DE1431148A1 - Vorrichtung zum Beiklappen von Hubschrauberdrehfluegeln - Google Patents

Vorrichtung zum Beiklappen von Hubschrauberdrehfluegeln

Info

Publication number
DE1431148A1
DE1431148A1 DE19641431148 DE1431148A DE1431148A1 DE 1431148 A1 DE1431148 A1 DE 1431148A1 DE 19641431148 DE19641431148 DE 19641431148 DE 1431148 A DE1431148 A DE 1431148A DE 1431148 A1 DE1431148 A1 DE 1431148A1
Authority
DE
Germany
Prior art keywords
folding
rotating wings
helicopter rotating
helicopter
wings
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.)
Pending
Application number
DE19641431148
Other languages
English (en)
Inventor
Mosinskis Victor S
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of DE1431148A1 publication Critical patent/DE1431148A1/de
Pending legal-status Critical Current

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

Description

Claims (1)

  1. Patentansprüche
DE19641431148 1963-09-18 1964-09-03 Vorrichtung zum Beiklappen von Hubschrauberdrehfluegeln Pending DE1431148A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US309809A US3247907A (en) 1963-09-18 1963-09-18 Blade folding mechanism for rotary wing aircraft

Publications (1)

Publication Number Publication Date
DE1431148A1 true DE1431148A1 (de) 1969-07-31

Family

ID=23199745

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19641431148 Pending DE1431148A1 (de) 1963-09-18 1964-09-03 Vorrichtung zum Beiklappen von Hubschrauberdrehfluegeln

Country Status (3)

Country Link
US (1) US3247907A (de)
DE (1) DE1431148A1 (de)
GB (1) GB1036028A (de)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3484175A (en) * 1967-10-12 1969-12-16 United Aircraft Corp Means and method of synchronously folding helicopter blades
US3438447A (en) * 1967-10-12 1969-04-15 United Aircraft Corp Dual linear output and dual rotary output actuator with redundant drive
US3749515A (en) * 1971-06-01 1973-07-31 Textron Inc Powered folding mechanism
US4284387A (en) * 1979-05-02 1981-08-18 United Technologies Corp. Blade fold restraint system
DE3272187D1 (en) * 1981-11-19 1986-08-28 Westland Plc Helicopter rotors
US5031858A (en) * 1989-11-20 1991-07-16 Bell Helicopter Textron, Inc. Apparatus and method for folding and locking rotor blades
US5322415A (en) * 1992-11-18 1994-06-21 United Technologies Corporation Pitch actuation system restraint device for a helicopter blade folding system
US5868351A (en) * 1996-05-23 1999-02-09 Bell Helicopter Textron Inc. Rotor blade stowing system
US20120134821A1 (en) * 2010-11-28 2012-05-31 Bruce Eugene Swanson Fluid Turbine Having Improved Cam and Follower Mechanism
US10301015B2 (en) * 2014-08-21 2019-05-28 Sikorsky Aircraft Corporation System for shimming blade fold angle about an axis of rotation
US11511848B2 (en) * 2020-05-20 2022-11-29 Textron Innovations Inc. Pitch-fold lock
CN114193989B (zh) * 2021-12-29 2024-02-20 广东汇天航空航天科技有限公司 折叠机构、折叠机翼以及飞行器
CN115056964B (zh) * 2022-03-16 2024-04-12 南京理工大学 一种用于空天飞行器内置式电液伺服驱动折翼机构

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB852841A (en) * 1957-12-10 1960-11-02 Westland Aircraft Ltd Improvements in or relating to rotary wing aircraft
US3153455A (en) * 1962-10-15 1964-10-20 Boeing Co Folding mechanism

Also Published As

Publication number Publication date
GB1036028A (en) 1966-07-13
US3247907A (en) 1966-04-26

Similar Documents

Publication Publication Date Title
DE1528211A1 (de) Schneidkopfanordnung
DE1555252A1 (de) Selbstsperrendes Ausgleichsgetriebe
DE1431148A1 (de) Vorrichtung zum Beiklappen von Hubschrauberdrehfluegeln
DE1427546A1 (de) Spiralbohrerschleifmaschine
DE1425952A1 (de) Wellen- oder Achszapfen fuer eine laengs eines Rollweges bewegliche Lasttragvorrichtung
DE1425029A1 (de) Selbstschmierende Gelenkverbindung
DE1431236A1 (de) Fallschirm und Verfahren zu seiner Herstellung
DE1439943A1 (de) Gleichrichteranlage
DE1427472A1 (de) Facetten-Schleifmaschine
DE1450677A1 (de) Untersetzungsgetriebe
DE1552307A1 (de) Patroneneinsatz zum Einbau in einen Koerper
DE1427551A1 (de) Bohrerschleifmaschine,insbesondere fuer konische Bohrerspitzen
DE1431177A1 (de) Flugkoerper mit gewoelbter Tragflaeche
DE1609587A1 (de) Paneel
DE1450140A1 (de) Bremse
DE1442408A1 (de) Flockungsmittel
DE1438337A1 (de) Wechselstrommaschine
DE1438566A1 (de) Polumschaltbare Drehstrom-Maschine
DE1652945A1 (de) Schleifscheibe
DE1531737A1 (de) Einrichtung auf einem Tankschiff zum Antrieb der Propellerwelle und von Hilfsmotoren
DE1577345A1 (de) Werkstueckgesteuerte Seitenkantenschleifmaschine
DE1453438A1 (de) Hydraulische Vorrichtung
DE1427698A1 (de) Vorschub- und Aufspannvorrichtung
DE1427759A1 (de) Verfahren zum Herstellen von Bordsteinen
DE1439637A1 (de) Halbleiterbauelement

Legal Events

Date Code Title Description
SH Request for examination between 03.10.1968 and 22.04.1971