FR2096434A1 - - Google Patents

Info

Publication number
FR2096434A1
FR2096434A1 FR7122617A FR7122617A FR2096434A1 FR 2096434 A1 FR2096434 A1 FR 2096434A1 FR 7122617 A FR7122617 A FR 7122617A FR 7122617 A FR7122617 A FR 7122617A FR 2096434 A1 FR2096434 A1 FR 2096434A1
Authority
FR
France
Prior art keywords
fibres
elastic
layer
fibre
graphite
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.)
Granted
Application number
FR7122617A
Other languages
English (en)
Other versions
FR2096434B1 (fr
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.)
Monsanto Co
Original Assignee
Monsanto Co
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 Monsanto Co filed Critical Monsanto Co
Publication of FR2096434A1 publication Critical patent/FR2096434A1/fr
Application granted granted Critical
Publication of FR2096434B1 publication Critical patent/FR2096434B1/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • 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
    • B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • 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
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/12—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by the relative arrangement of fibres or filaments of different layers, e.g. the fibres or filaments being parallel or perpendicular to each other
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/005—Selecting particular materials
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00—Armour; Armour plates
    • F41H5/02—Plate construction
    • F41H5/04—Plate construction composed of more than one layer
    • F41H5/0442—Layered armour containing metal
    • F41H5/0457—Metal layers in combination with additional layers made of fibres, fabrics or plastics
    • F41H5/0464—Metal layers in combination with additional layers made of fibres, fabrics or plastics the additional layers being only fibre- or fabric-reinforced layers
    • 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
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02—Composition of the impregnated, bonded or embedded layer
    • B32B2260/021—Fibrous or filamentary layer
    • B32B2260/023—Two or more layers
    • 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
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04—Impregnation, embedding, or binder material
    • B32B2260/046—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
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02—Synthetic macromolecular fibres
    • B32B2262/0207—Elastomeric fibres
    • 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
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/106—Carbon fibres, e.g. graphite fibres
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/558—Impact strength, toughness
    • 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
    • B32B2603/00—Vanes, blades, propellers, rotors with blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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
    • 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
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Composite Materials (AREA)
  • Ceramic Engineering (AREA)
  • Laminated Bodies (AREA)
FR7122617A 1970-06-23 1971-06-22 Expired FR2096434B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US4896170A 1970-06-23 1970-06-23

Publications (2)

Publication Number Publication Date
FR2096434A1 true FR2096434A1 (fr) 1972-02-18
FR2096434B1 FR2096434B1 (fr) 1975-02-07

Family

ID=21957361

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7122617A Expired FR2096434B1 (fr) 1970-06-23 1971-06-22

Country Status (4)

Country Link
CA (1) CA952806A (fr)
DE (1) DE2130995A1 (fr)
FR (1) FR2096434B1 (fr)
GB (1) GB1324898A (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2336577A1 (fr) * 1975-12-22 1977-07-22 Gen Electric Aube composite et procede de fabrication
FR2375442A1 (fr) * 1976-12-23 1978-07-21 United Technologies Corp Aube de rotor composite
FR2375441A1 (fr) * 1976-12-27 1978-07-21 United Technologies Corp Aubes de rotor a structure composite
FR2544481A1 (fr) * 1983-04-13 1984-10-19 Yves Moriceau Structure multicouches de protection contre les projectiles
FR2550621A1 (fr) * 1983-08-08 1985-02-15 Figgie Int Inc Panneau de cuirasse a resistance balistique et son procede de fabrication
CN113646556A (zh) * 2019-07-01 2021-11-12 三菱制钢株式会社 具有碳纤维和玻璃纤维层的复合线圈弹簧

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FI801415A (fi) * 1979-05-05 1980-11-06 Arthur Britton Arkmaterial
DE3004575A1 (de) * 1980-02-08 1981-08-13 Sigri Elektrographit Gmbh, 8901 Meitingen Pleuelstange aus verbundwerkstoff
GB2164293A (en) * 1984-08-31 1986-03-19 Motoplat Import resistant fuel tanks
GB9216186D0 (en) * 1992-07-30 1992-09-09 Ciba Geigy Ag Product and production method
US6242090B1 (en) 1993-07-26 2001-06-05 Hexcel Corporation Fibre reinforced resin composite products
US7575417B2 (en) * 2003-09-05 2009-08-18 General Electric Company Reinforced fan blade
GB2408016A (en) * 2003-11-14 2005-05-18 Intelligent Engineering Structural sandwich member
CN105909968A (zh) * 2016-06-29 2016-08-31 安丘东旭机械有限公司 一种耐磨件

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1538040A (fr) * 1966-08-20 1968-08-30 Matière première en feuille pour la fabrication de produits en matière stratifiée comprimée et dispositif pour la fabrication de ladite matière

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1538040A (fr) * 1966-08-20 1968-08-30 Matière première en feuille pour la fabrication de produits en matière stratifiée comprimée et dispositif pour la fabrication de ladite matière

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2336577A1 (fr) * 1975-12-22 1977-07-22 Gen Electric Aube composite et procede de fabrication
FR2375442A1 (fr) * 1976-12-23 1978-07-21 United Technologies Corp Aube de rotor composite
FR2375441A1 (fr) * 1976-12-27 1978-07-21 United Technologies Corp Aubes de rotor a structure composite
FR2544481A1 (fr) * 1983-04-13 1984-10-19 Yves Moriceau Structure multicouches de protection contre les projectiles
EP0122857A1 (fr) * 1983-04-13 1984-10-24 Daniel Moriceau Structure multicouches de protection contre les projectiles
WO1984004156A1 (fr) * 1983-04-13 1984-10-25 Daniel Moriceau Structure multicouches de protection contre les projectiles
FR2550621A1 (fr) * 1983-08-08 1985-02-15 Figgie Int Inc Panneau de cuirasse a resistance balistique et son procede de fabrication
CN113646556A (zh) * 2019-07-01 2021-11-12 三菱制钢株式会社 具有碳纤维和玻璃纤维层的复合线圈弹簧
CN113646556B (zh) * 2019-07-01 2023-06-23 三菱制钢株式会社 具有碳纤维和玻璃纤维层的复合线圈弹簧

Also Published As

Publication number Publication date
DE2130995A1 (de) 1972-06-15
FR2096434B1 (fr) 1975-02-07
GB1324898A (en) 1973-07-25
CA952806A (en) 1974-08-13

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Legal Events

Date Code Title Description
ST Notification of lapse