WO2015066407A1 - A method for selective placement of reinforcing fibers in polymeric components - Google Patents

A method for selective placement of reinforcing fibers in polymeric components Download PDF

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Publication number
WO2015066407A1
WO2015066407A1 PCT/US2014/063312 US2014063312W WO2015066407A1 WO 2015066407 A1 WO2015066407 A1 WO 2015066407A1 US 2014063312 W US2014063312 W US 2014063312W WO 2015066407 A1 WO2015066407 A1 WO 2015066407A1
Authority
WO
WIPO (PCT)
Prior art keywords
polymeric component
pins
reinforced polymeric
polymer
reinforcing fibers
Prior art date
Application number
PCT/US2014/063312
Other languages
French (fr)
Inventor
Evan BUTCHER
Wendell V. TWELVES
Gary A. SCHIRTZINGER
Joseph Ott
Lyutsia Dautova
Original Assignee
United Technologies Corporation
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 United Technologies Corporation filed Critical United Technologies Corporation
Priority to US15/033,283 priority Critical patent/US20160257081A1/en
Priority to EP14857775.2A priority patent/EP3062993A4/en
Publication of WO2015066407A1 publication Critical patent/WO2015066407A1/en
Priority to US15/826,142 priority patent/US20180169976A1/en

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Classifications

    • 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
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during 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
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/56—Winding and joining, e.g. winding spirally
    • B29C53/564—Winding and joining, e.g. winding spirally for making non-tubular articles
    • 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
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/80—Component parts, details or accessories; Auxiliary operations
    • B29C53/82—Cores or mandrels
    • B29C53/821—Mandrels especially adapted for winding and joining
    • B29C53/822—Single use mandrels, e.g. destructible, becoming part of the wound articles
    • 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
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/80—Component parts, details or accessories; Auxiliary operations
    • B29C53/82—Cores or mandrels
    • B29C53/821—Mandrels especially adapted for winding and joining
    • B29C53/828—Arrangements comprising a plurality of cores or mandrels, e.g. to increase production speed
    • 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
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • 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
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
    • 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
    • B29C70/347—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 combined with compressing after the winding of lay-ups having a non-circular cross-section, e.g. flat spiral windings
    • 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
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/541—Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement
    • 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
    • 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
    • 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
    • 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
    • B29K2071/00—Use of polyethers, e.g. PEEK, i.e. polyether-etherketone or PEK, i.e. polyetherketone 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
    • B29K2079/00—Use of polymers having nitrogen, with or without oxygen or carbon only, in the main chain, not provided for in groups B29K2061/00 - B29K2077/00, as moulding material
    • B29K2079/08—PI, i.e. polyimides or derivatives thereof
    • B29K2079/085—Thermoplastic polyimides, e.g. polyesterimides, PEI, i.e. polyetherimides, or polyamideimides; Derivatives thereof
    • 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
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/0058—Liquid or visquous
    • 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
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B29K2105/10—Cords, strands or rovings, e.g. oriented cords, strands or rovings
    • B29K2105/101—Oriented
    • 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
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/25—Solid
    • B29K2105/251—Particles, powder or granules
    • 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
    • B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0012—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular thermal properties
    • B29K2995/0017—Heat stable
    • 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
    • B29L2001/00—Articles provided with screw threads
    • 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
    • B29L2031/748—Machines or parts thereof not otherwise provided for
    • 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
    • B29L2031/748—Machines or parts thereof not otherwise provided for
    • B29L2031/7504—Turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/40—Organic materials
    • F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
    • F05D2300/436—Polyetherketones, e.g. PEEK

Definitions

  • the present invention relates generally to gas turbine engine components and, more particularly, to gas turbine engine components made from high- temperature polymers.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Textile Engineering (AREA)
  • Materials Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Moulding By Coating Moulds (AREA)
  • Reinforced Plastic Materials (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)

Abstract

A method of forming a reinforced polymeric component includes securing a plurality of pins within a mold and wrapping reinforcing fibers around the pins to form a web of reinforcing fibers. The web of reinforcing fibers has a plurality of layers. The method of forming a reinforced polymeric component further includes adding a polymer to the mold and processing the polymer to form a molded polymeric component that contains the pins and the web of reinforcing fibers. A reinforced polymeric component includes a web of reinforcing fibers wrapped around a plurality of pins. The web of reinforcing fibers includes a plurality of layers. The reinforced polymeric component further includes a molded and processed polymer containing the web of reinforcing fibers and pins.

