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GB2151741A - Blind rivet - Google Patents

Blind rivet Download PDF

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Publication number
GB2151741A
GB2151741A GB08431513A GB8431513A GB2151741A GB 2151741 A GB2151741 A GB 2151741A GB 08431513 A GB08431513 A GB 08431513A GB 8431513 A GB8431513 A GB 8431513A GB 2151741 A GB2151741 A GB 2151741A
Authority
GB
United Kingdom
Prior art keywords
rivet
insert
tail
region
mandrel
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
GB08431513A
Other versions
GB8431513D0 (en
GB2151741B (en
Inventor
Arnold Birks
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.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
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 British Aerospace PLC filed Critical British Aerospace PLC
Publication of GB8431513D0 publication Critical patent/GB8431513D0/en
Publication of GB2151741A publication Critical patent/GB2151741A/en
Application granted granted Critical
Publication of GB2151741B publication Critical patent/GB2151741B/en
Expired legal-status Critical Current

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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
    • F16B19/00Bolts without screw-thread; Pins, including deformable elements; Rivets
    • F16B19/04Rivets; Spigots or the like fastened by riveting
    • F16B19/08Hollow rivets; Multi-part rivets
    • F16B19/10Hollow rivets; Multi-part rivets fastened by expanding mechanically
    • F16B19/1027Multi-part rivets
    • F16B19/1036Blind rivets
    • F16B19/1045Blind rivets fastened by a pull - mandrel or the like

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Insertion Pins And Rivets (AREA)

Abstract

A blind rivet comprises a plastics insert 6 which is drawn by a metal mandrel (not shown) into the tail 11 of a plastics rivet body 5 to expand said tail 11 and thus set the rivet. Subsequent to setting, the mandrel is drawn completely through and out of the set rivet body 5 and insert 6. The insert 6 has one region having an external diameter similar to the internal diameter of the rivet body tail 11, and a larger diameter region for expanding the tail 11. Dimensions and tolerances are specified. <IMAGE>

