FR1230668A - Process and apparatus for the manufacture of heating laminates, applicable in particular to aircraft de-icing elements - Google Patents
Process and apparatus for the manufacture of heating laminates, applicable in particular to aircraft de-icing elementsInfo
- 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
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; ARRANGEMENTS 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
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 (en) | 1960-09-19 |
Family
ID=22406526
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR793001A Expired FR1230668A (en) | 1958-04-24 | 1959-04-22 | Process and apparatus for the manufacture of heating laminates, applicable in particular to aircraft de-icing elements |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1230668A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2530538A1 (en) * | 1982-07-24 | 1984-01-27 | Rolls Royce | PROCESS FOR MANUFACTURING ARTICLES OF COMPOSITE MATERIALS |
EP0277727A1 (en) * | 1987-01-20 | 1988-08-10 | SMITH & NEPHEW RICHARDS, INC. | Orthopedic device of biocompatible polymer with oriented fiber reinforcement |
FR2685250A1 (en) * | 1991-12-19 | 1993-06-25 | Aerospatiale | Method of incorporating a heating element in a structure made of composite material |
US5326051A (en) * | 1992-06-30 | 1994-07-05 | The B. F. Goodrich Company | Electro-expulsive deicing system having circuit board expulsive members |
FR2760400A1 (en) * | 1997-03-07 | 1998-09-11 | Aerovac Systems Keighley Ltd | MEMBRANE, VACUUM BAG AND PROCESS FOR PRODUCING MEMBRANE |
NL1025744C2 (en) * | 2004-03-16 | 2005-01-18 | Stork Fokker Aesp Bv | Laminate with metal layers, used for aerospace applications, contains electrical heating layer |
WO2006085054A1 (en) * | 2005-02-09 | 2006-08-17 | Qinetiq Limited | Ice protection of aerodynamic surfaces |
FR2883796A1 (en) * | 2005-04-05 | 2006-10-06 | Jallais Sa | Preformed fiber producing device comprises a polymeric resin puncher integrated to an electric heating system with an electric resistant cable circuit, which is insulated by a sheath |
WO2019186029A1 (en) * | 2018-03-28 | 2019-10-03 | Safran | Method for manufacturing a vane from a composite material with a fitted metal leading edge for a gas turbine |
CN111645337A (en) * | 2019-03-04 | 2020-09-11 | 波音公司 | Tool assembly for manufacturing porous composite structures and related systems and methods |
-
1959
- 1959-04-22 FR FR793001A patent/FR1230668A/en not_active Expired
Cited By (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2530538A1 (en) * | 1982-07-24 | 1984-01-27 | Rolls Royce | PROCESS FOR MANUFACTURING ARTICLES OF COMPOSITE MATERIALS |
EP0277727A1 (en) * | 1987-01-20 | 1988-08-10 | SMITH & NEPHEW RICHARDS, INC. | Orthopedic device of biocompatible polymer with oriented fiber reinforcement |
FR2685250A1 (en) * | 1991-12-19 | 1993-06-25 | Aerospatiale | Method of incorporating a heating element in a structure made of composite material |
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 (en) * | 1997-03-07 | 1998-09-11 | Aerovac Systems Keighley Ltd | MEMBRANE, VACUUM BAG AND PROCESS FOR PRODUCING MEMBRANE |
NL1025744C2 (en) * | 2004-03-16 | 2005-01-18 | Stork Fokker Aesp Bv | Laminate with metal layers, used for aerospace applications, contains electrical heating layer |
WO2005087589A1 (en) * | 2004-03-16 | 2005-09-22 | Stork Fokker Aesp B.V. | Laminate with heating element |
WO2006085054A1 (en) * | 2005-02-09 | 2006-08-17 | Qinetiq Limited | Ice protection of aerodynamic surfaces |
US9771158B2 (en) | 2005-02-09 | 2017-09-26 | Qinetiq Limited | Ice protection of aerodynamic surfaces |
FR2883796A1 (en) * | 2005-04-05 | 2006-10-06 | Jallais Sa | Preformed fiber producing device comprises a polymeric resin puncher integrated to an electric heating system with an electric resistant cable circuit, which is insulated by a sheath |
WO2006106195A1 (en) * | 2005-04-05 | 2006-10-12 | Jallais | Laminated heating device and method for producing same |
WO2019186029A1 (en) * | 2018-03-28 | 2019-10-03 | Safran | Method for manufacturing a vane from a composite material with a fitted metal leading edge for a gas turbine |
FR3079445A1 (en) * | 2018-03-28 | 2019-10-04 | Safran | PROCESS FOR MANUFACTURING A VANE OF COMPOSITE MATERIAL WITH A REPORTED METAL ATTACK RING FOR GAS TURBINE |
CN111936303A (en) * | 2018-03-28 | 2020-11-13 | 赛峰集团 | Method of manufacturing a blade for a gas turbine engine with a fitted metal leading edge from a composite material |
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 (en) * | 2018-03-28 | 2022-10-21 | 赛峰集团 | Method of manufacturing a blade for a gas turbine engine with a fitted metal leading edge from a composite material |
CN111645337A (en) * | 2019-03-04 | 2020-09-11 | 波音公司 | Tool assembly for manufacturing porous composite structures and related systems and methods |
CN111645337B (en) * | 2019-03-04 | 2023-09-19 | 波音公司 | Tool assembly for fabricating porous composite structures and related systems and methods |
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