EP1907711A1 - Toleranzausgleichsverbinder - Google Patents
ToleranzausgleichsverbinderInfo
- Publication number
- EP1907711A1 EP1907711A1 EP06773868A EP06773868A EP1907711A1 EP 1907711 A1 EP1907711 A1 EP 1907711A1 EP 06773868 A EP06773868 A EP 06773868A EP 06773868 A EP06773868 A EP 06773868A EP 1907711 A1 EP1907711 A1 EP 1907711A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- fastener
- torque
- sleeve
- tolerance compensating
- coil
- 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- Withdrawn
Links
- 239000007769 metal material Substances 0.000 claims description 4
- 230000001419 dependent effect Effects 0.000 claims description 2
- 238000003754 machining Methods 0.000 description 6
- 238000003780 insertion Methods 0.000 description 5
- 230000037431 insertion Effects 0.000 description 5
- 238000005266 casting Methods 0.000 description 4
- 230000004323 axial length Effects 0.000 description 3
- 229910000639 Spring steel Inorganic materials 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000003071 parasitic effect Effects 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 230000036316 preload Effects 0.000 description 1
- 239000012858 resilient material Substances 0.000 description 1
- 238000010079 rubber tapping Methods 0.000 description 1
- 239000000565 sealant Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000004575 stone Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
- F16B5/0216—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread the position of the plates to be connected being adjustable
- F16B5/0233—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread the position of the plates to be connected being adjustable allowing for adjustment perpendicular to the plane of the plates
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
Definitions
- the invention relates to a tolerance compensating connector, and more particularly to a tolerance compensating connector having a member for transmitting a torque from a fastener to a compensating sleeve which torque depends upon the direction of rotation of a fastener.
- Tolerances may be very small, fractions of a millimeter, or very large, several millimeters, depending upon the circumstances. Larger tolerances generally reduce manufacturing costs and make assembly more easy.
- shims or screw type devices that fill the gap between the mating surfaces of the components to be joined.
- the shims or screw type devices are generally a separate component from the fasteners .
- US publication number 2003/0077142 Al to Stone discloses a tolerance compensating mounting device comprising a bushing having an internal and external thread.
- the bushing is threaded into a part to be mounted to a surface.
- a bolt is then threaded into a bushing bore using the internal threads.
- the internal threads cause an interference fit between the bolt shank and the threads, temporarily preventing further insertion of the bolt.
- the bolt is then turned, thereby turning the bushing and causing the bushing to unscrew from the part toward the mounting surface until the bushing bears upon the mounting surface, thereby completely compensating for a tolerance gap.
- the sacrificial internal threads are stripped to allow the bolt to be fully torqued into the mounting surface hole, thereby simultaneously connecting the components while compensating for a tolerance gap.
- the primary aspect of the invention is to provide a reusable tolerance compensating connector having a member for transmitting a torque from a fastener to a compensating sleeve which torque depends upon the direction of rotation of the fastener.
- the invention comprises a tolerance compensating connector comprising a first member having a threaded portion, a second member comprising a bore and an outer surface, the outer surface having a helical thread engagable with a receiver, the first member engaged with the bore, a third member engaged with the first member and the second member, the third member transmitting a torque from the first member to the second member such that a first torque transmitted to the second member as the first member is turned in a first direction is sufficient to turn the second member in the receiver, the third member having a slipping engagement with the first member when the first torque is exceeded, and upon the first member being turned in a direction opposite the first direction the third member transmits a second torque to the second member sufficient to turn the second member in the receiver in a direction opposite the first direction.
- Figure 1 is a side cross-sectional view of tolerance compensating connector.
- Figure 2 is a cross-sectional view of the sleeve.
- Figure 3 is a perspective view of the sleeve.
- Figure 4 is a cross-sectional side view of the coil member in Fig. 5.
- Figure 5 is a plan view of the coil member.
- Figure 6 is a cross-sectional view of an alternate coil member in Figure 7.
- Figure 7 is a plan view of an alternate coil member.
- Figure 8 is a cross-sectional view of an alternate sleeve .
- Figure 9 is a perspective view of an alternate sleeve .
