FR1376305A - Dispositif de liaison feuilleté, travaillant à la traction et à la torsion, son montage et son mode de fabrication, utilisé notamment pour la fixation des pales au moyeu tournant d'un hélicoptère - Google Patents

Dispositif de liaison feuilleté, travaillant à la traction et à la torsion, son montage et son mode de fabrication, utilisé notamment pour la fixation des pales au moyeu tournant d'un hélicoptère

Info

Publication number
FR1376305A
FR1376305A FR956140A FR956140A FR1376305A FR 1376305 A FR1376305 A FR 1376305A FR 956140 A FR956140 A FR 956140A FR 956140 A FR956140 A FR 956140A FR 1376305 A FR1376305 A FR 1376305A
Authority
FR
France
Prior art keywords
helicopter
traction
torsion
blades
manufacture
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.)
Expired
Application number
FR956140A
Other languages
English (en)
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.)
Bendix Corp
Original Assignee
Bendix Corp
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
Priority to US150455A priority Critical patent/US3460628A/en
Application filed by Bendix Corp filed Critical Bendix Corp
Priority to FR956140A priority patent/FR1376305A/fr
Priority to GB8083/64A priority patent/GB1045723A/en
Priority claimed from GB8083/64A external-priority patent/GB1045723A/en
Application granted granted Critical
Publication of FR1376305A publication Critical patent/FR1376305A/fr
Priority to US496429A priority patent/US3434899A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C7/00—Connecting-rods or like links pivoted at both ends; Construction of connecting-rod heads
    • F16C7/02—Constructions of connecting-rods with constant length
    • F16C7/026—Constructions of connecting-rods with constant length made of fibre reinforced resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/59—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical
    • B64C27/605—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including swash plate, spider or cam mechanisms
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
    • F16B2200/40—Clamping arrangements where clamping parts are received in recesses of elements to be connected
    • F16B2200/403—Threaded clamping parts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00—Articles relating to transporting
    • F16C2326/43—Aeroplanes; Helicopters
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/34—Branched
    • Y10T403/341—Three or more radiating members
    • Y10T403/342—Polyhedral
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/45—Flexibly connected rigid members
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • Y10T428/24994—Fiber embedded in or on the surface of a polymeric matrix
    • Y10T428/249942—Fibers are aligned substantially parallel

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR956140A 1961-11-06 1963-12-05 Dispositif de liaison feuilleté, travaillant à la traction et à la torsion, son montage et son mode de fabrication, utilisé notamment pour la fixation des pales au moyeu tournant d'un hélicoptère Expired FR1376305A (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US150455A US3460628A (en) 1961-11-06 1961-11-06 Laminated tension-torsion tie-bar
FR956140A FR1376305A (fr) 1961-11-06 1963-12-05 Dispositif de liaison feuilleté, travaillant à la traction et à la torsion, son montage et son mode de fabrication, utilisé notamment pour la fixation des pales au moyeu tournant d'un hélicoptère
GB8083/64A GB1045723A (en) 1961-11-06 1964-02-26 Improvements in or relating to force transmitting members
US496429A US3434899A (en) 1961-11-06 1965-10-15 Laminated coupling

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US15045561A 1961-11-06 1961-11-06
FR956140A FR1376305A (fr) 1961-11-06 1963-12-05 Dispositif de liaison feuilleté, travaillant à la traction et à la torsion, son montage et son mode de fabrication, utilisé notamment pour la fixation des pales au moyeu tournant d'un hélicoptère
GB8083/64A GB1045723A (en) 1961-11-06 1964-02-26 Improvements in or relating to force transmitting members

Publications (1)

Publication Number Publication Date
FR1376305A true FR1376305A (fr) 1964-10-23

Family

ID=29407296

Family Applications (1)

Application Number Title Priority Date Filing Date
FR956140A Expired FR1376305A (fr) 1961-11-06 1963-12-05 Dispositif de liaison feuilleté, travaillant à la traction et à la torsion, son montage et son mode de fabrication, utilisé notamment pour la fixation des pales au moyeu tournant d'un hélicoptère

Country Status (2)

Country Link
US (1) US3460628A (fr)
FR (1) FR1376305A (fr)

