GB845138A - Method for the manufacture of an aircraft part, and aircraft part made according to this method - Google Patents
Method for the manufacture of an aircraft part, and aircraft part made according to this methodInfo
- Publication number
- GB845138A GB845138A GB2838/58A GB283858A GB845138A GB 845138 A GB845138 A GB 845138A GB 2838/58 A GB2838/58 A GB 2838/58A GB 283858 A GB283858 A GB 283858A GB 845138 A GB845138 A GB 845138A
- Authority
- GB
- United Kingdom
- Prior art keywords
- component
- mould
- resin
- vacuum
- fillets
- 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
- 238000000034 method Methods 0.000 title 2
- 238000004519 manufacturing process Methods 0.000 title 1
- 239000003822 epoxy resin Substances 0.000 abstract 2
- 239000003365 glass fiber Substances 0.000 abstract 2
- 238000010438 heat treatment Methods 0.000 abstract 2
- 229920000647 polyepoxide Polymers 0.000 abstract 2
- 239000000126 substance Substances 0.000 abstract 2
- 239000000853 adhesive Substances 0.000 abstract 1
- 230000001070 adhesive effect Effects 0.000 abstract 1
- 239000004411 aluminium Substances 0.000 abstract 1
- 229910052782 aluminium Inorganic materials 0.000 abstract 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract 1
- 239000011248 coating agent Substances 0.000 abstract 1
- 238000000576 coating method Methods 0.000 abstract 1
- 239000006260 foam Substances 0.000 abstract 1
- 239000011521 glass Substances 0.000 abstract 1
- 229910052751 metal Inorganic materials 0.000 abstract 1
- 239000002184 metal Substances 0.000 abstract 1
- 238000000465 moulding Methods 0.000 abstract 1
- 239000004627 regenerated cellulose Substances 0.000 abstract 1
- 229920005989 resin Polymers 0.000 abstract 1
- 239000011347 resin Substances 0.000 abstract 1
- 229920003002 synthetic resin Polymers 0.000 abstract 1
- 239000000057 synthetic resin Substances 0.000 abstract 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
- 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
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
- B29C70/086—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of pure plastics material, e.g. foam layers
-
- 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
- B29C70/04—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
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D24/00—Producing articles with hollow walls
- B29D24/002—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
- B29D24/005—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having joined ribs, e.g. honeycomb
-
- 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
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
-
- 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
- B64D15/16—De-icing or preventing icing on exterior surfaces of aircraft by mechanical means, e.g. pulsating mats or shoes attached to, or built into, surface
- B64D15/166—De-icing or preventing icing on exterior surfaces of aircraft by mechanical means, e.g. pulsating mats or shoes attached to, or built into, surface using pneumatic boots
-
- 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
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2021/00—Use of unspecified rubbers as moulding material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2063/00—Use of EP, i.e. epoxy resins or derivatives thereof, as moulding material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2309/00—Use of inorganic materials not provided for in groups B29K2303/00 - B29K2307/00, as reinforcement
- B29K2309/08—Glass
-
- 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
- B29L2031/3082—Fuselages
-
- 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
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Aviation & Aerospace Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL845138X | 1957-02-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB845138A true GB845138A (en) | 1960-08-17 |
Family
ID=19845141
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2838/58A Expired GB845138A (en) | 1957-02-20 | 1958-01-28 | Method for the manufacture of an aircraft part, and aircraft part made according to this method |
Country Status (2)
Country | Link |
---|---|
GB (1) | GB845138A (enrdf_load_stackoverflow) |
NL (1) | NL89352C (enrdf_load_stackoverflow) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1994014600A1 (en) * | 1992-12-23 | 1994-07-07 | United Technologies Corporation | A composite molding apparatus and method for high pressure co-cure molding of lightweight honeycomb core composite articles having ramped surfaces utilizing low density, stabilized ramped honeycomb cores and product formed thereby |
