GB2551159A - A fastener assembly - Google Patents

A fastener assembly Download PDF

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Publication number
GB2551159A
GB2551159A GB1609990.5A GB201609990A GB2551159A GB 2551159 A GB2551159 A GB 2551159A GB 201609990 A GB201609990 A GB 201609990A GB 2551159 A GB2551159 A GB 2551159A
Authority
GB
United Kingdom
Prior art keywords
retaining member
fastener
component
assembly
bore
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
GB1609990.5A
Other versions
GB201609990D0 (en
GB2551159B (en
Inventor
John Mallard Will
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.)
Ford Motor Co Ltd
Ford Motor Co
Original Assignee
Ford Motor Co Ltd
Ford Motor 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 Ford Motor Co Ltd, Ford Motor Co filed Critical Ford Motor Co Ltd
Priority to GB1609990.5A priority Critical patent/GB2551159B/en
Publication of GB201609990D0 publication Critical patent/GB201609990D0/en
Priority to CN201710402710.0A priority patent/CN107477062B/en
Priority to US15/615,282 priority patent/US10935066B2/en
Priority to DE102017112651.1A priority patent/DE102017112651A1/en
Publication of GB2551159A publication Critical patent/GB2551159A/en
Application granted granted Critical
Publication of GB2551159B publication Critical patent/GB2551159B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B31/00Screwed connections specially modified in view of tensile load; Break-bolts
    • F16B31/04Screwed connections specially modified in view of tensile load; Break-bolts for maintaining a tensile load
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B21/00Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings
    • F16B21/10Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B21/00Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings
    • F16B21/10Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts
    • F16B21/20Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts for bolts or shafts without holes, grooves, or notches for locking members
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D27/00Connections between superstructure or understructure sub-units
    • B62D27/06Connections between superstructure or understructure sub-units readily releasable
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B19/00Bolts without screw-thread; Pins, including deformable elements; Rivets
    • F16B19/02Bolts or sleeves for positioning of machine parts, e.g. notched taper pins, fitting pins, sleeves, eccentric positioning rings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B35/00Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws
    • F16B35/02Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws divided longitudinally
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B1/00Devices for securing together, or preventing relative movement between, constructional elements or machine parts
    • F16B1/02Means for securing elements of mechanisms after operation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B29/00Screwed connection with deformation of nut or auxiliary member while fastening

Abstract

A fastener assembly 8 comprises a fastener 10 configured to couple a first component 4 to a second component 6 of a motor vehicle and a retaining member 12. The fastener 10 comprises a shank 10a configured to be received within a bore 4a of the first component 4. The retaining member 12 is couplable to the fastener 10 and the first component 4 and comprises an opening configured to receive the fastener shank 10a and to provide a resistance against the removal of the fastener shank 10a from the bore 4a of the first component 4. The retaining member 12 comprises a deformable portion configured to deform from a first state to a second state such that the fastener shank 10a may be removed from the bore 4a when the deformable portion is in the second state.

Description

A fastener assembly Technical Field
The present disclosure relates to a fastener assembly and is particularly, although not exclusively, concerned with an engine assembly configured to allow a captive, single use fastener to be replaced during maintenance of the engine assembly.
Background A motor vehicle often comprises many different types of fastener that are used for coupling together the components and subassemblies of the vehicle. The different fasteners used on the vehicle may have different diameters, lengths and/or grades, e.g. strengths. Locating the appropriate fasteners to use for assembling each component or subassembly on to the vehicle may be a time consuming process.
In order to improve the efficiency with which the motor vehicle is assembled, it is often desirable to locate the appropriate fasteners for a particular component or subassembly prior to the stage in the assembly of the vehicle when the component or subassembly is installed onto the vehicle. In some cases the fasteners may be located and provided in bores of the component or subassembly on a subassembly line, e.g. away from a main vehicle production line, and may be transported to the main production line with the fasteners already in place. In this case, it is often desirable for the fasteners to be captive fasteners that are held within the bores of the component or subassembly and prevented from disengaging from the component or subassembly prior to installation on the vehicle.
