FR1085142A - Perfectionnements aux surfaces aérodynamiques et plus particulièrement aux pales d'hélicoptères - Google Patents
Perfectionnements aux surfaces aérodynamiques et plus particulièrement aux pales d'hélicoptèresInfo
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0025—Producing blades or the like, e.g. blades for turbines, propellers, or wings
- B29D99/0028—Producing blades or the like, e.g. blades for turbines, propellers, or wings hollow blades
-
- 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
- B29C70/30—Shaping 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
- B29C70/34—Shaping 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
- B29C70/342—Shaping 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
-
- 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
- B29C70/68—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
- B64C27/46—Blades
- B64C27/473—Constructional features
-
- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/10—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
- B29C43/12—Isostatic 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
- B29L2031/082—Blades, e.g. for helicopters
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Aviation & Aerospace Engineering (AREA)
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)
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 |
-
1953
- 1953-06-19 FR FR1085142D patent/FR1085142A/fr not_active Expired
Cited By (16)
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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