Description

A METHOD FOR SELECTIVE PLACEMENT OF REINFORCING FIBERS IN
POLYMERIC COMPONENTS
BACKGROUND
The present invention relates generally to gas turbine engine components and, more particularly, to gas turbine engine components made from high- temperature polymers.
Using a high-temperature polymer such as polyether ether ketone (PEEK) or polytheramide, such as Ultem, to make aircraft engine components has several advantages. In particular, high-temperature polymers make low-density components with the capacity to withstand high temperatures. Because mechanical properties fall as temperature rises, high- temperature polymer components are typically reinforced with load-bearing inserts. However, using load-bearing inserts requires curing multiple layers of discontinuous material.
SUMMARY
A method of forming a reinforced polymeric component includes securing a plurality of pins within a mold and wrapping reinforcing fibers around the pins to form a web of reinforcing fibers. The web of reinforcing fibers has a plurality of layers. The method of forming a reinforced polymeric component further includes adding a polymer to the mold and processing the polymer to form a molded polymeric component that contains the pins and the web of reinforcing fibers.
A reinforced polymeric component includes a web of reinforcing fibers wrapped around a plurality of pins. The web of reinforcing fibers includes a plurality of layers. The reinforced polymeric component further includes a molded and processed polymer containing the web of reinforcing fibers and pins.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a perspective view of an embodiment of reinforcing fibers in a mold.
FIG. 2 is a perspective view of an embodiment of a mold.
FIG. 3 is a perspective view of a fiber alignment pin.
FIG. 4 is a perspective view of a molded polymeric component. DETAILED DESCRIPTION
FIGs. 1 and 2 are perspective views of an embodiment of mold 10. Mold 10 includes base 12 and side wall 14. Base 12 includes holes 16, configured to secure alignment pins 18, as shown in FIG. 1. Alignment pins 18 include ribs 20 and grooves 22, which are configured to align reinforcing fibers 24. In FIG. 2, alignment pins 18 are not shown so that holes 16 can be seen.
Mold 10 forms a container for holding a polymer, such as PEEK or Ultem, in liquid or powder form while the polymer is being processed. Mold 10 may be any shape that may be used to form a reinforced polymeric component. Mold 10 may be any material suitable for processing a polymer. Base 12 is connected to side wall 14. Together, base 12 and side walls 14 form the exterior of mold 10. Base 12 further includes holes 16, which are arranged in a pattern representing desired points of reinforcement, discussed further in FIG. 2. Holes 16 are configured to secure alignment pins 18 in place by providing a close-fitting coupling. Alignment pins 18 are secured in the horizontal plane of mold 10 but may be lifted out of mold 10 when a reinforced polymeric component is lifted out of mold 10. Gaskets may be used to seal between holes 16 and alignment pins 18. Alignment pins 18 are positioned within holes 16 in the same pattern representing desired points of reinforcement, discussed further in conjunction with FIG. 4. Alignment pins 18 contain a plurality of ribs 20 and a plurality of grooves 22, which hold reinforcing fibers 24 in place, discussed further in FIG. 3. Reinforcing fibers 24 are drawn taut and secured around alignment pins 18 to form web 26 within mold 10. Reinforcing fibers 24 may be a single strand or multiple strands wound around alignment pins 18. Web 26 may have a plurality of layers depending on the degree of reinforcement desired, discussed further in conjunction with FIG. 3.
FIG. 3 is a perspective view of an embodiment of alignment pin 18. Alignment pin
18 includes a plurality of ribs 20 and a plurality of grooves 22, which are configured to hold reinforcing fibers 24. Gasket 28 is configured to seal alignment pin 18 into a hole in the base of the mold (not shown).
The number of ribs 20 and grooves 22 may vary depending on the number of reinforcing fibers 24 desired. The vertical position of grooves 22 may vary depending on the separation of reinforcing fibers 24 desired. The width of grooves 22 may vary to accommodate multiple strands of reinforcing fibers 24. Reinforcing fibers 24 pass between ribs 20. Alignment pin 18 forms a stable point around which reinforcing fibers 24 are pulled taut. Alignment pin 18 may provide attachment hard points for a molded component. For example, alignment pin 18 may include a bore B or thread.
To form a reinforced polymeric component, a plurality of pins 18 are secured within a mold 10. Reinforcing fibers 24 are wrapped around pins 18 to form web 26 of reinforcing fibers 24. Web 26 may include a plurality of layers. A polymer is added to mold 10 and processed to form a reinforced polymeric component that contains pins 18 and web 26. Pins 18 within mold 10 provide a nexus for reinforcing fibers 24 and are located at desired attachment points and load path tailored points on the molded polymeric component. Pins 18 typically include pins 18 secured near a periphery of mold 10 to provide attachment points. Mold 10, to which the polymer is added, comprises a container having base 12 comprising a plurality of holes 16 for securing pins 18. Holes 16 are close-fitting to form a seal around pins 18, and gaskets 28 may be used to aid in sealing around pins 18. The polymer added to mold 10 is a polymer capable of service in the thermal environment the component will see. Most preferably, the polymer is a high-temperature polymer. The polymer may be added to mold 10 in liquid or powder form. Following processing, the molded polymeric component is disengaged from mold 10.
FIG. 4 is a perspective view of a reinforced polymeric component 30 produced by the above method. Reinforced polymeric component 30 includes alignment pins 18 and web 26. Web 26 includes reinforcing fibers 24.
Reinforced polymeric component 30 may be any shape desired for a particular environment within a gas turbine engine. Reinforced polymeric component 30 may comprise any molded and processed polymer capable of service in the particular environment in which reinforced polymeric component 30 is placed. Alignment pins 18 are disengaged from a mold (not shown, discussed above), and contained within polymeric component 30. Alignment pins 18 may be in any pattern, most preferably the pattern representing desired points of reinforcement along the load-bearing path of reinforced polymeric component 30.
While the invention has been described with reference to an exemplary embodiment(s), the invention will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment(s) disclosed but that the invention will include all embodiments falling within the scope of the appended claims.

