EP1702697A1 - Over-sealing - Google Patents

Over-sealing Download PDF

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Publication number
EP1702697A1
EP1702697A1 EP05102047A EP05102047A EP1702697A1 EP 1702697 A1 EP1702697 A1 EP 1702697A1 EP 05102047 A EP05102047 A EP 05102047A EP 05102047 A EP05102047 A EP 05102047A EP 1702697 A1 EP1702697 A1 EP 1702697A1
Authority
EP
European Patent Office
Prior art keywords
tool
collar
sealant
notch
fastener head
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.)
Withdrawn
Application number
EP05102047A
Other languages
German (de)
French (fr)
Inventor
Adrian Paul Jones
John Ciaran BAE Systems plc Harrott
James William Law BAE Systems plc Woolley
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
BAE Systems 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 BAE Systems PLC filed Critical BAE Systems PLC
Priority to EP05102047A priority Critical patent/EP1702697A1/en
Publication of EP1702697A1 publication Critical patent/EP1702697A1/en
Withdrawn legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00Riveting
    • B21J15/38Accessories for use in connection with riveting, e.g. pliers for upsetting; Hand tools for riveting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00Riveting
    • B21J15/10Riveting machines
    • B21J15/14Riveting machines specially adapted for riveting specific articles, e.g. brake lining machines
    • B21J15/142Aerospace structures

Definitions

  • This invention relates to the over-sealing of the heads of fasteners, particularly to the over-sealing of aircraft electrical bond rivets.
  • rivets or fasteners To meet electrical earth bond requirements on aircraft, one in every 10 or so rivets or fasteners is an earth bonding point. This is so that minimum resistance is achieved between mating panels forming the outer surface of the aircraft, allowing any external current such as a lightning strike to pass freely through the aircraft and mitigating the damaging effects of electrical discharge. Once the correct low resistance is achieved the whole fastener (rivet or bolt) is covered, where they are visible on the surfaces of the panels, both head and tail, in a liquid rubber solution.
  • This sealant is an electrically conductive corrosion inhibitive material, and it encloses the fastener earth point from the atmosphere, which otherwise could contact and corrode the joint.
  • Corrosion increases electrical resistance; an increase in resistance would not allow unwanted current to pass freely and could result in serious electrical malfunctions within the aircraft. This is known as "over-sealing".
  • PRC liquid rubber solution
  • PRC-DeSoto International, Inc polysulphide rubber compound
  • Conventional practice is to apply a liquid rubber solution referred to as "PRC” ("polysulphide rubber compound” - PRC is a trademark of PRC-DeSoto International, Inc) by hand; the solution is applied to the head of the rivet and the immediately surrounding area, so as to encapsulate the rivet head, using a wire, stick or brush. The solution is built up by swirling the solution over the rivet head to completely encapsulate it. This is a time-consuming and messy task, which often results in an untidy result.
  • the present invention provides a tool for applying sealant to cover a fastener head on the surface of a workpiece, the tool comprising a cylindrical member having an internal diameter greater than the diameter of the fastener head, the member having a notch in its circumference and near to one end to form a collar.
  • Such an arrangement provides a cheap and easy-to-use tool which saves time compared with conventional practice and which results in a far neater and more accurate job (accuracy being especially important in aerospace applications).
  • the tool is used by immersing at least the collar in a liquid sealant long enough for the collar to pick up by the action of surface tension an amount of sealant, and placing the edge of the collar over and around the fastener head so as to deposit the sealant thereover. This is fast and produces reliable and neat, accurate encapsulation, enabling multiple rivet heads to be covered far more effectively than with known methods.
  • At least a part of the notch adjacent the said end of the member is substantially parallel to the said end.
  • the height of the collar relative to its circumference is preferably determined by several factors, such as the viscosity and surface tension of the sealant and the amount of sealant required, so as to ensure the rivet head is covered effectively.
  • the tool is easily cleaned by brushing or wiping, and the notch assists in this process by allowing access to the inside of the collar.
  • the side of the notch distant from the said end of the member is at an acute angle to the longitudinal axis of the cylindrical member. This creates a wide notch so as to facilitate easy cleaning of the tool.
  • the central axis of the collar is at an angle to the longitudinal axis of the cylindrical member. This further facilitates cleaning, as it effectively "opens up" the notch if the member is bent somewhere along the length of the notch, it also enables the tool to access rivets which are in awkward, difficult to access, locations.
  • the tool 2 shown in Figure 1 comprises a hollow cylindrical shank 4 and an annular collar section 6, which has been formed by cutting a notch 8 into the cylinder.
  • the resulting structure has been bent so that the axes of the collar 6 and shank 4 are inclined.
  • the tool is cheap and easy to fabricate from a cylinder of suitable diameter.
  • Use of this tool is also very simple: the collar 6 is dipped into a liquid sealant solution (not shown) so that it "picks up” an amount of the sealant by surface tension (in much the same way that a child's bubble-blowing ring pick ups soap solution for blowing a soap bubble).
  • the tool is then moved and the collar 6 placed over a rivet head (not shown, but which in aircraft applications is usually countersunk so as to be flush with the aircraft surface, but which could equally be rounded flat or pan-shaped).
  • a rivet head not shown, but which in aircraft applications is usually countersunk so as to be flush with the aircraft surface, but which could equally be rounded flat or pan-shaped.
  • Figure 2 illustrates the tool 2 of Figure 1 together with two other tools, 2 and 2b (in which equivalent elements to those of the tool 2 are identified by the suffixes "a" and "b").
  • Tool 2a is similar to tool 2, but has been bent adjacent the end of the notch 8a distant from the collar 6a.
  • Tool 2b has been bent at a point along the shank 4b, so that the notch 8b is substantially undistorted (and resembles the cut out position of a whistle, or organ pipe).

