086T
Other languages
English (en)
Inventor
Donald Leroy Ferris
Original Assignee
United Technologies Corporation
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 United Technologies Corporation filed Critical United Technologies Corporation
Application granted granted Critical
Publication of ATE4185T1 publication Critical patent/ATE4185T1/de

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/46Blades
    • B64C27/473Constructional features
    • B64C27/50Blades foldable to facilitate stowage of aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)
  • Transmission Devices (AREA)
  • Catching Or Destruction (AREA)
  • Rotary Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Nonmetal Cutting Devices (AREA)
  • Toys (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Compositions Of Oxide Ceramics (AREA)
  • Disintegrating Or Milling (AREA)
  • Cereal-Derived Products (AREA)
  • Motorcycle And Bicycle Frame (AREA)
  • Bending Of Plates, Rods, And Pipes (AREA)
  • Shaping Of Tube Ends By Bending Or Straightening (AREA)
  • Radio Relay Systems (AREA)
  • Walking Sticks, Umbrellas, And Fans (AREA)
AT80901086T 1979-05-02 1980-04-09 Rueckhaltesystem fuer zusammenenlegbare blaetter. ATE4185T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/035,364 US4284387A (en) 1979-05-02 1979-05-02 Blade fold restraint system
EP80901086A EP0027468B1 (de) 1979-05-02 1980-11-17 Rückhaltesystem für zusammenenlegbare blätter

Publications (1)

Publication Number Publication Date
ATE4185T1 true ATE4185T1 (de) 1983-08-15

Family

ID=21882218

Family Applications (1)

Application Number Title Priority Date Filing Date
AT80901086T ATE4185T1 (de) 1979-05-02 1980-04-09 Rueckhaltesystem fuer zusammenenlegbare blaetter.

Country Status (12)

Country Link
US (1) US4284387A (de)
EP (1) EP0027468B1 (de)
JP (1) JPS55148697A (de)
AT (1) ATE4185T1 (de)
AU (1) AU530102B2 (de)
BE (1) BE882683A (de)
BR (1) BR8008669A (de)
CA (1) CA1121786A (de)
DE (1) DE3064203D1 (de)
IT (1) IT1131116B (de)
NO (1) NO148145C (de)
WO (1) WO1980002408A1 (de)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1161413A (en) * 1980-10-10 1984-01-31 Roderick A. Maclennan Automatic lock-positioning of foldable helicopter blades
US5322415A (en) * 1992-11-18 1994-06-21 United Technologies Corporation Pitch actuation system restraint device for a helicopter blade folding system
FR2750948B1 (fr) * 1996-07-12 1998-10-30 Eurocopter France Dispositif de blocage, au moins en pas, des pales d'un rotor
FR2765188B1 (fr) * 1997-06-30 1999-09-17 Eurocopter France Dispositif pour le repliage d'une pale de rotor de giravion
FR2765550B1 (fr) * 1997-07-07 1999-10-01 Eurocopter France Dispositif de blocage en pas des pales d'un rotor principal de giravion
US5951252A (en) * 1997-09-12 1999-09-14 Mcdonnell Douglas Helicopter Company Helicopter flap lock assembly
US6783327B1 (en) 2002-12-12 2004-08-31 Davis Aircraft Products Co., Inc. Helicopter blade folding with blade droop
US20060067822A1 (en) * 2004-09-24 2006-03-30 D Anna Frank P Pitch lock and lag positioner for a rotor blade folding system
US20060120873A1 (en) * 2004-12-03 2006-06-08 Sikorsky Aircraft Corporation Damper positioner for a rotor blade folding system
FR2882543B1 (fr) * 2005-02-28 2008-10-10 Eurocopter France Dispositif de verrouillage d'une structure de fixation d'une pale au moyeu d'un rotor de giravion
US7798442B2 (en) * 2006-03-17 2010-09-21 Sikorsky Aircraft Corporation Rotor assemblies having automatic blade folding systems
US7530790B2 (en) * 2006-09-20 2009-05-12 Sikorsky Aircraft Corporation Rotor blade folding system
US9009938B2 (en) * 2009-04-24 2015-04-21 Rusty J. Noyes Tool for removing from or joining together a bearing and a hub
US8919692B2 (en) 2009-04-28 2014-12-30 Sikorsky Aircraft Corporation Proximity sensor valve and lock system using same
US9108727B2 (en) 2010-06-16 2015-08-18 Sikorsky Aircraft Corporation Blade fold system monitoring
DE102012206755B4 (de) 2012-04-25 2022-11-24 Zf Friedrichshafen Ag Steuerstangenanordnung
CN102768518B (zh) * 2012-07-11 2014-05-21 清华大学 多无人机平台协同控制系统
US9156545B1 (en) 2013-05-22 2015-10-13 Bell Helicopter Textron Inc. Folding of rotorcraft rotor blades
PL3218263T3 (pl) 2014-11-10 2022-07-11 Ascent Aerosystems Inc. Bezzałogowe urządzenie latające
US10287009B2 (en) * 2015-05-19 2019-05-14 Alion Science And Technology Corporation Helicopter blade folding apparatus
KR101713669B1 (ko) * 2016-03-31 2017-03-08 한국생산기술연구원 접이식 날개를 갖는 드론
FR3056554B1 (fr) * 2016-09-29 2018-08-31 Airbus Helicopters Butee d'une pale
EP4015364B1 (de) 2020-12-18 2023-09-27 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Neigungswinkelsperrvorrichtung