Description

SPECIFICATION Rivet arrangement This invention relates to rivet arrangements According to one aspect of the present invention, a rivet arrangement comprises a rivet having a tubular tail or resiliently deformable material, and an insert adapted to be urged into and remain within the tail to effect setting the rivet, the insert having two regions of differing external diameter, a first region having a diameter similar to the internal diameter of the rivet tail, and a second region being of a diameter to effect substantial expansion of the tail whereby when the rivet is placed to extend through an aperture in work pieces to be joined, the insert can be urged into the said tail until its first region protrudes into a region of the tail constrained by a work piece, at which stage the second region of the insert has expanded the tail at a desired position to effect rivet setting.
Preferably, both the rivet and the insert are of a resiliently deformable plastics material, for example a nylon or nylon-like material. Additionally, both items are preferably of tubular form. In this case, the rivet and the insert can be mounted in tandem on a headed mandrel for insertion into a blind aperture in the work pieces and withdrawal of the mandrel through the rivet head used to effect setting of the rivet. Unlike some well-known rivet arrangements, the mandrel is preferably totally withdrawn and is not severed to remain partially within the set rivet arrangement. This is possible due to the resilience of the insert and the rivet.
These and other aspects of the invention are disclosed in the exemplary description of one embodiment of the invention with reference to the accompanying drawings in which: Figure 1 is a cross-sectional view of a set rivet arrangement; Figure 2 is a cross-sectional view of an unset rivet assembly, Figure 3 is a cross-sectional view of a rivet plus a table of dimensions suitable for use in a hole formed by Drill Morse No. 11 (0.191" dia.), and Figure 4 is a cross-sectional view of an insert plus a table of dimensions suitable for use with the rivet of Figure 3.
In Figure 1, a rivet arrangement attaches a layer of material 1 to a composite structure comprising a skin 2 bonded to a core material 3. A bonding and sealing agent may also be used to aid attachment.
A blind hole 4 of sufficient depth to allow insertion of a rivet assembly is formed in the work piece 1, 2 and 3. Into this hole is inserted the assembly of Figure 2 comprising a rivet 5 (see Figure 3), an insert 6 (see Figure 4) and a steel mandrel 7, the rivet and the insert being mounted in tandem upon the mandrel as shown.
The rivet 5 has a head region 10 and a tail or shank region 11.
The mandrel has a constant diameter shank 8 which extends through the rivet and the insert when they are undeformed and a head region 9 of enlarged diameter which engages and draws the insert 6 into the tail 11 but effects temporary deformation thereof to exit completely. To set the rivet arrangement, the assembly of Figure 2 is inserted into the blind hole 4 and the mandrel 7 is withdrawn whilst the rivet is held in the position shown. This is effected by a known form of riveting machine, for example a Tucker TT 55 with a slightly modified nose. The modification comprises a counterbore to the tube through which the mandrel is drawn of sufficient diameter to accept the mandrel head 8 as it exits from the rivet 5.
As can be seen, mandrel withdrawal caused the insert 6 to be drawn axially into the rivet tail 11 temporarily and locally causing it to expand until the insert finally achieves the position illustrated in Figure 1 in which its region of diameter M protrudes into the hole formed in the layer 2. This layer is relatively rigid material and therefore stops further axial movement by constraining the tail 11.
The region of the insert of diameter R maintains the rivet tail 11 in a locally expanded condition protruding locally into the core material 3 to both clamp the core material and the two layers 1 and 2 together. The head 9 of the mandrel is allowed to pass through the insert 6 and the rivet 5 at this stage due to the resilience of their material.
The insert shape is of significance in that (a) its external diameter R must pass into the hole 4, (b) its transition shape X between diameters M and R is selected to be smoothly curved to cause rivet tail expansion without splitting, (c) its diameter M and length T are chosen to intrude into that portion of the rivet tail constrained by the relatively rigid material of the layer 2 to give positive permanent rivet deformation and, moreover, to give radial location during the setting process as the insert travels along the rivet.
The mandrel is a standard "off the shelf" item and for the rivet sizes described is referenced AGS 2052-3-25 in the Society of British Aerospace Companies Limited published engineering standards.
The illustrated arrangement is particularly useful for anchoring glass fibre clamping strips (e.g. layer 1) to radomes (items 2 and 3), the clamping strips themselves being utilised to clamp aluminium alloy lightning conductor strips to the radome.
1. A rivet arrangement comprises a rivet having a tubular tail of resiliently deformable material, and an insert adapted be urged into and remain within the tail to effect setting the rivet, the insert having two regions of differing external diameter, a first region having a diameter similar to the internal diameter of the rivet tail, and a second region being of a diameter to effect substantial expansion of the tail whereby when the rivet is placed to extend through an aperture in work pieces to be joined, the insert can be urged into the said tail until its first region protrudes into a region of the tail constrained by a work piece, at which stage the second region of the insert has expanded the tail at a
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (5)