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

Abstract

A tool (2,2a,2b) for over-sealing rivet heads comprising an annular collar (6,6a,6b) formed by notching (8,8a,8b) the end of a cylinder (4,4a,4b) of appropriate diameter. The collar is dipped into the liquid sealant to pick up some and them placed over the rivet head to as to encapsulate it with liquid sealant, which then sets.

Description

  • This invention relates to the over-sealing of the heads of fasteners, particularly to the over-sealing of aircraft electrical bond rivets.
  • To meet electrical earth bond requirements on aircraft, one in every 10 or so rivets or fasteners is an earth bonding point. This is so that minimum resistance is achieved between mating panels forming the outer surface of the aircraft, allowing any external current such as a lightning strike to pass freely through the aircraft and mitigating the damaging effects of electrical discharge. Once the correct low resistance is achieved the whole fastener (rivet or bolt) is covered, where they are visible on the surfaces of the panels, both head and tail, in a liquid rubber solution. This sealant is an electrically conductive corrosion inhibitive material, and it encloses the fastener earth point from the atmosphere, which otherwise could contact and corrode the joint. Corrosion increases electrical resistance; an increase in resistance would not allow unwanted current to pass freely and could result in serious electrical malfunctions within the aircraft. This is known as "over-sealing". Conventional practice is to apply a liquid rubber solution referred to as "PRC" ("polysulphide rubber compound" - PRC is a trademark of PRC-DeSoto International, Inc) by hand; the solution is applied to the head of the rivet and the immediately surrounding area, so as to encapsulate the rivet head, using a wire, stick or brush. The solution is built up by swirling the solution over the rivet head to completely encapsulate it. This is a time-consuming and messy task, which often results in an untidy result.
  • The present invention provides a tool for applying sealant to cover a fastener head on the surface of a workpiece, the tool comprising a cylindrical member having an internal diameter greater than the diameter of the fastener head, the member having a notch in its circumference and near to one end to form a collar.
  • Such an arrangement provides a cheap and easy-to-use tool which saves time compared with conventional practice and which results in a far neater and more accurate job (accuracy being especially important in aerospace applications). The tool is used by immersing at least the collar in a liquid sealant long enough for the collar to pick up by the action of surface tension an amount of sealant, and placing the edge of the collar over and around the fastener head so as to deposit the sealant thereover. This is fast and produces reliable and neat, accurate encapsulation, enabling multiple rivet heads to be covered far more effectively than with known methods.
  • Preferably, at least a part of the notch adjacent the said end of the member is substantially parallel to the said end. This creates an annular collar, so that in use a consistent amount of sealant is picked up and deposited over each rivet head. The height of the collar relative to its circumference is preferably determined by several factors, such as the viscosity and surface tension of the sealant and the amount of sealant required, so as to ensure the rivet head is covered effectively.
  • Once the sealant has been deposited, the tool is easily cleaned by brushing or wiping, and the notch assists in this process by allowing access to the inside of the collar. Preferably the side of the notch distant from the said end of the member is at an acute angle to the longitudinal axis of the cylindrical member. This creates a wide notch so as to facilitate easy cleaning of the tool. Additionally or alternatively the central axis of the collar is at an angle to the longitudinal axis of the cylindrical member. This further facilitates cleaning, as it effectively "opens up" the notch if the member is bent somewhere along the length of the notch, it also enables the tool to access rivets which are in awkward, difficult to access, locations.
  • The invention will now be described by way of example and with reference to the accompanying drawings, in which:
    • Figure 1 shows an embodiment of a tool in accordance with the invention, and
    • Figure 2 shows the tool of Figure 1 with other embodiments of the tool in accordance with the invention.
  • The tool 2 shown in Figure 1 comprises a hollow cylindrical shank 4 and an annular collar section 6, which has been formed by cutting a notch 8 into the cylinder. In addition, the resulting structure has been bent so that the axes of the collar 6 and shank 4 are inclined. The tool is cheap and easy to fabricate from a cylinder of suitable diameter. Use of this tool is also very simple: the collar 6 is dipped into a liquid sealant solution (not shown) so that it "picks up" an amount of the sealant by surface tension (in much the same way that a child's bubble-blowing ring pick ups soap solution for blowing a soap bubble). The tool is then moved and the collar 6 placed over a rivet head (not shown, but which in aircraft applications is usually countersunk so as to be flush with the aircraft surface, but which could equally be rounded flat or pan-shaped). As the collar 6 contacts the surface the liquid solution adheres to the surface and the rivet and, as the tool 2 is removed, is deposited there, neatly encapsulating the rivet.
  • Figure 2 illustrates the tool 2 of Figure 1 together with two other tools, 2 and 2b (in which equivalent elements to those of the tool 2 are identified by the suffixes "a" and "b"). Tool 2a is similar to tool 2, but has been bent adjacent the end of the notch 8a distant from the collar 6a. Tool 2b has been bent at a point along the shank 4b, so that the notch 8b is substantially undistorted (and resembles the cut out position of a whistle, or organ pipe).
  • Although described in relation to the application of a sealant to fastener heads, it will be appreciated that principles of the present invention have other applications, where there is a requirement to encapsulate something with a liquid, setting solution, such as in certain medical applications.

