Embodiments of the present invention relate to fastener arrangements. They relate to fastener arrangements for gas turbine engines.
In many industries, it is desirable to fasten and clamp together a plurality of articles so that they effectively become a unitary body. For example, it is often desirable to clamp together two or more sheets of metal in the manufacture of gas turbine engines.
The fasteners which are currently used comprise a resiliently deformable head with two or more barbed arms which extend from the head. In order to insert such a fastener, it is necessary to insert the fastener into an aperture of the plurality of articles with a large insertion force so that the head may deform and allow the barbed arms to engage the plurality of articles in a clamping manner.
However, the above mentioned fasteners are not suitable for all applications. If the plurality of articles are delicate, the large insertion force needed for the fastener may damage the articles. Additionally, if there is little space around the plurality of articles, it may be difficult to provide a sufficiently large force to deform the head so that the fastener may engage the plurality of articles.
Therefore, it is desirable to provide an alternative fastener arrangement.
According to various embodiments of the present invention, there is provided a fastener arrangement for fastening two or more articles together, the two or more articles having a first length, the fastener arrangement comprising: a fastener including an elongate clamping member for being received in an aperture of the two or more articles, the elongate clamping member being moveable between a contracted configuration in which the elongate clamping member has a length which is less than the first length and a lengthened configuration in which the elongate clamping member has a length which is greater than the first length, the elongate clamping member being resiliently biased towards the contracted configuration; and an actuator for moving the elongate clamping member, while in the aperture of the two or more articles, from the contracted configuration towards the lengthened configuration to enable the elongate clamping member to protrude through the aperture and to engage the articles in a clamping manner.
The fastener arrangement may further comprise a guide. The guide may include a recess for receiving the elongate clamping member of the fastener. The guide and fastener combination may be moved through the aperture together.
The guide may include the actuator for moving the elongate clamping member. The actuator may be arranged such that when the guide is removed from the fastener when the elongate clamping member is in the aperture, the actuator acts on the elongate clamping member and moves it from the contracted configuration towards the lengthened configuration.
The fastener may comprise a substantially straight elongate holding member for being received in the aperture of the articles. The elongate holding member may have a length which is greater than the first length. The elongate holding member may be arranged to prevent the fastener from being removed from the two or more articles accidentally.
The fastener arrangement may further comprise a locking mechanism arranged to be received in the aperture, adjacent the elongate clamping member, and to prevent the fastener from being removed from the two or more articles.
When the elongate clamping member is in the contracted configuration, the elongate clamping member may have a concave profile. When the elongate clamping member is in the lengthened configuration, the elongate clamping member may have a substantially straight profile.
According to various embodiments of the present invention, there is provided a gas turbine engine comprising a fastener arrangement as described in the preceding paragraphs.
According to various embodiments of the present invention, there is provided a method of fastening two or more articles together, the two or more articles having a first length, the method comprising: providing a fastener including an elongate clamping member; inserting the elongate clamping member into an aperture of the two or more articles, the elongate clamping member being moveable between a contracted configuration in which the elongate clamping member has a length which is less than the first length and a lengthened configuration in which the elongate clamping member has a length which is greater than the first length, the elongate clamping member being resiliently biased towards the contracted configuration; and moving the elongate clamping member, while in the aperture of the two or more articles, from the contracted configuration towards the lengthened configuration to enable the elongate clamping member to protrude through the aperture and to engage the articles in a clamping manner.
The method may further comprise providing a guide which includes a recess; inserting the elongate clamping member of the fastener into the recess of the guide and moving the combination of the guide and the fastener through the aperture together.
The method may further comprise removing the guide from the fastener while the elongate clamping member is in the aperture.
When the guide is removed from the fastener, an actuator portion of the guide may act on the elongate clamping member and may move it from the contracted configuration towards the lengthened configuration.