Following manufacture of the vehicle, it is often desirable to disassemble components or subassemblies from the vehicle in order to perform service and maintenance procedures on the vehicle. During maintenance it may be desirable to replace one or more of the fasteners used to couple a component or subassembly to the vehicle. For example, it may be desirable to replace a single use fastener that has been exposed to stresses equal to or greater than its yield stress during a previous assembly procedure. However, if the fastener is a captive fastener that cannot be removed from the bore of the component or subassembly, it may be necessary for the component or subassembly itself to be replaced in order to replace the fastener.
Furthermore, during some service and maintenance operations, it may be desirable to fully remove the fasteners from a component or subassembly in order to provide clearance for the component or subassembly to be removed from the vehicle, e g. to replace the component. However, if the fasteners are captive within the component, it may not be possible to fully remove the fasteners and further disassembly of the vehicle may be required in order to replace the component or subassembly.
Statements of Invention
According to an aspect of the present disclosure, there is provided, a fastener assembly for a motor vehicle, the fastener assembly comprising: a fastener configured to couple a first component to a second component of the motor vehicle, the fastener comprising a shank configured to be received within a bore of the first component; and a retaining member, the retaining member being couplable to the fastener and the first component, the retaining member comprising an opening configured to receive the fastener shank and to provide a resistance against the removal of the fastener shank from the bore, wherein the retaining member comprises a deformable portion configured to deform from a first state to a second state by virtue of the first component operating environment such that the fastener may be removed from the bore when the deformable portion is in the second state following operation of the motor vehicle.
The terms deform and deformable used within the specification are intended to encompass any process by which the retaining member or a portion of the retaining member changes its shape or form. For example, deforming may include, melting, subliming, breaking, e.g. fracturing or shattering, decomposing, e.g. thermally decomposing, oxidising, plastically deforming or any other type of deformation.
The fastener assembly may be for use in an engine assembly of the motor vehicle. The first component may be a component of the engine. The first component operating environment may correspond to an engine operating environment.
The fastener assembly may be used on an engine, transmission, or another component of the powertrain or the exhaust system of the motor vehicle, including the exhaust after-treatment systems.
The deformable portion may have a melting point less than or equal an operating temperature of the first component. For example, the deformable portion may have a melting temperature lower than 70 degrees Celsius or lower than 60 degrees Celsius.
The deformable portion may be made from a polymer material, such as polycaprolactone. Alternatively, the deformable portion may be made from a wax material. The retaining member may consist of the deformable portion.
The retaining member may be configured to at least partially melt during operation of the motor vehicle. For example, the deformable portion may be configured to at least partially melt. The deformable portion may be configured such that substantially all of the deformable portion melts during operation of the motor vehicle, eg. the engine assembly of the motor vehicle.
The retaining member may be configured such that at least a portion of the retaining member, e.g. the deformable portion or at least part of the deformable portion, evaporates during operation of the motor vehicle.
The retaining member may be configured to vibrate during operation of the motor vehicle. The retaining member may be configured such that a natural frequency of vibration of the retaining member may be substantially equal to an operating frequency of the motor vehicle. For example, a natural frequency of vibration of the retaining member may be substantially equal to an engine running speed of the engine assembly of the motor vehicle. Alternatively, the natural frequency of the retaining member may be a multiple or fraction of the engine running speed.
The retaining member may be configured such that the natural frequency of the retaining member varies according to the temperature of the retaining member. For example, the retaining member may be configured such that that a natural frequency of vibration of the retaining member may be substantially equal to an operating frequency of the motor vehicle at the operating temperature of the first component.
The retaining member may be configured to fracture into a plurality of fragments during operation of the engine assembly. For example, the deformable portion may fracture or the retaining member may fracture such that the deformable portion becomes detached from a remaining portion of the retaining member.
The retaining member may be configured to be at least partially received within the bore. The bore and/or the retaining member may be configured such that the retaining member forms an interference fit with the bore.
The fastener shank may comprise a mid portion and a distal portion. The mid portion may have a smaller diameter than the distal portion. The mid portion and the distal portion may be separated by a shoulder. The retaining member may act against the shoulder in order to provide resistance against the removal of the fastener.
The retaining member may be couplable to the fastener by inserting the shank of the fastener through the opening such that the retaining member engages the shoulder of the fastener shank.