- FIG. 1 is a side cross-sectional view of tolerance compensating connector.
- Connector 100 comprises a first member, namely, a fastener 10.
- Fastener 10 comprises a threaded portion 12, head 13 and flange 14.
- the embodiment shown in Figure 1 shows threaded portion 12 extending along the entire length of fastener 10.
- Fastener 10 may comprise an SAE or metric thread on portion 12. Threaded portion 12 may comprise either left or right handed threads. Threaded portion 12 may comprise either coarse or fine threads of any known style and type. Fastener 10 may have a hex head, Torx head or any other suitable driver head known in the art . Thread portion 12 has a diameter D2. Second member or sleeve 20 comprises an outer threaded portion 21 and a bore 22. Outer threaded portion 21 comprises a helical thread for engaging a receiver portion 40. Outer threaded portion 21 may comprise an SAE or metric threads. Outer threaded portion 21 may comprise either left or right hand threads. Outer threaded portion 21 may comprise either coarse or fine threads of any known style.
- Receiver portion 40 may comprise any component to be mounted to another component 50, for example, a water pump mounted to an engine block 50.
- Engine block 50 comprises a threaded receiver portion 51, namely a threaded hole.
- Receiver portion 51 comprises threads 52 which cooperatively engage threaded portion 12 of fastener 10.
- Surface 24 bears upon a surface of the portion to which component 40 is attached, in this case, an engine block 50.
- Third member 30 is engaged between the first member and the second member.
- Third member comprises a coil or coils 32 of wire or other resilient material that wraps about and thereby grips or clasps fastener 10.
- An end 31 of third member 30 is engaged with the second member 20 such that the third member cannot rotate with respect to the second member, but the third member may rotate with respect to the first member 10 in a predetermined direction Rl.
- first member 10 is inserted into the bore 22 of second member 20 while being simultaneously turned into third member 30.
- the assembly of the first member, second member and third member comprises the inventive tolerance compensating connector.
- Connector 100 is then threaded into the receiver portion 40 by engagement between threaded portion 21 and threaded portion 41.
- Sleeve 20 is turned by applying a torque to fastener 10 until fastener 10 comes into contact with receiver portion 51, or until surface 24 comes into contact with component 50. In most cases surface 24 will contact component 50 before fastener 10 contact receiver portion 51. Once surface 24 is in contact with component 50 and fastener 10 is engaged with portion 51, fastener 10 is then fully threaded into receiver portion 51 until flange 14 engages surface 42 and torqued to a final value.
- Third member 30 transmits a first torque from the fastener 10 to sleeve 20.
- the coil direction of third member 30 is such that it does not tightly grip fastener 10 as fastener 10 is threaded into receiving portion 51 and as sleeve 20 is turned into threaded portion 41. However, the grip is sufficient to cause sleeve 20 to turn in threaded portion 41.
- Third member 30 then slips on fastener 10 once the first torque is exceeded, that is, when sleeve 20 stops turning after surface 24 comes into contact with component 50. Once sleeve 20 stops turning fastener 10 is then fully screwed into the receiving portion 51 due in part to the slipping engagement between third member 30 and fastener 10.
- the engagement between third member 30 and fastener 10 must be sufficient to not only ensure contact between surface 24 and component 50, but sufficient so that sleeve 24 is torqued enough to ensure proper engagement of surface 24, namely, by overcoming parasitic friction between the surfaces so that substantially all of surface 24 is in contact with component 50. This ensures the load bearing capacity of sleeve 20 is fully developed thereby ensuring proper rigidity of the assembled components.
- Sleeve 20 spans a gap "T" between components being connected.
- the size of gap T which can be spanned is only limited by the length of sleeve 20.
- Sleeve 20 only need have sufficient threads engaged with portion 40 to fully develop the theoretical shear strength required by the application.
- fastener 10 is fully torqued, sleeve 20 is held in place by a compressive load.
- the number of threads 21 which must be engaged with receiver portion 41 is a function of maximum preload in the fastener and thereby the shear load imposed upon the threads 21.
- the fastener 10 is turned in the direction opposite that used to engage it.
