FR2822749B1 - Procede de fabrication d'un arbre d'entrainement tubulaire rigide en torsion et en flexion - Google Patents

Procede de fabrication d'un arbre d'entrainement tubulaire rigide en torsion et en flexion

Info

Publication number
FR2822749B1
FR2822749B1 FR0204058A FR0204058A FR2822749B1 FR 2822749 B1 FR2822749 B1 FR 2822749B1 FR 0204058 A FR0204058 A FR 0204058A FR 0204058 A FR0204058 A FR 0204058A FR 2822749 B1 FR2822749 B1 FR 2822749B1
Authority
FR
France
Prior art keywords
torsion
bending
drive shaft
rigid tubular
tubular drive
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 - Lifetime
Application number
FR0204058A
Other languages
English (en)
Other versions
FR2822749A1 (fr
Inventor
Anton Bergmann
Marinus Sedlmeier
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.)
Airbus Helicopters Deutschland GmbH
Original Assignee
Eurocopter Deutschland GmbH
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 claimed from DE10205657A external-priority patent/DE10205657C2/de
Application filed by Eurocopter Deutschland GmbH filed Critical Eurocopter Deutschland GmbH
Publication of FR2822749A1 publication Critical patent/FR2822749A1/fr
Application granted granted Critical
Publication of FR2822749B1 publication Critical patent/FR2822749B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F16C3/00—Shafts; Axles; Cranks; Eccentrics
    • F16C3/02—Shafts; Axles
    • F16C3/026—Shafts 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
    • 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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
    • 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
    • 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
    • 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
    • B29C53/566—Winding and joining, e.g. winding spirally for making tubular articles followed by compression
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S464/00—Rotary shafts, gudgeons, housings, and flexible couplings for rotary shafts
    • Y10S464/902—Particular material
    • Y10S464/903—Nonmetal
    • 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
    • Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
    • Y10T428/1352—Polymer or resin containing [i.e., natural or synthetic]
    • Y10T428/1369—Fiber or fibers wound around each other or into a self-sustaining shape [e.g., yarn, braid, fibers shaped around a core, etc.]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • General Engineering & Computer Science (AREA)
  • Ocean & Marine Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
FR0204058A 2001-04-03 2002-04-02 Procede de fabrication d'un arbre d'entrainement tubulaire rigide en torsion et en flexion Expired - Lifetime FR2822749B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10116478 2001-04-03
DE10205657A DE10205657C2 (de) 2001-04-03 2002-02-12 Verfahren zur Herstellung einer rohrförmigen, torsions-und biegesteifen Antriebswelle

Publications (2)

Publication Number Publication Date
FR2822749A1 FR2822749A1 (fr) 2002-10-04
FR2822749B1 true FR2822749B1 (fr) 2005-03-11

Family

ID=26008991

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0204058A Expired - Lifetime FR2822749B1 (fr) 2001-04-03 2002-04-02 Procede de fabrication d'un arbre d'entrainement tubulaire rigide en torsion et en flexion

Country Status (3)

Country Link
US (1) US6835263B2 (fr)
FR (1) FR2822749B1 (fr)
IT (1) ITMI20020486A1 (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BR0117299B1 (pt) 2000-03-03 2014-11-25 Quickstep Technologies Pty Ltd Métodos para unir componentes compósitos
EP1365908B1 (fr) * 2001-01-25 2014-09-10 Quickstep Technologies Pty, Ltd Système et méthode de production de pièce composite ou de liaison de composants metalliques
US20050257847A1 (en) * 2004-05-24 2005-11-24 Alenia Aeronautica S.P.A. Multi-layer duct for air distribution in air conditioning systems for vehicles, in particular aircrafts, and an element for fixing the duct to the structure of an aircraft
AU2006227545B2 (en) * 2005-03-22 2010-12-02 Quickstep Technologies Pty Ltd Composite tube production
CA2601843C (fr) * 2005-03-22 2013-11-26 Quickstep Technologies Pty Ltd Production de tube composite
NZ565042A (en) * 2005-07-05 2009-10-30 Quickstep Technologies Pty Ltd Composite component production using fluid density and pressure
DE102008022377B4 (de) * 2008-05-06 2014-02-13 Eurocopter Deutschland Gmbh Stützstrebe zur Abstützung eines in einem Flugzeugrumpf angeordneten Zwischendecks sowie Verfahren zur Herstellung eines Stangenkörpers für eine solche Stützstrebe
EP2293417B1 (fr) * 2009-09-05 2016-07-06 Grundfos Management A/S Pale de rotor
BRPI1003150A2 (pt) * 2010-08-17 2012-05-02 Marco Antonio Rodrigues De Souza processo para fabricação de estrutura compósita utilizando enrolamento filamentar com resinas termoplásticas
DE102011109362A1 (de) * 2011-08-04 2013-02-07 Thyssen Krupp Bilstein Suspension GmbH Stoßdämpfer für ein Fahrzeug in Leichtbauweise
CN104228291B (zh) * 2014-08-08 2017-01-11 苏州苏净船用机械有限公司 一种重型螺旋桨轴包覆玻璃钢的工装
FR3033139B1 (fr) * 2015-02-27 2017-03-31 Faurecia Automotive Composites Procede de fabrication de profile creux en materiaux composites
CN111745999A (zh) * 2020-06-12 2020-10-09 陕西飞机工业（集团）有限公司 一种带r角复合材料件的外观加工方法

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3148102A (en) * 1960-08-24 1964-09-08 Debell & Richardson Inc Method for the manufacture of multifilament glass tapes
SE317915B (fr) 1968-05-08 1969-11-24 Akerlund & Rausing Ab
GB1304015A (fr) * 1969-04-30 1973-01-24
US4089190A (en) * 1976-04-14 1978-05-16 Union Carbide Corporation Carbon fiber drive shaft
US4174243A (en) * 1977-07-25 1979-11-13 Ameron, Inc. Method and apparatus for wiping resin from filament wound pipe
US4171626A (en) * 1978-03-27 1979-10-23 Celanese Corporation Carbon fiber reinforced composite drive shaft
DE3822417A1 (de) 1987-07-15 1989-01-26 Man Technologie Gmbh Welle zur uebertragung von torsionskraeften
US5076871A (en) * 1990-01-11 1991-12-31 The Boeing Company Method of forming composite prepreg articles utilizing heat-shrinkable braided sleeves
US5208051A (en) 1990-11-02 1993-05-04 Massachusetts Institute Of Technology Helical tooling for consolidation of thermoplastic composite tubes
US5474630A (en) * 1991-10-31 1995-12-12 Gkn Glaenzer Spicer Process for manufacturing a transmission shaft made of a composite material and shaft manufactured according to the process
JP3232117B2 (ja) * 1991-11-19 2001-11-26 鐘淵化学工業株式会社 ポリスルホン多孔質中空糸

Also Published As

Publication number Publication date
US20020160138A1 (en) 2002-10-31
FR2822749A1 (fr) 2002-10-04
ITMI20020486A0 (it) 2002-03-08
US6835263B2 (en) 2004-12-28
ITMI20020486A1 (it) 2003-09-08

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Legal Events

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Owner name: AIRBUS HELOCOPTERS DEUTSCHLAND GMBH, DE

Effective date: 20141024

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