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US3571492A (en) * 1969-03-25 1971-03-16 Us Navy R.f. high voltage insulation link
US3520637A (en) * 1969-07-24 1970-07-14 Boeing Co Torsion-tension coupling
US3926536A (en) * 1970-10-15 1975-12-16 Westland Aircraft Ltd Semi-rigid rotor systems for rotary wing aircraft
US3945628A (en) * 1973-12-26 1976-03-23 Textron Inc. Nodal beam inertial flexure
US4059247A (en) * 1976-09-15 1977-11-22 Prewitt Richard H Convertiblade
US4158397A (en) * 1978-01-09 1979-06-19 Reynolds Richard F Basic cyclecar frame
DE2918028C2 (de) * 1979-05-04 1981-05-07 Audi Nsu Auto Union Ag, 7107 Neckarsulm Verfahren zum Anbringen eines Pleuels auf dem Hubzapfen einer einteiligen Kurbelwelle und Vorrichtung zur Durchführung des Verfahrens
US4973372A (en) * 1984-08-29 1990-11-27 Allied-Signal Inc. Method of making a tie-bar with internal lubrication
DE3567513D1 (en) * 1984-08-29 1989-02-16 Allied Signal Inc Tie-bar with internal lubrication
US4873889A (en) * 1984-08-29 1989-10-17 Allied-Signal Inc. Tie bar with internal lubrication
US4695227A (en) * 1985-02-27 1987-09-22 Hughes Helicopters Inc. All composite, constant speed universal joint for use in a shaft driven tiltable main rotor for a helicopter
US5215616A (en) * 1986-03-14 1993-06-01 Envirex Inc. Method for manufacturing a high strength, non-metallic transmission chain
US4978413A (en) * 1989-07-25 1990-12-18 Hughes Aircraft Company In-line filament cleaner and adhesive applicator
US5768847A (en) * 1995-05-15 1998-06-23 Policelli; Frederick J. Concrete reinforcing devices, concrete reinforced structures, and method of and apparatus for producing such devices and structures
DE19738621C2 (de) * 1997-09-04 2001-09-13 Daimler Chrysler Ag Wellengelenk
GB2380984B (en) * 2001-10-15 2003-08-27 Boyce Spars Holdings Ltd A method of manufacturing an elongate structural member and a method of rigging a boat
US8303248B2 (en) * 2005-10-05 2012-11-06 Sikorsky Aircraft Corporation Swash plate anti-torque mechanism
BE1016960A3 (nl) 2006-01-19 2007-11-06 Rostyne Alexander Jozef Magdal Verbeterde helikopter.
US8002604B2 (en) 2006-01-19 2011-08-23 Silverlit Limited Remote controlled toy helicopter
US7883392B2 (en) 2008-08-04 2011-02-08 Silverlit Toys Manufactory Ltd. Toy helicopter
US8357023B2 (en) 2006-01-19 2013-01-22 Silverlit Limited Helicopter
US7815482B2 (en) 2006-01-19 2010-10-19 Silverlit Toys Manufactory, Ltd. Helicopter
US20090047861A1 (en) * 2006-01-19 2009-02-19 Silverlit Toys Manufactory Ltd. Remote controlled toy helicopter
US20070181742A1 (en) * 2006-01-19 2007-08-09 Silverlit Toys Manufactory, Ltd. Flying object with tandem rotors
US7662013B2 (en) 2006-01-19 2010-02-16 Silverlit Toys Manufactory Ltd. Helicopter with horizontal control
US8235665B2 (en) * 2008-08-07 2012-08-07 The Boeing Company Sculptured throat spool
DE102011013050A1 (de) * 2011-03-04 2012-09-06 SGF SüDDEUTSCHE GELENKSCHEIBENFABRIK GMBH & CO. KG Fadenversteifte Axialkupplung
GB2491129B (en) * 2011-05-23 2014-04-23 Blue Bear Systems Res Ltd Air vehicle
US20150308473A1 (en) * 2012-11-14 2015-10-29 Saab Ab Fastening means and attachment assembly
US9487291B2 (en) 2012-12-05 2016-11-08 The Boeing Company Apparatus, system, and method for pitching and twisting a blade of a rotorcraft
US9533754B2 (en) 2014-04-19 2017-01-03 The Boeing Company Wing aerial refueling system
EP3177525B1 (fr) * 2014-08-08 2020-03-11 Sikorsky Aircraft Corporation Plaque de flexion pour ensemble rotor
US11242690B2 (en) * 2018-01-19 2022-02-08 Titcomb Brothers Manufacturing, Inc. Loop tie for concrete forming panel systems
US10907365B2 (en) * 2018-01-19 2021-02-02 Titcomb Brothers Manufacturing, Inc. Loop tie for concrete forming panel systems

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FR568951A (fr) * 1923-07-23 1924-04-04 Perfectionnements dans les hélices à pas variable
US2073852A (en) * 1935-05-31 1937-03-16 Caterpillar Tractor Co Drive connecting link
US2369876A (en) * 1942-09-03 1945-02-20 Jr Richard F Warren Inorganic fiber rope
US2443239A (en) * 1944-01-31 1948-06-15 Greenwood Ida Controllable pitch propeller
US2478953A (en) * 1945-07-30 1949-08-16 Lester M Tint Adjustable power coupling
US2530520A (en) * 1946-09-17 1950-11-21 Everel Propeller Corp Propeller hub
GB752815A (en) * 1953-02-24 1956-07-18 Eduard Erhardt Universal joints
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US2977748A (en) * 1955-05-18 1961-04-04 William A Zisman Lubricated wire rope
US2814581A (en) * 1955-08-08 1957-11-26 Gen Electric Self-supporting electromagnetic coil
US2961051A (en) * 1955-11-17 1960-11-22 Wilford Edward Burke Rotor hub and drive system
US2949965A (en) * 1957-10-15 1960-08-23 Bell Helicopter Corp Rotor hub
US3025205A (en) * 1958-01-30 1962-03-13 Hercules Powder Co Ltd Filament delivery systems and methods
US3056706A (en) * 1958-07-16 1962-10-02 Proman Inc High lineal strength member and method of making same
US2985222A (en) * 1958-09-25 1961-05-23 Bjorksten Res Lab Inc Method of making a v-belt
US2983305A (en) * 1959-01-12 1961-05-09 Nat Plastic Products Co Bonding panels to base surfaces
US2992469A (en) * 1959-05-14 1961-07-18 Lindsay Wire Weaving Co Fourdrinier wire cloth
US3026942A (en) * 1959-07-07 1962-03-27 Bell Helicopter Corp Helicopter rotor system
US3080268A (en) * 1959-09-28 1963-03-05 Smith Corp A O Lightweight structural panel and method of making the same

Also Published As

Publication number Publication date
US3460628A (en) 1969-08-12

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