The retaining member may comprise one or more resilient grip elements. The resilient grip elements may be configured to deform in order to allow the fastener to be inserted through the opening. The resilient grip elements may be configured to grip the fastener to couple the fastener to the retaining member. The resilient grip elements may engage the central portion and/or the shoulder of the fastener shank.
The fastener may be a single use fastener. The fastener may be configured such that stresses within the fastener are substantially equal to or exceed the yield stress of the material of the fastener, when the first and second components are coupled together.
According to another aspect of the present disclosure, there is provided a fastener for an assembly of a motor vehicle, the fastener comprising: a shank configured to be received within a bore of the assembly; and a retaining member configured to retain the shank at least partially within the bore, wherein the retaining member is configured to release during an operation of the assembly, such that the retaining member no longer retains the shank within the bore following the operation of the assembly.
According to another aspect of the present disclosure, there is provide an engine assembly for a motor vehicle, the engine assembly comprising: the fastener assembly according to a previously mentioned aspect of the disclosure and the first component.
The first component may comprise a drain channel. The drain channel may be configured to allow a melted portion of the retaining member to drain away from the bore. The drain channel may comprise an opening, e.g. through the first component, allowing the melted portion of the retaining member to drain out of and/or away from the first component.
Alternatively, the first component may comprise a chamber. The chamber may be configured such that the melted portion of the retaining member is received within the chamber. The melted portion may be retained within the chamber, e.g. during future operation of the motor vehicle.
To avoid unnecessary duplication of effort and repetition of text in the specification, certain features are described in relation to only one or several aspects or embodiments of the invention. However, it is to be understood that, where it is technically possible, features described in relation to any aspect or embodiment of the invention may also be used with any other aspect or embodiment of the invention.
Brief Description of the Drawings
For a better understanding of the present invention, and to show more clearly how it may be carried into effect, reference will now be made, by way of example, to the accompanying drawings, in which:
Figure 1 is a partial sectional view of an engine assembly, according to an arrangement of the present disclosure, prior to assembly of the engine assembly;
Figure 2 is a partial sectional view of a fastener assembly, according to arrangements of the present disclosure;
Figures 3a and 3b are end views of retaining members according to an arrangements of the present disclosure;
Figure 4 is a partial sectional view of the engine assembly following assembly;
Figure 5 is a partial sectional view of the engine assembly following operation of die engine assembly; and
Figure 6 is a partial sectional view of an engine assembly, according to another arrangement of the present disclosure.
Detailed Description
With reference to Figure 1, an engine assembly 2 for a motor vehicle, according to an arrangement of the present disclosure, comprises a first component 4 and a second component 6. In the arrangement shown in Figure 1, the first component 4 comprises a cylinder head and the second component 6 comprises a cylinder block. However it is equally envisaged that the first and second components may comprise any components or subassemblies of an engine assembly that are configured to be coupled together using one or more fasteners.
The engine assembly 2 may further comprise a fastener assembly 8, comprising a fastener 10 and a retaining member 12. The fastener 10 may comprise an elongate shank 10a and ahead lOd. As shown in Figure 1 the head lOd may comprise a washer 11 integral with the head lOd. However, in other arrangements, such as the arrangement depicted in Figure 6, the washer 11 may be a separate component.
As shown in Figure 1, prior to assembly of the engine assembly 2, the fastener 10, e.g. shank 10a of the fastener, may be provided within a bore 4a of the first component 4 and the retaining member 12 may be configured to provide a resistance against the removal of the shank 10a from the bore 4a.
In the arrangement shown in Figure 1, the retaining member 12 is coupled to the first component 4, e.g. fixed axially relative to the first component 4. The retaining member 12 may be at least partially received within the bore 4a of the first component 4. The retaining member 12 may form an interference fit with the bore 4a. For example, a body portion 12d of the retaining member 12 may form an interference fit with the bore 4a. The body portion 12d may be substantially annular. A rim portion 12c of the retaining member 12 may extend radially outward from the body portion.
As depicted in Figure 1, the bore may comprise a counterbore 4a’. The rim portion 12c of the retaining member may be received within the counterbore 4a’. In some arrangements, the rim portion 12c may form an interference with the counterbore. In such arrangements, the body portion 12d may also form an interference fit with the bore 4a or the body portion 12d may form a clearance fit with the bore 4a.