Claims

CLAIMS:
1. A method of forming a reinforced polymeric component, the method
comprising:
securing a plurality of pins within a mold;
wrapping reinforcing fibers around the pins to form a web of reinforcing fibers, wherein the web has a plurality of layers;
adding a polymer to the mold; and
processing the polymer to form a molded polymeric component containing the web of reinforcing fibers and pins.
2. The method of forming a reinforced polymeric component of claim 1, wherein each of the pins provides a nexus for the reinforcing fibers.
3. The method of forming a reinforced polymeric component of claim 2, wherein the pins are located at desired attachment points and load path tailored points on a molded polymeric component.
4. The method of forming a reinforced polymeric component of claim 3, wherein the plurality of pins typically include pins secured near a periphery of the mold to provide attachment hard points.
5. The method of forming a reinforced polymeric component of claim 1, wherein the mold comprises a container having a base comprising a plurality of holes configured to secure the pins.
6. The method of forming a reinforced polymeric component of claim 5, wherein close-fitting holes or a plurality of gaskets are configured to seal around the pins at the holes configured to secure the pins.
7. The method of forming a reinforced polymeric component of claim 1, wherein the polymer is capable of service in the thermal environment the component will see. Preferably, the polymer is a high-temperature polymer.
8. The method of forming a reinforced polymeric component of claim 1, wherein the polymer is added in liquid or powder form.
9. The method of forming a reinforced polymeric component of claim 1, wherein the molded polymeric component is disengaged from the mold.
10. A reinforced polymeric component comprising:
a web of reinforcing fibers wrapped around a plurality of pins, wherein the web has a plurality of layers; and
a molded and processed polymer containing the web of reinforcing fibers and pins.
11. The reinforced polymeric component of claim 10, wherein the pins comprise a plurality of ribs.
12. The reinforced polymeric component of claim 11, wherein the pins are configured to provide a bolt or screw attachment feature and to act as a hard point in the reinforced polymeric component.
13. The reinforced polymeric component of claim 12, wherein the pins are located at desired attachment points and load path tailored points on the molded polymeric component.
14. The reinforced polymeric component of claim 10, wherein the polymer is capable of service in the thermal environment the component will see. Preferably, the polymer is a high-temperature polymer.
15. The reinforced polymeric component of claim 10, wherein the polymer is molded in liquid or powder form.
PCT/US2014/063312 2013-10-31 2014-10-31 A method for selective placement of reinforcing fibers in polymeric components WO2015066407A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US15/033,283 US20160257081A1 (en) 2013-10-31 2014-10-31 A method for selective placement of reinforcing fibers in polymeric components
EP14857775.2A EP3062993A4 (en) 2013-10-31 2014-10-31 A method for selective placement of reinforcing fibers in polymeric components
US15/826,142 US20180169976A1 (en) 2013-10-31 2017-11-29 Method for selective placement of reinforcing fibers in polymeric components

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Application Number Priority Date Filing Date Title
US201361898201P 2013-10-31 2013-10-31
US61/898,201 2013-10-31

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US15/033,283 A-371-Of-International US20160257081A1 (en) 2013-10-31 2014-10-31 A method for selective placement of reinforcing fibers in polymeric components
US15/826,142 Continuation US20180169976A1 (en) 2013-10-31 2017-11-29 Method for selective placement of reinforcing fibers in polymeric components

