DE2332435A1 - Verbindungseinrichtung - Google Patents

Verbindungseinrichtung

Info

Publication number
DE2332435A1
DE2332435A1 DE2332435A DE2332435A DE2332435A1 DE 2332435 A1 DE2332435 A1 DE 2332435A1 DE 2332435 A DE2332435 A DE 2332435A DE 2332435 A DE2332435 A DE 2332435A DE 2332435 A1 DE2332435 A1 DE 2332435A1
Authority
DE
Germany
Prior art keywords
belt
jacket
connecting device
pressure
deformable
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
DE2332435A
Other languages
German (de)
English (en)
Inventor
Richard J Ditlinger
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
Application filed by Bendix Corp filed Critical Bendix Corp
Publication of DE2332435A1 publication Critical patent/DE2332435A1/de
Pending 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
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/56—Winding and joining, e.g. winding spirally
    • B29C53/564—Winding and joining, e.g. winding spirally for making non-tubular articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/56—Tensioning reinforcements before or during shaping
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/327—Retention means relieving the stress from the arm, e.g. tie-bars
    • 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
    • Y10T74/00—Machine element or mechanism
    • Y10T74/21—Elements
    • Y10T74/2142—Pitmans and connecting rods

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Devices For Conveying Motion By Means Of Endless Flexible Members (AREA)
  • Ropes Or Cables (AREA)
  • Springs (AREA)
DE2332435A 1972-06-26 1973-06-26 Verbindungseinrichtung Pending DE2332435A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US26601272A 1972-06-26 1972-06-26

Publications (1)

Publication Number Publication Date
DE2332435A1 true DE2332435A1 (de) 1974-01-17

Family

ID=23012807

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2332435A Pending DE2332435A1 (de) 1972-06-26 1973-06-26 Verbindungseinrichtung

Country Status (7)

Country Link
US (1) US3768334A (enExample)
JP (1) JPS4950697A (enExample)
CA (1) CA961465A (enExample)
DE (1) DE2332435A1 (enExample)
FR (1) FR2191644A5 (enExample)
GB (1) GB1378263A (enExample)
IT (1) IT989466B (enExample)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0098739A1 (en) * 1982-07-01 1984-01-18 Dunlop Limited Improvements in or relating to link means
US4542567A (en) * 1982-09-30 1985-09-24 The Boeing Company Method of fabricating a helicopter rotor hub
US4776076A (en) * 1982-09-30 1988-10-11 Boeing Company Method of fabricating a rotor hub of composite material
US4868962A (en) * 1982-09-30 1989-09-26 The Boeing Company Method of fabricating a helicopter rotor system

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2951111C2 (de) * 1979-12-19 1983-10-13 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Pleuelstange für Kraftmaschinen
US4300410A (en) * 1980-01-04 1981-11-17 Ford Motor Company Tension-compression member
US4377386A (en) * 1980-08-22 1983-03-22 Lord Corporation Link coupling
DE3340817C2 (de) * 1983-11-11 1986-05-15 Akzo Gmbh, 5600 Wuppertal Pleuel-Kolben-Anordnung für Zylinder-Kolben-Motoren
US4841801A (en) * 1987-03-25 1989-06-27 Trw Inc. Connecting rod
DE3805245A1 (de) * 1988-02-19 1989-08-31 Roblon As Kraftuebertragungsband
JP3021047B2 (ja) * 1991-08-02 2000-03-15 ザ、ボーイング、カンパニー トルク反作用および片揺れ姿勢制御を成す回転翼型航空機のダクト尾部回転翼
EP0597038B1 (en) 1991-08-02 1999-01-20 The Boeing Company Ducted fan and pitch controls for tail rotor of rotary wing aircraft
FR2762267B1 (fr) * 1997-04-16 1999-06-04 Mavic Sa Ame d'un rayon pour roue a rayons, rayon et roue de bicyclette
US6205873B1 (en) * 1997-09-12 2001-03-27 Unisys Corporation Transmit motion via flexures
FR2784622B1 (fr) * 1998-10-15 2000-12-29 Mavic Sa Rayon composite pour une roue de bicyclette et son procede de fabrication
FR2792251B1 (fr) * 1999-04-16 2001-07-27 Mavic Sa Rayon realise en materiau composite pour une roue, et roue de bicyclette equipee desdits rayons
US20050016001A1 (en) 2003-06-24 2005-01-27 Milwaukee Electric Tool Corporation Drive mechanism and power tool
GB2426545B (en) * 2005-05-26 2007-07-18 Siemens Magnet Technology Ltd Compact support system using low aspect ratio composite support bands
US8544361B2 (en) * 2011-09-06 2013-10-01 Blair Hsm Composites Llc Composite link fitting
CN117104504A (zh) * 2023-09-06 2023-11-24 株洲时代橡塑元件开发有限责任公司 一种降低拉扭条扭转刚度的方法

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3279278A (en) * 1964-04-24 1966-10-18 Bendix Corp Tension-torsion tie-bar and end fittings therefor
US3411379A (en) * 1967-03-13 1968-11-19 Bendix Corp Multiple loop tie-bar

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0098739A1 (en) * 1982-07-01 1984-01-18 Dunlop Limited Improvements in or relating to link means
US4552035A (en) * 1982-07-01 1985-11-12 Dunlop Limited Reinforced connecting link means
US4542567A (en) * 1982-09-30 1985-09-24 The Boeing Company Method of fabricating a helicopter rotor hub
US4776076A (en) * 1982-09-30 1988-10-11 Boeing Company Method of fabricating a rotor hub of composite material
US4868962A (en) * 1982-09-30 1989-09-26 The Boeing Company Method of fabricating a helicopter rotor system

Also Published As

Publication number Publication date
GB1378263A (en) 1974-12-27
US3768334A (en) 1973-10-30
CA961465A (en) 1975-01-21
IT989466B (it) 1975-05-20
JPS4950697A (enExample) 1974-05-16
FR2191644A5 (enExample) 1974-02-01

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