As shown in Figure 1, the fastener 10 may be axially movable relative to the retaining member 12. The retaining member may be configured to act against the fastener 10 to resist the removal of the shank 10a from the bore 4a.
With reference to Figure 2, the retaining member 12 may comprise an opening 12a configured to receive the shank 10a of the fastener. The retaining member 12 may further comprise one or more grip members 12b. The grip members 12b may extend radially inwards from the body portion 12d of the retaining member 12 towards the opening 12a. As shown in Figure 2, the grip members 12b may extend in a direction comprising a component in a direction of a central axis of the fastener shank 10a. Grip surfaces 12e may be provided at distal ends of each of the grip members 12b. The grip surfaces 12e may at least partially define the opening 12a.
With reference to Figure 3a, in some arrangements, the retaining member 12 may comprise a plurality of grip members 12b arranged circumferentially about the body portion lOd. The grip members 12b may be separated by gaps between the body portion 12d and the opening 12a in which no grip member is provided. As shown in Figure 3a, sidewalls 12b’ of the grip portions may extend in a substantially radial direction of the retaining member 12. The grip members 12b may be resilient. When the shank 10a of the fastener is inserted into the opening 12a, the grip members 12b may be deflected in order to allow the fastener 10 to be received within the opening 12a.
In the arrangements shown in Figure 3b, a single grip member 12b is provided. The single grip member extends around, e.g. completely around, the circumference of the body part 12d. The grip member 12b forms a resilient ring that may be deformed in order to allow the shank 10a to be inserted into the opening 12a of the retaining member 12.
Following installation of the shank 10a into the opening 12a, the grip members 12b may grip the fastener 10, e.g. at the grip surfaces 12e, to provide a resistance against its removal. The resistance may be at least partially due to friction between the grip surfaces 123 and the shank 4a.
With reference to Figure 2, a central portion 10b of the shank 10a may have a smaller diameter than a distal portion 10c of the shank. The central and distal portions 10b, 10c of the shank 10a may be separated by a shoulder or lip lOe. As described above, the grip members 12b may be deformed in order to allow the shank to be received within the opening 12a. Once the distal portion 10c of the shank has been received within the opening 12a, e.g. such that the grip members 12b are aligned with the central portion 10b of the shank 10a, the grip members 12a may spring back inwardly, due to their resilient nature, and the grip surfaces 12e may contact the central portion 10b of the shank 10a. The grip members 12b may be positioned to act against the shoulder lOe to resist the removal of the fastener 10 from the bore 4a. The fastener 10 may otherwise be movable, e.g. axially movable, relative to the retaining member 12, e.g. such that the grip members 12b remain aligned with the central portion 10b of the shank 10a.
In another arrangement (not shown) the retaining member 12 may be coupled to the fastener 10, e.g. fixed axially relative to the fastener 10. The fastener 10 and the retaining member 12 may be axially movable relative to the first component 4 and the retaining member 12 may act against the first component 4 to resist the removal of the shank 10a from the bore 4a.
When the first component 4 is coupled to second component 6, as shown in Figure 4, the fastener 10 may initially be tightened until a tightening torque applied to the fastener reaches a desired level. The fastener 10 may then be tightened further by turning the fastener through a desired angle. Tightening the fastener 10 in this way may allow the tensile stress in the fastener to be increased to a consistent and repeatable level, such that the fastener applies a desirable clamping force between the first and second components 4, 6. The fastener 10 may be a single use fastener and the level of tensile stress in the fastener may be greater than or equal to a yield strength of the material of the fastener 10. It may be undesirable for the fastener to be exposed to such tensile stresses more than once, and hence, if it is desirable to disassemble the first component 4 from the second components 6, it may be desirable to replace the fastener 10 before reassembling the engine assembly 2.
As shown in Figure 4, the retaining member 12 may be configured such that it is unaffected by the coupling of the first component 4 to the second component 6 using the fastener 10. For example, as shown in Figure 4, the rim portion 12c of the retaining member 12, the counterbore 4a’ and/or the second component 6 may be configured such that a load path provided between the first and second components 4, 6 does not act through the retaining member 12.