**WARNING** start of CLMS field may overlap end of DESC **. SPECIFICATION Rivet arrangement This invention relates to rivet arrangements According to one aspect of the present invention, a rivet arrangement comprises a rivet having a tubular tail or resiliently deformable material, and an insert adapted to be urged into and remain within the tail to effect setting the rivet, the insert having two regions of differing external diameter, a first region having a diameter similar to the internal diameter of the rivet tail, and a second region being of a diameter to effect substantial expansion of the tail whereby when the rivet is placed to extend through an aperture in work pieces to be joined, the insert can be urged into the said tail until its first region protrudes into a region of the tail constrained by a work piece, at which stage the second region of the insert has expanded the tail at a desired position to effect rivet setting. Preferably, both the rivet and the insert are of a resiliently deformable plastics material, for example a nylon or nylon-like material. Additionally, both items are preferably of tubular form. In this case, the rivet and the insert can be mounted in tandem on a headed mandrel for insertion into a blind aperture in the work pieces and withdrawal of the mandrel through the rivet head used to effect setting of the rivet. Unlike some well-known rivet arrangements, the mandrel is preferably totally withdrawn and is not severed to remain partially within the set rivet arrangement. This is possible due to the resilience of the insert and the rivet. These and other aspects of the invention are disclosed in the exemplary description of one embodiment of the invention with reference to the accompanying drawings in which: Figure 1 is a cross-sectional view of a set rivet arrangement; Figure 2 is a cross-sectional view of an unset rivet assembly, Figure 3 is a cross-sectional view of a rivet plus a table of dimensions suitable for use in a hole formed by Drill Morse No. 11 (0.191" dia.), and Figure 4 is a cross-sectional view of an insert plus a table of dimensions suitable for use with the rivet of Figure 3. In Figure 1, a rivet arrangement attaches a layer of material 1 to a composite structure comprising a skin 2 bonded to a core material 3. A bonding and sealing agent may also be used to aid attachment. A blind hole 4 of sufficient depth to allow insertion of a rivet assembly is formed in the work piece 1, 2 and 3. Into this hole is inserted the assembly of Figure 2 comprising a rivet 5 (see Figure 3), an insert 6 (see Figure 4) and a steel mandrel 7, the rivet and the insert being mounted in tandem upon the mandrel as shown. The rivet 5 has a head region 10 and a tail or shank region 11. The mandrel has a constant diameter shank 8 which extends through the rivet and the insert when they are undeformed and a head region 9 of enlarged diameter which engages and draws the insert 6 into the tail 11 but effects temporary deformation thereof to exit completely. To set the rivet arrangement, the assembly of Figure 2 is inserted into the blind hole 4 and the mandrel 7 is withdrawn whilst the rivet is held in the position shown. This is effected by a known form of riveting machine, for example a Tucker TT 55 with a slightly modified nose. The modification comprises a counterbore to the tube through which the mandrel is drawn of sufficient diameter to accept the mandrel head 8 as it exits from the rivet 5. As can be seen, mandrel withdrawal caused the insert 6 to be drawn axially into the rivet tail 11 temporarily and locally causing it to expand until the insert finally achieves the position illustrated in Figure 1 in which its region of diameter M protrudes into the hole formed in the layer 2. This layer is relatively rigid material and therefore stops further axial movement by constraining the tail 11. The region of the insert of diameter R maintains the rivet tail 11 in a locally expanded condition protruding locally into the core material 3 to both clamp the core material and the two layers 1 and 2 together. The head 9 of the mandrel is allowed to pass through the insert 6 and the rivet 5 at this stage due to the resilience of their material. The insert shape is of significance in that (a) its external diameter R must pass into the hole 4, (b) its transition shape X between diameters M and R is selected to be smoothly curved to cause rivet tail expansion without splitting, (c) its diameter M and length T are chosen to intrude into that portion of the rivet tail constrained by the relatively rigid material of the layer 2 to give positive permanent rivet deformation and, moreover, to give radial location during the setting process as the insert travels along the rivet. The mandrel is a standard "off the shelf" item and for the rivet sizes described is referenced AGS 2052-3-25 in the Society of British Aerospace Companies Limited published engineering standards. The illustrated arrangement is particularly useful for anchoring glass fibre clamping strips (e.g. layer 1) to radomes (items 2 and 3), the clamping strips themselves being utilised to clamp aluminium alloy lightning conductor strips to the radome. CLAIMS
1. A rivet arrangement comprises a rivet having a tubular tail of resiliently deformable material, and an insert adapted be urged into and remain within the tail to effect setting the rivet, the insert having two regions of differing external diameter, a first region having a diameter similar to the internal diameter of the rivet tail, and a second region being of a diameter to effect substantial expansion of the tail whereby when the rivet is placed to extend through an aperture in work pieces to be joined, the insert can be urged into the said tail until its first region protrudes into a region of the tail constrained by a work piece, at which stage the second region of the insert has expanded the tail at a desired position to effect rivet setting.
2. A rivet arrangement according to Claim 1 wherein both the rivet and the insert are of a resiliently deformable plastics material.
3. A rivet arrangement according to Claim 2 wherein the insert has a transition region between its first and second regions of different external diameter, shaped to prevent splitting of the tubular tail of the rivet by having an annular concave curvature portion blending with the first region, an annular convex curvature portion blending with the second region, the concave and convex portions themselves blending with one another.
4. A rivet assembly suitable for blind rivetting comprising a mandrel and the rivet arrangement of Claim 3, the mandrel having a shank portion and a head portion, the two components of the rivet arrangement being mounted in tandem upon the mandrel shank with the insert lying adjacent the mandrel head, and the shank protruding through both components, the rivet having a portion of reduced internal diameter to lightly grip the shank of the mandrel.
5. A rivet arrangement substantially as described with reference to the Figures.
GB08431513A 1983-12-21 1984-12-13 Blind rivet Expired GB2151741B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB838334095A GB8334095D0 (en) 1983-12-21 1983-12-21 Rivet arrangement