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2405777A (en) * 1943-03-31 1946-08-13 United Aircraft Corp Foldable rotor
US2549886A (en) * 1947-07-18 1951-04-24 United Aircraft Corp Folding rotor blade
US2925130A (en) * 1954-10-01 1960-02-16 United Aircraft Corp Means of folding rotor blades
US3153455A (en) * 1962-10-15 1964-10-20 Boeing Co Folding mechanism
US3247907A (en) * 1963-09-18 1966-04-26 Boeing Co Blade folding mechanism for rotary wing aircraft
US3282350A (en) * 1965-10-20 1966-11-01 Boeing Co Rotor blade mounting construction
US3759631A (en) * 1972-07-05 1973-09-18 United Aircraft Corp Compound bearing for connecting a helicopter blade to a helicopter rotor
US3853426A (en) * 1972-09-05 1974-12-10 United Aircraft Corp Elastomeric helicopter rotor head with dynamic and static blade coning and droop stops
US3778189A (en) * 1972-09-05 1973-12-11 United Aircraft Corp Elastomeric helicopter rotor head with dynamic and static blade coning and droop stops
US4028001A (en) * 1975-07-28 1977-06-07 Westland Aircraft Limited Rotor for rotary wing aircraft
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
AU5731880A (en) 1980-11-06
JPH0255279B2 (de) 1990-11-26
JPS55148697A (en) 1980-11-19
EP0027468A4 (de) 1981-09-01
IT8021731A0 (it) 1980-05-02
NO803955L (no) 1980-12-30
NO148145C (no) 1983-08-17
BE882683A (fr) 1980-07-31
IT1131116B (it) 1986-06-18
DE3064203D1 (en) 1983-08-25
EP0027468B1 (de) 1983-07-20
US4284387A (en) 1981-08-18
AU530102B2 (en) 1983-06-30
WO1980002408A1 (en) 1980-11-13
BR8008669A (pt) 1981-04-14
NO148145B (no) 1983-05-09
EP0027468A1 (de) 1981-04-29
CA1121786A (en) 1982-04-13

Similar Documents

Publication Publication Date Title
ATE4185T1 (de) Rueckhaltesystem fuer zusammenenlegbare blaetter.
GB981637A (en) Variable geometry system and apparatus for aircraft
SE8000362L (sv) Batpropeller med fellbara blad
SE8304281D0 (sv) Starrflugel-flugkorper
SE8403094L (sv) Varningssystem for alltfor stor hojdforlust efter start for flygplan med roterande vingar
GB1316320A (en) Rotary wing aircraft with folding rotor blades
CN208842624U (zh) 一种巡航时能够收放旋翼的垂直起降固定翼无人机
GB995061A (en) Helicopter which can be packed for transport
CN109018331A (zh) 一种巡航时能够收放旋翼的垂直起降固定翼无人机
RU96114015A (ru) Самолет короткого взлета и посадки
GB1326652A (en) Aircraft
HUBER et al. High-speed tests with the helicopter BO 105 HGH
BR8706925A (pt) Conjunto para chapeletas que operam aerodinamicamente em asas de sustentacao de aeronaves,especialmente chapeletas dobraveis
BELLEMAN et al. Design and fabrication of an aeroelastic flap element for a Short TakeOff and Landing(STOL) aircraft model[Final Report]
Nguyen et al. High angle-of-attack characteristics of three-surface fighter aircraft
Nagel Aerodynamic applications at Boeing.
BEKIRBAEV et al. The Yak-40 aircraft flight test procedures(Yak 40 aircraft flight test program, discussing airworthiness requirements, static structural, vibration and wind tunnel tests)
Horn et al. Transient thermal testing of a flight test article for high speed flight
NARK Design, development, and flight evaluation of the Boeing YC-14 USB powered lift aircraft
Shane The role of the test pilot in UAV development
FR2425380A1 (fr) Installation de commande automatique pour avion a decollage et atterrissage courts (adac)
Hodge et al. Aerospace Highlights 1981: Aeroacoustics.
Decker et al. Civil tiltrotor terminal area operations research activities
SE7907104L (sv) Skovelhjul, propeller eller liknande anordning framkallande en axial verkan
HOPKINS Regional challenge(flight test of Canadair Regional Jet)

Legal Events

Date Code Title Description
UEP Publication of translation of european patent specification
REN Ceased due to non-payment of the annual fee