- the coil direction of third member 30 causes third member 30 to tightly grip fastener 10.
- Third member 30 grips the fastener tightly enough so that a sufficient second torque is transmitted from the fastener to the sleeve by the third member to cause sleeve 20 to be withdrawn from engagement with component 50 and from receiver portion 41.
- the third member does not slip on the fastener when the second torque is being transmitted to the sleeve.
- the torque applied to the sleeve by the third member is dependent upon the direction of rotation of the fastener.
- the insertion, or first, torque is generally less than the second or withdrawal torque, but this is not always the case. In some instances sleeve 20 will be locked in place once sleeve 20 is installed.
- Connector 100 can be fully withdrawn fully intact from the components which it is used to attach together. Since the manner of operation of the connector is not sacrificial or damaging to any of its parts, the connector may be reused.
- Figure 2 is a cross-sectional view of the sleeve.
- Sleeve 20 comprises outer threaded portion 21.
- Portion 21 may be threaded along its entire axial length as shown, or along a portion comprising less than its entire axial length.
- Bore 22 receives fastener 10.
- Receiving portion 23 may comprise a hole or other means for engaging end 31 of third member 30, see Fig. 5.
- Portion 21 has the same thread hand as the threaded portion 12 of fastener 10. This is to cause sleeve 20 to move in the same engagement direction as the fastener during engagement and disengagement .
- FIG. 3 is a perspective view of the sleeve. Hole 23 is shown disposed at an end of sleeve 20 in a location that keeps end 31 from contacting threaded portion 41 during engagement. Hole 23 may be disposed at any location on sleeve 20 so long as end 31 does not interfere with threaded portion 41.
- Figure 4 is a cross-sectional side view of the coil member in Fig. 5.
- End 31 extends radially and engages hole 23 in sleeve 20.
- Coils 32 wrap about fastener 10 in a predetermined direction. The direction of wrap determines whether third member 30 will lightly or tightly grip fastener 10 for a given rotational direction.
- An inside diameter D3 see Fig. 5, is selected to cause the coils to grip threaded portion 12 of fastener 10.
- the coil comprises spring steel or its equivalent so that the coil exerts a spring force in response to the fastener "opening" the coils to a somewhat greater diameter than D3. In this way the coils "grip" fastener 10 in a manner similar to the operation of a band brake .
- Third member 30 further comprises a larger coil 320 having an inside diameter D5.
- D5 is greater than diameter D3 giving member 30 a somewhat tapered appearance.
- Diameter D5 facilitates engagement of the third member 30 with sleeve recess 220 as well as with 23.
- the coils grip the fastener lightly when the fastener is turned in a first direction, for example during insertion of the fastener.
- the coils grip the fastener tightly when turned in the opposite direction, for example during withdrawal of the fastener.
- the coils need to also grip the fastener tightly enough to cause sleeve 20 to be threaded into threaded portion 41 as fastener 10 is turned.
- Figure 5 is a plan view of the coil member.
- Coils 32 have a diameter D3 and a thickness D6.
- Coil 320 has a diameter D5 as shown in Figure 4.
- End 33 may be angled somewhat inward toward the fastener to allow edge 34 of end 33 to better engage the fastener. This enhances the capacity of the third member coils to grip the fastener. In other applications end 33 need not be angled.
- Third member may comprise any material capable of gripping fastener sufficient to generate the torques as described herein.
- third member 30 may comprise a metallic material such as spring steel, steel, or aluminum. It may also comprise non-metallic materials such as plastic, ceramic or polyurethane, as well as combinations or equivalents of either the metallic or non-metallic materials.
- Figure 6 is a cross-sectional view of an alternate coil member in Figure 7.
- Alternate third member 30 comprises coils 32 as described in Figure 4. However, in this alternate embodiment end 31 is omitted. Retention of third member 30 in sleeve 20 is accomplished by a frictional fit of coil 320 in recess 220, please see Figure 8. Namely, coil 320 has an outside diameter D7 that is slightly larger than the inside diameter D4 , see Figure 2, of sleeve 20.