Claims (6)

  1. A tool for applying sealant to cover a fastener head on the surface of a workpiece, the tool comprising a cylindrical member having an internal diameter greater than the diameter of the fastener head, the member having a notch in its circumference and near to one end to form a collar.
  2. A tool according to claim 1 wherein at least a part of the notch adjacent the said end of the member being substantially parallel to the said end.
  3. A tool according to Claim 1 or 2 wherein the side of the notch distant from the said end of the member is at an acute angle to the longitudinal axis of the cylindrical member.
  4. A tool according any of claims 1 to 3 wherein the central axis of the collar is at an angle to the longitudinal axis of the cylindrical member.
  5. A tool substantially as hereinbefore described and with reference to the accompanying drawing.
  6. A method of applying sealant to cover a fastener head on the surface of a workpiece using a tool according to any preceding claim, the method comprising immersing at least the collar in a liquid sealant long enough for the collar to pick up by the action of surface tension an amount of sealant, and placing the edge of the collar over and around the fastener head so as to deposit the sealant thereover.
EP05102047A 2005-03-15 2005-03-15 Over-sealing Withdrawn EP1702697A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP05102047A EP1702697A1 (en) 2005-03-15 2005-03-15 Over-sealing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP05102047A EP1702697A1 (en) 2005-03-15 2005-03-15 Over-sealing

Publications (1)

Publication Number Publication Date
EP1702697A1 true EP1702697A1 (en) 2006-09-20

Family

ID=34938986

Family Applications (1)

Application Number Title Priority Date Filing Date
EP05102047A Withdrawn EP1702697A1 (en) 2005-03-15 2005-03-15 Over-sealing

Country Status (1)

Country Link
EP (1) EP1702697A1 (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1136259A2 (en) * 2000-03-24 2001-09-26 Nicolae Dr. Barsan Applicator device for locally applying viscous or liquid materials in defined quantity
US6461458B1 (en) * 1999-04-20 2002-10-08 Bae Systems Plc Method of sealing a panel to an aircraft structure

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6461458B1 (en) * 1999-04-20 2002-10-08 Bae Systems Plc Method of sealing a panel to an aircraft structure
US20030015278A1 (en) * 1999-04-20 2003-01-23 Bae Systems Plc Method of sealing a panel to an aircraft structure
EP1136259A2 (en) * 2000-03-24 2001-09-26 Nicolae Dr. Barsan Applicator device for locally applying viscous or liquid materials in defined quantity

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