FR1230668A - Procédé et appareillage pour la fabrication des stratifiés chauffants, applicables notamment aux éléments de dégivrage d'avions - Google Patents
Procédé et appareillage pour la fabrication des stratifiés chauffants, applicables notamment aux éléments de dégivrage d'avionsInfo
- Publication number
- FR1230668A FR1230668A FR793001A FR793001A FR1230668A FR 1230668 A FR1230668 A FR 1230668A FR 793001 A FR793001 A FR 793001A FR 793001 A FR793001 A FR 793001A FR 1230668 A FR1230668 A FR 1230668A
- Authority
- FR
- France
- Prior art keywords
- aircraft
- applicable
- manufacture
- icing elements
- laminates
- 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
- 238000010438 heat treatment Methods 0.000 title 1
- 238000004519 manufacturing process Methods 0.000 title 1
- 238000000034 method Methods 0.000 title 1
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
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/02—Moulds or cores; Details thereof or accessories therefor with incorporated heating or cooling means
-
- 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
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
- B29C35/0272—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould using lost heating elements, i.e. heating means incorporated and remaining in the formed article
-
- 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
-
- 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
-
- 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
- B29C70/865—Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
-
- 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
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
- B29C33/54—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles made of powdered or granular material
-
- 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
- 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
- B29C70/685—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 by laminating inserts between two plastic films or plates
- B29C70/687—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 by laminating inserts between two plastic films or plates the inserts being oriented, e.g. nets or meshes
-
- 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
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
- B29L2031/3085—Wings
-
- 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
- B29L2031/779—Heating equipment
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Health & Medical Sciences (AREA)
- Oral & Maxillofacial Surgery (AREA)
- Thermal Sciences (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US1230668XA | 1958-04-24 | 1958-04-24 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR1230668A true FR1230668A (fr) | 1960-09-19 |
Family
ID=22406526
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR793001A Expired FR1230668A (fr) | 1958-04-24 | 1959-04-22 | Procédé et appareillage pour la fabrication des stratifiés chauffants, applicables notamment aux éléments de dégivrage d'avions |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR1230668A (fr) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2530538A1 (fr) * | 1982-07-24 | 1984-01-27 | Rolls Royce | Procede de fabrication d'articles en materiaux composites |
| EP0277727A1 (fr) * | 1987-01-20 | 1988-08-10 | SMITH & NEPHEW RICHARDS, INC. | Dispositif orthopédique de polymère biocompatible à renforcement de fibres orientées |
| FR2685250A1 (fr) * | 1991-12-19 | 1993-06-25 | Aerospatiale | Procede d'incorporation d'un element de rechauffage dans une structure en materiau composite. |
| US5326051A (en) * | 1992-06-30 | 1994-07-05 | The B. F. Goodrich Company | Electro-expulsive deicing system having circuit board expulsive members |
| FR2760400A1 (fr) * | 1997-03-07 | 1998-09-11 | Aerovac Systems Keighley Ltd | Membrane, sac a vide et procede de production de la membrane |
| NL1025744C2 (nl) * | 2004-03-16 | 2005-01-18 | Stork Fokker Aesp Bv | Laminaat met verwarmingselement. |
| WO2006085054A1 (fr) * | 2005-02-09 | 2006-08-17 | Qinetiq Limited | Protection de surfaces aérodynamiques contre la glace |
| FR2883796A1 (fr) * | 2005-04-05 | 2006-10-06 | Jallais Sa | Dispositif de realisation de preformes fibreuses ou autres pieces |
| WO2019186029A1 (fr) * | 2018-03-28 | 2019-10-03 | Safran | Procede de fabrication d'une aube en materiau composite a bord d'attaque metallique rapporte pour turbine a gaz. |
| CN111645337A (zh) * | 2019-03-04 | 2020-09-11 | 波音公司 | 用于制造多孔复合结构的工具组件以及相关的系统和方法 |
-
1959
- 1959-04-22 FR FR793001A patent/FR1230668A/fr not_active Expired
Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2530538A1 (fr) * | 1982-07-24 | 1984-01-27 | Rolls Royce | Procede de fabrication d'articles en materiaux composites |
| EP0277727A1 (fr) * | 1987-01-20 | 1988-08-10 | SMITH & NEPHEW RICHARDS, INC. | Dispositif orthopédique de polymère biocompatible à renforcement de fibres orientées |
| FR2685250A1 (fr) * | 1991-12-19 | 1993-06-25 | Aerospatiale | Procede d'incorporation d'un element de rechauffage dans une structure en materiau composite. |
| US5396699A (en) * | 1991-12-19 | 1995-03-14 | Aerospatiale Societe Nationale Industrielle Et Aerospatiale | Method for incorporating a heating element in a composite structure |
| US5326051A (en) * | 1992-06-30 | 1994-07-05 | The B. F. Goodrich Company | Electro-expulsive deicing system having circuit board expulsive members |
| FR2760400A1 (fr) * | 1997-03-07 | 1998-09-11 | Aerovac Systems Keighley Ltd | Membrane, sac a vide et procede de production de la membrane |
| NL1025744C2 (nl) * | 2004-03-16 | 2005-01-18 | Stork Fokker Aesp Bv | Laminaat met verwarmingselement. |
| WO2005087589A1 (fr) * | 2004-03-16 | 2005-09-22 | Stork Fokker Aesp B.V. | Stratifie avec elements chauffants |
| WO2006085054A1 (fr) * | 2005-02-09 | 2006-08-17 | Qinetiq Limited | Protection de surfaces aérodynamiques contre la glace |
| US9771158B2 (en) | 2005-02-09 | 2017-09-26 | Qinetiq Limited | Ice protection of aerodynamic surfaces |
| FR2883796A1 (fr) * | 2005-04-05 | 2006-10-06 | Jallais Sa | Dispositif de realisation de preformes fibreuses ou autres pieces |
| WO2006106195A1 (fr) * | 2005-04-05 | 2006-10-12 | Jallais | Dispositif stratifie chauffant et methode de production d' un tel dispositif |
| WO2019186029A1 (fr) * | 2018-03-28 | 2019-10-03 | Safran | Procede de fabrication d'une aube en materiau composite a bord d'attaque metallique rapporte pour turbine a gaz. |
| FR3079445A1 (fr) * | 2018-03-28 | 2019-10-04 | Safran | Procede de fabrication d'une aube en materiau composite a bord d'attaque metallique rapporte pour turbine a gaz |
| CN111936303A (zh) * | 2018-03-28 | 2020-11-13 | 赛峰集团 | 由复合材料制造用于燃气涡轮发动机的具有装配金属前缘的叶片的方法 |
| US11208904B2 (en) | 2018-03-28 | 2021-12-28 | Safran | Method for manufacturing a vane from a composite material with a fitted metal leading edge for a gas turbine |
| CN111936303B (zh) * | 2018-03-28 | 2022-10-21 | 赛峰集团 | 由复合材料制造用于燃气涡轮发动机的具有装配金属前缘的叶片的方法 |
| CN111645337A (zh) * | 2019-03-04 | 2020-09-11 | 波音公司 | 用于制造多孔复合结构的工具组件以及相关的系统和方法 |
| CN111645337B (zh) * | 2019-03-04 | 2023-09-19 | 波音公司 | 用于制造多孔复合结构的工具组件以及相关的系统和方法 |
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