The fastener may further comprise a substantially straight elongate holding member for being received in the aperture of the articles. The elongate holding member may have a length greater than the first length. The elongate holding member may be arranged to prevent the fastener from being removed from the two or more articles accidentally.
The fastener arrangement may further comprise providing a locking mechanism and inserting the locking mechanism in the aperture, adjacent the elongate clamping member, to prevent the fastener from being removed from the two or more articles.
When the elongate clamping member is in the contracted configuration, the elongate clamping member may have a concave profile. When the elongate clamping member is in the lengthened configuration, the elongate clamping member may have a substantially straight profile.
For a better understanding of the present invention reference will now be made by way of example only to the accompanying drawings in which:
Referring to
The gas turbine engine 10 operates in a conventional manner so that air entering the intake 11 is accelerated by the fan 12 which produce two air flows: a first air flow into the intermediate pressure compressor 13 and a second air flow which provides propulsive thrust. The intermediate pressure compressor compresses the air flow directed into it before delivering that air to the high pressure compressor 14 where further compression takes place.
The compressed air exhausted from the high pressure compressor 14 is directed into the combustor 15 where it is mixed with fuel and the mixture combusted. The resultant hot combustion products then expand through, and thereby drive, the high, intermediate and low pressure turbines 16, 17 and 18 before being exhausted through the nozzle 19 to provide additional propulsive thrust. The high, intermediate and low pressure turbines 16, 17 and 18 respectively drive the high and intermediate pressure compressors 14 and 13 and the fan 12 by suitable interconnecting shafts 20.
A Cartesian co-ordination system 28 is also illustrated which includes an X axis 30 and a Y axis 32 which are orthogonal to one another. The co-ordinate system shall be used in the following description to describe the structure of the fastener arrangement 22 in detail.
The fastener arrangement 22 includes a fastener 24 for fastening two or more articles together and a guide 26 for guiding the fastener through an aperture of the two or more articles. The fastener 24 comprises a body 34, a first elongate clamping member 36 and a second elongate clamping member 38. In this embodiment, the fastener 24 and the guide 26 comprise a metal such as titanium. However, in other embodiments the fastener 24 and the guide 26 may comprise other materials such as plastics.
The first and second elongate clamping members 36, 38 extend from the centre of the body 34 and define abutment surfaces 40 on the body 34 between where the elongate clamping members 36, 38 extend from the body 34 and the periphery of the body 34. The function of the abutment surfaces 40 will be explained in more detail in the following paragraphs with reference to
The first and second elongate clamping members 36, 38 extend from the body 34 in the +X direction and each end at a barb 42, 44 respectively. The elongate clamping members 36, 38 are moveable between a contracted configuration (as illustrated in
In this embodiment, the elongate clamping members 36, 38 have a concave profile when they are in the contracted configuration. For example if the first elongate clamping member 36 is considered, the first elongate clamping member 36 curves in the +X and −Y directions until a mid-point 46 and then curves to the barb 42 in the +X and +Y directions. If the second elongate clamping member 38 is considered, the second elongate clamping member 38 curves in the +X and +Y directions until the mid-point 46 and then curves to the barb 44 in the +X and −Y directions.
In this embodiment, the elongate clamping members 36, 38 have a straightened profile when they are in the lengthened configuration. Consequently, in the lengthened configuration the first and second elongate clamping members 36, 38 extend substantially only in the +X direction from the body 34 (it should be appreciated that the first and second elongate clamping members 36, 38 may have some curvature when in the lengthened configuration and have a small +/−Y component of extension).
The first and second elongate clamping members 36, 38 and the body 34 define a cavity 47 whose purpose will be described in the following paragraphs.
The guide 26 includes a body 48 and an actuator 50 which extends from a first end 52 of the body 48 in the −Y direction. The second end 54 of the body 48 (opposite to the first end 52) is tapered to a curved end. The first end 52 of the body 48 and the actuator 50 define a first recess 56 and a second recess 58 which are arranged to receive the barbs 42, 44 of the fastener 24.