WO1998046418A1 (en) * | 1997-04-16 | 1998-10-22 | Sikorsky Aircraft Corporation | Apparatus and method for installing a leading-edge sheath onto a helicopter main rotor blade subassembly |
JP2008126793A (ja) * | 2006-11-20 | 2008-06-05 | Honda Motor Co Ltd | 前縁スキンの段差調整構造および前縁スキンの組付方法 |
FR2918036A1 (fr) * | 2007-06-26 | 2009-01-02 | Sogeclair Sa | Dispositif formant bord d'attaque pour une voilure d'aeronef et voilure equipee d'un tel dispositif. |
ITTO20080912A1 (it) * | 2008-12-09 | 2010-06-10 | Alenia Aeronautica Spa | Bordo d'attacco per ali ed impennaggi di aeromobili |
WO2016162374A1 (de) * | 2015-04-08 | 2016-10-13 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Flügelstruktur für flugobjekte |
EP4071350A1 (en) * | 2021-04-09 | 2022-10-12 | LM Wind Power A/S | A wind turbine blade with a fairing |
CN117067639A (zh) * | 2023-09-22 | 2023-11-17 | 哈尔滨远驰航空装备有限公司 | 小圆角复合材料外衬的成型方法及产品 |
CN117325463A (zh) * | 2023-09-27 | 2024-01-02 | 中航西安飞机工业集团股份有限公司 | 一种机尾翼前缘除冰套的粘接方法 |
PL443923A1 (pl) * | 2023-02-28 | 2024-09-02 | Air-Concept Spółka Z Ograniczoną Odpowiedzialnością | Sposób wytwarzania kadłuba jednostki lotniczej |
-
0
- NL NL89352D patent/NL89352C/xx active
-
1958
- 1958-01-28 GB GB2838/58A patent/GB845138A/en not_active Expired
Cited By (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1994014600A1 (en) * | 1992-12-23 | 1994-07-07 | United Technologies Corporation | A composite molding apparatus and method for high pressure co-cure molding of lightweight honeycomb core composite articles having ramped surfaces utilizing low density, stabilized ramped honeycomb cores and product formed thereby |
TR28891A (tr) * | 1992-12-23 | 1997-07-17 | United Technologies Corp | Alcak dansiteli, stabilize edilmis rampali balpetegi gövdeler kullanarak rampali satihlara sahip hafif balpetegi gövdeli kompozit esyalarin yüksek basincta birlikte sertlestirme suretile kaliplanmsi icin bir kompozit kaliplama cihazi ve usulü ve bu suretle meydana getirilmis mamül. |
US5688353A (en) * | 1992-12-23 | 1997-11-18 | Sikorsky Aircraft Corporation | Method of fabricating a low total density, stabilized ramped honeycomb core for high pressure co-cure composite molding |
JP3335355B2 (ja) | 1992-12-23 | 2002-10-15 | ユナイテッド テクノロジーズ コーポレイション | 低密度の、安定化した傾斜形ハニカムコアを使用して、傾斜面を有する軽量のハニカムコア複合製品を高圧共硬化成形する複合成形装置、および成形方法、ならびにそれによって製造した製品 |
WO1998046418A1 (en) * | 1997-04-16 | 1998-10-22 | Sikorsky Aircraft Corporation | Apparatus and method for installing a leading-edge sheath onto a helicopter main rotor blade subassembly |
JP2008126793A (ja) * | 2006-11-20 | 2008-06-05 | Honda Motor Co Ltd | 前縁スキンの段差調整構造および前縁スキンの組付方法 |
US7992822B2 (en) | 2006-11-20 | 2011-08-09 | Honda Motor Co., Ltd. | Leading edge skin height difference adjusting structure and method of assembling leading edge skin |
FR2918036A1 (fr) * | 2007-06-26 | 2009-01-02 | Sogeclair Sa | Dispositif formant bord d'attaque pour une voilure d'aeronef et voilure equipee d'un tel dispositif. |
EP2196309A1 (en) * | 2008-12-09 | 2010-06-16 | Alenia Aeronautica S.P.A. | Leading edge for aircraft wings and empennages |
ITTO20080912A1 (it) * | 2008-12-09 | 2010-06-10 | Alenia Aeronautica Spa | Bordo d'attacco per ali ed impennaggi di aeromobili |
US8245972B2 (en) | 2008-12-09 | 2012-08-21 | Alenia Aeronautica S.P.A. | Leading edge for aircraft wings and empennages |
WO2016162374A1 (de) * | 2015-04-08 | 2016-10-13 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Flügelstruktur für flugobjekte |
US10661886B2 (en) | 2015-04-08 | 2020-05-26 | Deutsches Zentrum Luft- Und Raumfahrt E.V. | Wing structure for flying objects |
EP4071350A1 (en) * | 2021-04-09 | 2022-10-12 | LM Wind Power A/S | A wind turbine blade with a fairing |
WO2022214426A1 (en) * | 2021-04-09 | 2022-10-13 | Lm Wind Power A/S | A wind turbine blade with a fairing |
PL443923A1 (pl) * | 2023-02-28 | 2024-09-02 | Air-Concept Spółka Z Ograniczoną Odpowiedzialnością | Sposób wytwarzania kadłuba jednostki lotniczej |
CN117067639A (zh) * | 2023-09-22 | 2023-11-17 | 哈尔滨远驰航空装备有限公司 | 小圆角复合材料外衬的成型方法及产品 |
CN117067639B (zh) * | 2023-09-22 | 2023-12-29 | 哈尔滨远驰航空装备有限公司 | 小圆角复合材料外衬的成型方法及产品 |
CN117325463A (zh) * | 2023-09-27 | 2024-01-02 | 中航西安飞机工业集团股份有限公司 | 一种机尾翼前缘除冰套的粘接方法 |
Also Published As
Publication number | Publication date |
---|---|
NL89352C (enrdf_load_stackoverflow) | 1900-01-01 |
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