Publications (3)

Publication Number Publication Date
GB8431513D0 GB8431513D0 (en) 1985-01-23
GB2151741A true GB2151741A (en) 1985-07-24
GB2151741B GB2151741B (en) 1987-09-30

Family

ID=10553649

Family Applications (2)

Application Number Title Priority Date Filing Date
GB838334095A Pending GB8334095D0 (en) 1983-12-21 1983-12-21 Rivet arrangement
GB08431513A Expired GB2151741B (en) 1983-12-21 1984-12-13 Blind rivet

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB838334095A Pending GB8334095D0 (en) 1983-12-21 1983-12-21 Rivet arrangement

Country Status (1)

Country Link
GB (2) GB8334095D0 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0264870A1 (en) * 1986-10-20 1988-04-27 The B.F. Goodrich Company Fasteners for honeycomb structures
GB2220454A (en) * 1988-05-27 1990-01-10 Avdel Ltd Blind rivet
US5074726A (en) * 1988-11-28 1991-12-24 The B. F. Goodrich Company Blind fastener
US10214923B2 (en) 2014-12-16 2019-02-26 20 Emma 20 S.L. Sealing plug for closing holes in walls and the like

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB472329A (en) * 1936-03-26 1937-09-22 A T S Company Ltd Improvements in and relating to rivets and rivetting
GB1066033A (en) * 1963-08-30 1967-04-19 Avdel Ltd Improvements in or relating to blind rivet fastening devices
GB1124749A (en) * 1964-11-27 1968-08-21 Textron Ind Inc Rivet assemblies and methods of riveting therewith
GB1548880A (en) * 1975-07-23 1979-07-18 Tucker Fasteners Ltd Blind riveting
GB2097083A (en) * 1981-04-21 1982-10-27 Gkn Screws Fasteners Ltd Blind rivet
GB2127514A (en) * 1982-09-28 1984-04-11 Huck Mfg Co Two piece blind fastener

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB472329A (en) * 1936-03-26 1937-09-22 A T S Company Ltd Improvements in and relating to rivets and rivetting
GB1066033A (en) * 1963-08-30 1967-04-19 Avdel Ltd Improvements in or relating to blind rivet fastening devices
GB1124749A (en) * 1964-11-27 1968-08-21 Textron Ind Inc Rivet assemblies and methods of riveting therewith
GB1548880A (en) * 1975-07-23 1979-07-18 Tucker Fasteners Ltd Blind riveting
GB2097083A (en) * 1981-04-21 1982-10-27 Gkn Screws Fasteners Ltd Blind rivet
GB2127514A (en) * 1982-09-28 1984-04-11 Huck Mfg Co Two piece blind fastener

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0264870A1 (en) * 1986-10-20 1988-04-27 The B.F. Goodrich Company Fasteners for honeycomb structures
GB2220454A (en) * 1988-05-27 1990-01-10 Avdel Ltd Blind rivet
US5074726A (en) * 1988-11-28 1991-12-24 The B. F. Goodrich Company Blind fastener
US10214923B2 (en) 2014-12-16 2019-02-26 20 Emma 20 S.L. Sealing plug for closing holes in walls and the like

Also Published As

Publication number Publication date
GB8431513D0 (en) 1985-01-23
GB8334095D0 (en) 1984-02-01
GB2151741B (en) 1987-09-30

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PCNP Patent ceased through non-payment of renewal fee