The actuator 50 extends from the first end 52 of the body 48 in the −Y direction to form a cam lobe 60. The cam lobe 60 has a relatively low coefficient of friction and the tangent of its surface forms a relatively small angle with respect to the X axis 30. The cam lobe 60 is arranged so that it may be received in the cavity 47 of the fastener 24. The function of the cam lobe 60 will be explained in detail in the following paragraphs.
The operation of the fastener arrangement 22 will now be described in detail with reference to
The initial step is illustrated in
Prior to this step, the first and second elongate clamping members 36, 38 have been moved together in the Y axis direction and coupled to one another as mentioned in the previous paragraph. It should be appreciated that when both the elongate clamping members 36, 38 are acted on so that they may fit in the recesses 56, 58, the NET force for moving them together is substantially equal to zero.
Also illustrated in
In
In
In
In
In
Embodiments of present invention provide an advantage in that the fastener arrangement 22 is relatively easy to insert into an aperture of a plurality of articles and therefore doesn't require a large insertion force. Consequently, embodiments of the present invention are less likely to damage the outer surface of a plurality of articles during insertion. Additionally, the provision of an actuator for moving the elongate clamping members 36, 38 from the contracted configuration toward the lengthened configuration enables the fastener to engage and clamp the plurality of articles together with greater force.
The arrangement of the cam lobe 60 provides an advantage in that it moves the elongate clamping members 36, 38 from the contracted configuration towards the lengthened configuration. The cam lobe 60 is also relatively easy to remove from the fastener 24 since it does not require a large removal force (due to its low coefficient of friction and small surface tangent angles). This may result in less or no damage being done to the plurality of articles 62 during removal of the guide 26 from the fastener 24.
In this figure, a fastener 24 is inserted in an aperture 64 of a plurality of articles 62 and is clamping them together as described in the previous paragraphs. In this embodiment, the fastener arrangement 22 includes a locking mechanism 70 which is arranged to be inserted between the first and second elongate clamping members 36, 38 when the fastener 24 is inserted in the aperture 64 and thereby prevent them from being accidentally knocked from the contracted configuration to the lengthened configuration.
In more detail, the locking mechanism 70 includes a locking portion 72 which is shaped and sized to fit snugly between the first and second elongate clamping members 36, 38 when they are inserted in the aperture 64. The locking mechanism 70 also includes a neck portion 74 which is arranged to extend into the cavity 47 of the fastener 24. The neck portion 74 includes a larger part at its end which is for location in the cavity 47 and which prevents the locking mechanism 70 from being removed accidentally from the fastener 24.
It should be appreciated that the locking mechanism 70 provides an advantage in that it may improve the safety of a device which includes the fastener arrangement 22 because the locking mechanism 70 may prevent the fastener 24 from being accidentally removed from the plurality of articles 62.
In this embodiment, the fastener 24 is the same as the fastener 24 illustrated in
In this embodiment, the fastener 24 is the same as the fastener illustrated in
The embodiment illustrated in
It should be appreciated that embodiments of the present invention may be used in various different applications. Since the insertion force of the fastener arrangement into a plurality of articles and the removal force of the guide from the fastener are relatively small, embodiments of the present invention provide an advantage when used in applications where the plurality of articles are delicate. For example, embodiments of the present invention may be particularly advantageous when used in surgery on the human or animal body.
Although embodiments of the present invention have been described in the preceding paragraphs with reference to various examples, it should be appreciated that modifications to the examples given can be made without departing from the scope of the invention as claimed. For example, a fastener 24 may include more than two elongate clamping members and more than one elongate holding member.