- a frictional fit is achieved between third member 30 and sleeve 20 by the snug fit between coil 320 and recess 220.
- the frictional fit between fastener 10 and coil 320, and of coil 320 with sleeve 20 causes sleeve 20 to rotate in receiver portion 40.
- Sleeve 20 rotates until surface 24 engages component 50 as described elsewhere in this specification.
- the turn direction of coil 30 is preferably the same hand as the insertion rotation direction of fastener 10.
- Figure 7 is a plan view of an alternate coil member. End 31 is omitted from member 30, but it is otherwise as described in Figure 5.
- FIG 8 is a cross-sectional view of an alternate sleeve.
- Recess 220 comprises a diameter D4 as shown in Figure 2.
- sleeve 20 does not include receiving portion 23.
- Figure 9 is a perspective view of an alternate sleeve. Threads 21 are shown extending along the entire axial length of sleeve 20. Receiving portion 23 is omitted from this embodiment .
- the installation torque that is, the torque required to install sleeve 20 into receiver portion 41 is less than the torque required to " back the fastener 10 out of sleeve 20.
- the installation sleeve 20 will screw into receiver portion 41 until it "bottoms" on surface 24.
- Fastener 10 will then continue to turn within third member 30 as described. Extraction of fastener 10 from receiver portion 51 will cause third member 30 to grip fastener 10 thereby- causing sleeve 20 to be extracted from receiver portion 41.
- the inventive connector may also be used to speed machine assembly and reduce machining costs. Namely, when two machined castings or fabrications are bolted together the surfaces to be joined are usually machined flat to assure a proper fit-up. A seal or sealant is used between the two surfaces. This requires a surface finish and flatness that can only achieved by machining. This requires time and specialized equipment. The machining of castings usually results in some distortion taking place when stresses on the outer ⁇ skin' of the casting are removed. On larger castings sometimes a second pass is required to take out the distortion produced by the first machining pass. Where no seal is required, or, where the required sealing could be achieved in another way, then there is the possibility of eliminating the machining of the surfaces to be joined with associated cost savings.
- inventive connectors Instead of machining flat spaces, spot-faced bosses for tapping's and dowels are used on the component surfaces to control lateral movement and for proper fitment and alignment. Variations in spacing or gap between the surfaces is accommodated by use of the inventive connectors. Further, use of the inventive connector allows the parts to be later disassembled, for example for maintenance purposes, because the connector is reusable.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Details Of Connecting Devices For Male And Female Coupling (AREA)
- Connection Of Plates (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US17888205A | 2005-07-11 | 2005-07-11 | |
PCT/US2006/024533 WO2007008372A1 (en) | 2005-07-11 | 2006-06-23 | Tolerance compensating connector |
Publications (1)
Publication Number | Publication Date |
---|---|
EP1907711A1 true EP1907711A1 (de) | 2008-04-09 |
Family
ID=37057216
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP06773868A Withdrawn EP1907711A1 (de) | 2005-07-11 | 2006-06-23 | Toleranzausgleichsverbinder |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP1907711A1 (de) |
JP (1) | JP4926170B2 (de) |
KR (1) | KR20080025754A (de) |
CN (1) | CN101243260A (de) |