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FR3067279A1 (en) * 2017-06-13 2018-12-14 Conseil Et Technique METHOD FOR PRODUCING A COMPOSITE MATERIAL PART AND COMPOSITE PART OBTAINED

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101743458B1 (en) * 2016-03-24 2017-06-07 주식회사 엠에스 오토텍 Bushing for making structural composite preforms
FR3091300B1 (en) * 2018-12-31 2021-02-19 Paris Sciences Lettres Quartier Latin new method of weaving textile articles and device for the implementation

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3056706A (en) 1958-07-16 1962-10-02 Proman Inc High lineal strength member and method of making same
US5721047A (en) * 1991-11-01 1998-02-24 Applied Research Of Australia Pty Ltd Polymeric moldings reinforced with tows of fibers
US5939013A (en) * 1997-08-25 1999-08-17 Florida State University Process and apparatus for the production of high strength polymer composite structures
WO2001098064A2 (en) * 2000-06-16 2001-12-27 Decillion, Llc Molding of reinforced thermoplastic composites
US20020195742A1 (en) * 2001-05-08 2002-12-26 Charles Beck System and method of making a layered, reinforced composite
EP2289690A2 (en) * 2009-06-02 2011-03-02 Johns Manville Method and systems for making reinforced thermoplastic composites, and the products

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3123948A (en) * 1964-03-10 Reinforced
US3694284A (en) * 1969-11-10 1972-09-26 Aerojet General Co Method of making honeycomb structures
US3891488A (en) * 1970-09-28 1975-06-24 Charles S White Structural bearing element having a low friction surface and method
US4137354A (en) * 1977-03-07 1979-01-30 Mcdonnell Douglas Corporation Ribbed composite structure and process and apparatus for producing the same
US4376669A (en) * 1980-08-15 1983-03-15 The British Petroleum Company Limited Method of fabricating energy absorbing structure
US4414049A (en) * 1981-09-25 1983-11-08 Kelsey-Hayes Company Method of manufacture of an energy absorbing beam
GB8405844D0 (en) * 1984-03-06 1984-04-11 Ici Plc Making reinforced fibre products
GB8722271D0 (en) * 1987-09-22 1987-10-28 Ici Plc Thermoplastic composites
US5330599A (en) * 1988-12-19 1994-07-19 Lockheed Missiles & Space Company, Inc. Grid structures
US5264274A (en) * 1991-02-04 1993-11-23 Honda Giken Kogyo Kabushiki Kaisha Thermoplastic composite material having improved toughness and method of producing same
FR2710870B1 (en) * 1993-10-08 1995-12-08 Inst Francais Du Petrole Device and method for mass production of fiber-reinforced resin parts.
US5913994A (en) * 1996-08-30 1999-06-22 Norton Company Method for fabricating abrasive discs
US20050204697A1 (en) * 2004-03-03 2005-09-22 Rue Jerry R Insulated structural building panel and assembly system

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3056706A (en) 1958-07-16 1962-10-02 Proman Inc High lineal strength member and method of making same
US5721047A (en) * 1991-11-01 1998-02-24 Applied Research Of Australia Pty Ltd Polymeric moldings reinforced with tows of fibers
US5939013A (en) * 1997-08-25 1999-08-17 Florida State University Process and apparatus for the production of high strength polymer composite structures
WO2001098064A2 (en) * 2000-06-16 2001-12-27 Decillion, Llc Molding of reinforced thermoplastic composites
US20020195742A1 (en) * 2001-05-08 2002-12-26 Charles Beck System and method of making a layered, reinforced composite
EP2289690A2 (en) * 2009-06-02 2011-03-02 Johns Manville Method and systems for making reinforced thermoplastic composites, and the products

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP3062993A4 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITUA20164792A1 (en) * 2016-06-30 2017-12-30 Mauro Pastore Double and simple construction net in pultruded fiber rods connected by composite connectors drilled to form nets or cages with known resistance to block insulating cladding panels, renovation of old walls or construction of new ones
WO2018002865A1 (en) * 2016-06-30 2018-01-04 Mauro Pastore Wall with cages and connectors of composite pultruded fiber rods bounto block coating insulating panels to a core
FR3067279A1 (en) * 2017-06-13 2018-12-14 Conseil Et Technique METHOD FOR PRODUCING A COMPOSITE MATERIAL PART AND COMPOSITE PART OBTAINED
WO2018229437A1 (en) 2017-06-13 2018-12-20 Conseil Et Technique Method for producing a composite material part, and composite part obtained
US11590714B2 (en) 2017-06-13 2023-02-28 Conseil Et Technique Method for producing a part made of composite material, and so obtained composite part

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US20160257081A1 (en) 2016-09-08
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