Additionally, the grip members 12b and/or the shank 10a may be configured such that the fastener 10 may be rotated without disrupting the grip members 12b or other portions of the retaining member. As the retaining member 12 is unaffected by the coupling of the first and second components 4, 6, the fastener 10 may remain captive within the bore 4a of the first component 4 following disassembly of the engine assembly 2.
In order to allow the fastener 10 to be replaced, the retaining member 12 may be configured such that during operation of the motor vehicle, eg. during operation of the engine assembly 2, the configuration of the retaining member 12 changes such that the resistance provided by the retaining member 12 against the removal of the shank 10a from the bore 4a is reduced. As described below, at least a portion, e.g. a deformable portion, of the retaining member 12 may be configured such that its shape, form and/or material phase changes during operation of the engine assembly. Additionally or alternatively, the retaining member 12 may be configured such that the material of at least a portion of the retaining member undergoes a chemical reaction during operation of the engine assembly 2.
In some arrangements, the retaining member 12 may consist of the deformable portion, e.g. substantially all of the retaining member 12 may be deformable. Alternatively, the deformable portion of the retaining member 12 may correspond to the grip members 12b, the body portion 12d, and/or the rim portion 12c. Alternatively again, the deformable portion may comprise a sector or segment of the retaining member 12.
With reference to Figure 5, the retaining member 12, may be made from a material having a low melting point, e.g. lower than or equal to an operating temperature of the first component 4 or engine assembly 2. The retaining member 12 may be made from a material having a melting temperature lower than 70 degrees Celsius or lower than 60 degrees Celsius. For example, the retaining member 12 may be made from a polymer material, such as polycaprolactone. Alternatively, the retaining member 12 may be made from a wax material. The retaining member 12 may therefore be configured to deform during operation of the motor vehicle as the engine assembly 2, e.g. the first component 4, approaches the melting point of the retaining member 12. Once the retaining member 12 has deformed, the retaining member 12 may no longer act against the fastener and/or first component 4 to resist removal of the shank 10a from the bore 4a of the first component.
In the arrangement depicted, substantially all of the retaining member 12 is made from the low melting temperature material. However, it is equally envisaged that, in some arrangements, a portion, e.g. the deformable portion, of the retaining member 12 may be made from the low melting temperature material and a remaining portion of the retaining member 12 may be made from any other desirable material, such as a higher melting temperature polymer material or a metal material.
If the engine assembly 2 continues operating at a temperature greater than the melting point of the retaining member for a period of time, e.g. such that the first component 4 reaches the temperature equal to or greater than the melting point, the retaining member 12 may at least partially melt. As show in Figure 5, the first component 4 may comprise a drain channel 4b configured to allow a melted portion 12f of the retaining member 12 to drain away from the bore 4a, such that the retaining member no longer acts against the removal of the fastener 10 from the bore 4a. As depicted, the drain channel 4b may be provided at the bottom, e.g. the lowest point, of the bore 4a, such that the melted portion flows towards the drain channel 4b under the action of gravity.
In the arrangement shown in Figure 5, the drain channel 4b forms a chamber 4c configured to receive the melted portion 12f of the retaining member, such that the melted portion 12f is retained within the first component 4. The volume of the chamber 4c may be sufficient to contain the melted portion 12f. It is also envisaged that, in other arrangements, the drain channel 4b may comprise an opening (not shown) at an end of the drain channel. The opening may be provided through the first component 4 and may be configured to allow the melted portion 12f to drain out of or away from the first component 4.
Providing the drain channel 4b to allow the melted portion to drain away may prevent the melted portion burning on to and/or staining the first component 4. Additionally or alternatively, allowing the melted portion to drain away from the first component into the drain channel 4b may prevent the melted portion contaminating other components of the engine. For example, providing the drain channel may prevent the melted portion draining into and/or contaminating an oil system of the engine.
In some arrangements, a temperature at which the material of the retaining member 12, or a portion of the retaining member, thermally decomposes may be less than or equal to an operating temperature of the engine assembly 2. Hence, the retaining member 12 may at least partially thermally decompose during operation of the engine assembly 2. The retaining member 12 may thermally decompose into gaseous elements and/or compounds, which may disperse away from the bore 4a.
Additionally or alternatively, in some arrangements, a boiling or sublimation point of the material from which the retaining member 12, or a portion of the retaining member 12, is made may be sufficiently low that at least a portion of the retaining member 12 may evaporate during operation of the engine assembly 2. The retaining member 12 may therefore no longer act to resist removal of the shank 10a from the bore 4a following operation of the engine assembly 2.