Number | Date | Country | Kind |
---|---|---|---|
0721325.9 | Oct 2007 | GB | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/GB2008/003302 | 10/1/2008 | WO | 00 | 3/31/2010 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2009/056788 | 5/7/2009 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
684497 | Davies | Oct 1901 | A |
1900574 | Meader | Mar 1933 | A |
2006813 | Powers | Jul 1935 | A |
2386922 | Andrews et al. | Oct 1945 | A |
2438533 | Booth | Mar 1948 | A |
2585285 | Tonge et al. | Feb 1952 | A |
2758498 | Johnson | Aug 1956 | A |
2909957 | Rapata | Oct 1959 | A |
3042156 | Rohe | Jul 1962 | A |
3147525 | Texier | Sep 1964 | A |
3153975 | Rapata | Oct 1964 | A |
3476165 | Vaughn | Nov 1969 | A |
4276806 | Morel | Jul 1981 | A |
4352589 | Allison et al. | Oct 1982 | A |
4405272 | Wollar | Sep 1983 | A |
4934885 | Woods et al. | Jun 1990 | A |
4970761 | Nakamura | Nov 1990 | A |
5028187 | Sato | Jul 1991 | A |
5065490 | Wivagg et al. | Nov 1991 | A |
5135341 | Leyder | Aug 1992 | A |
5223674 | Reznikov | Jun 1993 | A |
5259689 | Arand et al. | Nov 1993 | A |
5407160 | Hollingsworth et al. | Apr 1995 | A |
5452975 | Grant | Sep 1995 | A |
5476350 | Kurtz et al. | Dec 1995 | A |
5562375 | Jackson | Oct 1996 | A |
5599512 | Latulippe et al. | Feb 1997 | A |
5601260 | Shinohara et al. | Feb 1997 | A |
5673887 | Hollingsworth et al. | Oct 1997 | A |
5678953 | Usui et al. | Oct 1997 | A |
5741102 | Everett et al. | Apr 1998 | A |
5845883 | Meyer | Dec 1998 | A |
5881982 | Hollingsworth et al. | Mar 1999 | A |
5963275 | Cho | Oct 1999 | A |
6186455 | Hollingsworth et al. | Feb 2001 | B1 |
6238230 | Sadler et al. | May 2001 | B1 |
6475030 | Chang | Nov 2002 | B1 |
6513205 | Mathieu | Feb 2003 | B1 |
6652206 | Heflin et al. | Nov 2003 | B2 |
6679712 | Chang | Jan 2004 | B2 |
6719512 | O'Banion et al. | Apr 2004 | B2 |
6722711 | Kitzis | Apr 2004 | B2 |
7014408 | O'Banion et al. | Mar 2006 | B2 |
7082650 | Awakura et al. | Aug 2006 | B2 |
7377823 | Chen | May 2008 | B2 |
7731888 | Nowicky et al. | Jun 2010 | B2 |
7736107 | Okada | Jun 2010 | B2 |
7908717 | Alhof et al. | Mar 2011 | B2 |
7993084 | Hitchcock | Aug 2011 | B2 |
8081481 | Wright et al. | Dec 2011 | B2 |
8356964 | Rottinghaus | Jan 2013 | B2 |
8517650 | Niklewicz et al. | Aug 2013 | B2 |
20030053881 | Huang et al. | Mar 2003 | A1 |
20070289107 | Alhof et al. | Dec 2007 | A1 |
20080112138 | Lin | May 2008 | A1 |
20100209241 | Bishop | Aug 2010 | A1 |
20110206476 | Brewer | Aug 2011 | A1 |
20130228538 | Engelvin et al. | Sep 2013 | A1 |
Number | Date | Country |
---|---|---|
44 16 348 | Jun 1995 | DE |
1 291 534 | Mar 2003 | EP |
WO 9908893 | Feb 1999 | WO |
WO 0247866 | Jun 2002 | WO |
Entry |
---|
Apr. 7, 2009 Written Opinion issued in PCT/GB2008/003302. |
Apr. 7, 2009 International Search Report issued in PCT/GB2008/003302. |
Number | Date | Country | |
---|---|---|---|
20100209241 A1 | Aug 2010 | US |