FR1085142A - Perfectionnements aux surfaces aérodynamiques et plus particulièrement aux pales d'hélicoptères - Google Patents

Perfectionnements aux surfaces aérodynamiques et plus particulièrement aux pales d'hélicoptères

Info

Publication number
FR1085142A
FR1085142A FR1085142DA FR1085142A FR 1085142 A FR1085142 A FR 1085142A FR 1085142D A FR1085142D A FR 1085142DA FR 1085142 A FR1085142 A FR 1085142A
Authority
FR
France
Prior art keywords
aerodynamic surfaces
helicopter blades
helicopter
blades
aerodynamic
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
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.)
Societe Nationale des Constructions Aeronautiques du Sud Est SNCASE
Original Assignee
Societe Nationale des Constructions Aeronautiques du Sud Est SNCASE
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 Societe Nationale des Constructions Aeronautiques du Sud Est SNCASE filed Critical Societe Nationale des Constructions Aeronautiques du Sud Est SNCASE
Application granted granted Critical
Publication of FR1085142A publication Critical patent/FR1085142A/fr
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/0025Producing blades or the like, e.g. blades for turbines, propellers, or wings
    • B29D99/0028Producing blades or the like, e.g. blades for turbines, propellers, or wings hollow blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/342Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping 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
    • B29C70/446Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping 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
    • B29C70/86Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/46Blades
    • B64C27/473Constructional features
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/10Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
    • B29C43/12Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies using bags surrounding the moulding material or using membranes contacting the moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/08Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • B29L2031/082Blades, e.g. for helicopters

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR1085142D 1953-06-19 1953-06-19 Perfectionnements aux surfaces aérodynamiques et plus particulièrement aux pales d'hélicoptères Expired FR1085142A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1085142T 1953-06-19

Publications (1)

Publication Number Publication Date
FR1085142A true FR1085142A (fr) 1955-01-27

Family

ID=9612051

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1085142D Expired FR1085142A (fr) 1953-06-19 1953-06-19 Perfectionnements aux surfaces aérodynamiques et plus particulièrement aux pales d'hélicoptères

Country Status (1)

Country Link
FR (1) FR1085142A (fr)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2234130A1 (fr) * 1973-05-14 1975-01-17 Kamov Nikolai
FR2315433A1 (fr) * 1975-06-25 1977-01-21 United Technologies Corp Systeme de fixation de poids en bout de pale d'helicoptere
FR2447800A1 (fr) * 1979-02-05 1980-08-29 Westland Aircraft Ltd Procede pour produire des objets creux en une matiere plastique renforcee de fibres et objets creux ainsi obtenus
FR2477502A1 (fr) * 1980-03-07 1981-09-11 Dechaux Charles Structure de voilure tournante pour helicoptere
FR2555501A1 (fr) * 1983-11-28 1985-05-31 Septem Sa Procede de fabrication de structures rigides creuses en fibres impregnees de resine, dispositif pour sa mise en oeuvre et structure obtenue
WO2001046582A2 (fr) * 1999-12-22 2001-06-28 Aerodyn Engineering Gmbh Pale de rotor destinee a des installations d'energie eolienne
EP1539464A2 (fr) * 2002-07-30 2005-06-15 Rocky Mountain Research Inc. Procede d'assemblage d'une structure co-durcie en une seule piece
US7445744B2 (en) 1999-11-18 2008-11-04 Rocky Mountain Composites, Inc. Process for forming a single piece co-cure composite wing
US7681835B2 (en) 1999-11-18 2010-03-23 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
EP3812263A1 (fr) * 2019-10-23 2021-04-28 The Boeing Company Volet de bord de fuite ayant une structure intérieure en forme de grille

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2234130A1 (fr) * 1973-05-14 1975-01-17 Kamov Nikolai
FR2315433A1 (fr) * 1975-06-25 1977-01-21 United Technologies Corp Systeme de fixation de poids en bout de pale d'helicoptere
FR2447800A1 (fr) * 1979-02-05 1980-08-29 Westland Aircraft Ltd Procede pour produire des objets creux en une matiere plastique renforcee de fibres et objets creux ainsi obtenus
FR2477502A1 (fr) * 1980-03-07 1981-09-11 Dechaux Charles Structure de voilure tournante pour helicoptere
FR2555501A1 (fr) * 1983-11-28 1985-05-31 Septem Sa Procede de fabrication de structures rigides creuses en fibres impregnees de resine, dispositif pour sa mise en oeuvre et structure obtenue
WO1985002365A1 (fr) * 1983-11-28 1985-06-06 Septem S.A. Procede de fabrication de structures rigides creuses en fibres impregnees de resine, dispositif pour sa mise en oeuvre et structure obtenue
US7445744B2 (en) 1999-11-18 2008-11-04 Rocky Mountain Composites, Inc. Process for forming a single piece co-cure composite wing
US7681835B2 (en) 1999-11-18 2010-03-23 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
WO2001046582A3 (fr) * 1999-12-22 2001-12-27 Aerodyn Eng Gmbh Pale de rotor destinee a des installations d'energie eolienne
WO2001046582A2 (fr) * 1999-12-22 2001-06-28 Aerodyn Engineering Gmbh Pale de rotor destinee a des installations d'energie eolienne
EP1539464A2 (fr) * 2002-07-30 2005-06-15 Rocky Mountain Research Inc. Procede d'assemblage d'une structure co-durcie en une seule piece
EP1539464A4 (fr) * 2002-07-30 2006-04-19 Rocky Mountain Res Inc Procede d'assemblage d'une structure co-durcie en une seule piece
US7204951B2 (en) 2002-07-30 2007-04-17 Rocky Mountain Composites, Inc. Method of assembling a single piece co-cured structure
US7216832B2 (en) 2002-07-30 2007-05-15 Rocky Mountain Composites, Inc. Method of assembling a single piece co-cured structure
EP3812263A1 (fr) * 2019-10-23 2021-04-28 The Boeing Company Volet de bord de fuite ayant une structure intérieure en forme de grille
US11046420B2 (en) 2019-10-23 2021-06-29 The Boeing Company Trailing edge flap having a waffle grid interior structure

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