In another arrangement, the retaining member 12 may be configured to vibrate during operation of the engine assembly 2. The retaining member 12 may be configured such that a natural frequency of vibration of the retaining member is substantially equal to an operating frequency of the motor vehicle, e.g. a running speed of the engine, such as an idle speed of the engine. For example, the length and/or thickness of the grip members 12b and/or the stiffness of the material of the retaining member 12 may be configured in order to achieve a desired natural frequency of vibration. The natural frequency of vibration of the retaining member may vary according to the temperature of the retaining member. In some arrangements, the retaining member 12 may be configured such that the natural frequency of the retaining member 12 is substantially equal to the running frequency of the engine at the operating temperature of the engine. The magnitude of vibration of the retaining member during operation of the engine assembly 2 may therefore be large.
In some arrangements, the retaining member 12, or the deformable portion of the retaining member, may be made from a brittle material such that vibration of the retaining member causes at least a portion of the retaining member to fracture. The retaining member 12 may be configured to fracture into a plurality of fragments during operation of the engine assembly 12. Alternatively, the retaining member may be configured such that the deformable portion of the retaining member 12 breaks away from a remaining portion of the retaining member.
Following fracture of the retaining member 12, the resistance provided by the retaining member 12 against the removal of the shank 10a of the fastener 10 from the bore 4a of the first component 4 may be reduced. For example, fracture of the retaining member 12 may occur at or near one or more of the grip members 12b. The friction force between the grip surfaces 12e and the shank 4a may therefore be reduced. Additionally or alternatively, a fractured grip member 12b may not act against the shoulder 4d to resist removal of the shank 10a from the bore 4a.
In some arrangements, the retaining member 12 may be configured such that vibration of the retaining member 12 leads to the material of the retaining member being work hardened. Work hardening may occur due to the vibration of the engine assembly 2 repeatedly applying a strain to the retaining member 12. Work hardening may cause the material of the retaining member to become brittle. Hence, the retaining member may be more liable to fracture as the length of time over which the engine assembly 2 is operated increases.
Configuring the retaining member 12 such that it becomes brittle during operation of the engine assembly 2 may allow the retaining member 12 to be sufficiently tough prior to assembly of the of the engine assembly 2 to suitably resist the removal of the fastener 10 from the bore 4a.
In some arrangements, vibration of the retaining member 12 during operation of the engine assembly may not itself cause the retaining member to fracture. However, the work hardening of the retaining member during the operation of the engine assembly may cause the retaining member 12 to fracture when an attempt is made to remove the fastener 10 from the bore 4a, such that the retaining member 12 no longer acts to resist removal of the fastener.
With reference to Figure 6, in some arrangements, the retaining member 12 may not comprise the grip members 12b. In such arrangements, the body portion 12d of the retaining member 12 may form the opening 12a and/or may be configured to form an engineering fit, e.g. an interference fit, with the fastener 10. The retaining member 12 may thereby resist removal of the fastener 10 from the opening 12a due to friction resulting from the fit between the fastener shank 10a and the body portion 12d. The engineering fit formed between the fastener 10 and the retaining member 12 may be configured to allow the fastener 10 to be rotated, such that the first component 4 may be coupled to the second component 6, without affecting the ability of the retaining member to resist removal of the fastener 10 from the bore 4a.
It will be appreciated by those skilled in the art that although the invention has been described by way of example, with reference to one or more exemplary examples, it is not limited to the disclosed examples and that alternative examples could be constructed without departing from the scope of the invention as defined by the appended claims.

Claims (21)

Claims
1. A fastener assembly for a motor vehicle, the fastener assembly comprising: a fastener configured to couple a first component to a second component of the motor vehicle, the fastener comprising a shank configured to be received within a bore of the first component; and a retaining member, the retaining member being couplable to the fastener and the first component, the retaining member comprising an opening configured to receive the fastener shank and to provide a resistance against the removal of the fastener shank from the bore of the first component, wherein the retaining member comprises a deformable portion configured to deform from a first state to a second state by virtue of the operating environment of the first component such that the fastener may be removed from the bore of the first component when the deformable portion is in the second state following operation of the motor vehicle.
2. The fastener assembly, of claim 1, wherein the deformable portion has a melting point less than or equal an operating temperature of the first component.
3. The fastener assembly according to claim 1 or 2, wherein the deformable portion is made from a polymer material.
4. The fastener assembly according to claim 1 to 2, wherein the deformable portion is made from a wax material.
5. The fastener assembly of any of the preceding claims, wherein the retaining member consists of the deformable portion.
6. The fastener assembly of any of the preceding claims, wherein the retaining member is configured to at least partially melt during operation of the motor vehicle.
7. The fastener assembly of any of the preceding claims, wherein the retaining member is configured such that at least a portion of the retaining member evaporates during operation of the motor vehicle.
8. The fastener assembly of any of the preceding claims, wherein the retaining member is configured to vibrate during operation of the motor vehicle.
9. The fastener assembly of any of the preceding claims, wherein the retaining member is configured such that a natural frequency of vibration of the retaining member is substantially equal to an operating frequency of the motor vehicle.
10. The fastener assembly of claim 9, wherein the retaining member is configured such that the natural frequency of the retaining member varies according to the temperature of the retaining member.
11. The fastener assembly of any of the preceding claims, wherein the retaining member is configured to fracture into a plurality of fragments during operation of the engine assembly.
12. The fastener assembly of any of the preceding claims, wherein the retaining member is configured to be at least partially received within the bore.
13. The fastener assembly of claim 12, wherein the bore and/or the retaining member is configured such that the retaining member forms an interference fit with the bore.
14. The fastener assembly of any of the preceding claims, wherein the fastener shank comprises a mid portion and a distal portion, the mid portion having a smaller diameter than the distal portion, the mid portion and the distal portion being separated by a shoulder; wherein the retaining member acts against the shoulder in order to provide resistance against the removal of the fastener.
15. The fastener assembly of claims 14, wherein the retaining member is couplable to the fastener by inserting the shank of the fastener through the opening such that the retaining member engages the shoulder of the fastener shank.
16. The fastener assembly of any of the preceding claims, wherein the retaining member comprises one or more resilient grip elements configured to deform in order to allow the fastener to be inserted through the opening, the resilient grip elements configured to grip the fastener to couple the fastener to the retaining member.
17. The fastener assembly of any of the preceding claims, wherein the fastener is a single use fastener.
18. An engine assembly for a motor vehicle, the engine assembly comprising: the fastener assembly of any of the preceding claims; and the first component.
19. The engine assembly of claim 18 when depending on claim 6, wherein the first component comprises a drain channel, the drain channel being configured to allow a melted portion of the retaining member to drain away from the bore.
20. The engine assembly of claim 18 or 19 when depending on claim 6, wherein the first component comprises a chamber, the chamber being configured such that a melted portion of the retaining member is received within the chamber.
21. A fastener assembly or engine assembly substantially as described herein, with reference to and as shown in the drawings.
GB1609990.5A 2016-06-08 2016-06-08 A fastener assembly Expired - Fee Related GB2551159B (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB1609990.5A GB2551159B (en) 2016-06-08 2016-06-08 A fastener assembly
CN201710402710.0A CN107477062B (en) 2016-06-08 2017-06-01 Fastener assembly
US15/615,282 US10935066B2 (en) 2016-06-08 2017-06-06 Fastener assembly
DE102017112651.1A DE102017112651A1 (en) 2016-06-08 2017-06-08 mounting assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1609990.5A GB2551159B (en) 2016-06-08 2016-06-08 A fastener assembly

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GB201609990D0 GB201609990D0 (en) 2016-07-20
GB2551159A true GB2551159A (en) 2017-12-13
GB2551159B GB2551159B (en) 2018-06-20

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CN (1) CN107477062B (en)
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US20200147768A1 (en) * 2018-11-13 2020-05-14 Katerra Inc. Captive fastener

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GB201609990D0 (en) 2016-07-20
GB2551159B (en) 2018-06-20
DE102017112651A1 (en) 2017-12-14
CN107477062A (en) 2017-12-15
US20170356484A1 (en) 2017-12-14
CN107477062B (en) 2020-12-25
US10935066B2 (en) 2021-03-02

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