BR (1) | BRPI0612715A2 (de) |
TW (1) | TWI299381B (de) |
WO (1) | WO2007008372A1 (de) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BRPI1105325B1 (pt) * | 2011-12-22 | 2021-07-20 | Embraer S.A. | Acoplamento auto-alinhável para superfícies sobrepostas e método de acoplamento auto-alinhável para superfícies sobrepostas |
US20090047094A1 (en) * | 2007-08-14 | 2009-02-19 | Roger Derrick Stone | Tolerance compensating fastener |
CA2598137C (en) * | 2007-08-20 | 2015-04-28 | Intier Automotive Inc. | System and method for staking an assembly of components with compensation for component tolerances |
CN102166942A (zh) * | 2011-04-12 | 2011-08-31 | 重庆长安汽车股份有限公司 | 一种发动机u型支架的安装结构 |
KR101437623B1 (ko) * | 2012-07-19 | 2014-09-05 | 한국기계연구원 | 틈새 보정용 볼트 어셈블리 |
US9726211B2 (en) | 2013-03-15 | 2017-08-08 | Schlumberger Technology Corporation | 5 degrees of freedom alignment-correcting preloaded bearing connection system |
US9689511B1 (en) * | 2016-06-16 | 2017-06-27 | The Monadnock Company | Tie wrap plastic anchor assemblies and methods of assembly |
DE102017124470A1 (de) * | 2017-10-19 | 2019-04-25 | Böllhoff Verbindungstechnik GmbH | Toleranzausgleichsanordnung |
DE102017124809A1 (de) * | 2017-10-24 | 2019-04-25 | Böllhoff Verbindungstechnik GmbH | Toleranzausgleichsanordnung |
DE102017130605A1 (de) | 2017-12-19 | 2019-06-19 | Böllhoff Verbindungstechnik GmbH | Toleranzausgleichsanordnung mit Klemmsicherung |
CN109964674A (zh) * | 2017-12-28 | 2019-07-05 | 天津市天龙得冷成型部件有限公司 | 防水园林剪刀用剪刀轴 |
DE102019108910A1 (de) * | 2019-04-04 | 2020-10-08 | Böllhoff Verbindungstechnik GmbH | Mehrteiliges Verstellelement für eine Toleranzausgleichsanordnung |
PL4095395T3 (pl) * | 2021-05-27 | 2023-12-18 | Böllhoff Verbindungstechnik GmbH | Element nastawczy, pierwszy komponent z elementem nastawczym, konstrukcja łącząca zawierająca pierwszy komponent, sposób wytwarzania elementu nastawczego i sposób połączenia |
KR102385282B1 (ko) * | 2021-06-22 | 2022-04-08 | 강재성 | 공차 보정 시스템 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3436166A1 (de) * | 1984-10-03 | 1986-04-10 | Ewald Witte & Co, 5620 Velbert | Schraubverbindung |
WO2002010597A1 (en) * | 2000-07-28 | 2002-02-07 | Ozawa, Junzo | Fastening implement |
JP2002122114A (ja) * | 2000-08-10 | 2002-04-26 | Aoyama Seisakusho Co Ltd | ボルトおよびこのボルトを用いた部材の締結方法および締結解除方法 |
DE20016100U1 (de) * | 2000-09-16 | 2002-01-31 | Schwarzbich Joerg | Mehrteilige Distanzscheibe |
DE20016150U1 (de) * | 2000-09-18 | 2002-01-24 | Schwarzbich Joerg | Vorrichtung zum Verbinden von Bauteilen |
DE10052448A1 (de) * | 2000-10-23 | 2002-05-02 | Hilti Ag | Befestigungselement |
DE20021194U1 (de) * | 2000-12-14 | 2002-04-18 | Schwarzbich Joerg | Vorrichtung zum Verbinden von Bauteilen |
ATE364795T1 (de) * | 2000-12-20 | 2007-07-15 | Acument Gmbh & Co Ohg | Toleranzausgleichselement |
US6884014B2 (en) * | 2001-04-23 | 2005-04-26 | The Gates Corporation | Tolerance compensating mounting device |
US20020154966A1 (en) * | 2001-04-23 | 2002-10-24 | Roger Stone | Tolerance compensating mounting device |
JP4028968B2 (ja) * | 2001-05-23 | 2008-01-09 | 本田技研工業株式会社 | 車両のプレート取付構造。 |
-
2006
- 2006-06-23 CN CNA2006800304369A patent/CN101243260A/zh active Pending
- 2006-06-23 KR KR1020087002800A patent/KR20080025754A/ko not_active Application Discontinuation
- 2006-06-23 BR BRPI0612715-0A patent/BRPI0612715A2/pt not_active Application Discontinuation
- 2006-06-23 JP JP2008521406A patent/JP4926170B2/ja not_active Expired - Fee Related
- 2006-06-23 WO PCT/US2006/024533 patent/WO2007008372A1/en active Application Filing
- 2006-06-23 EP EP06773868A patent/EP1907711A1/de not_active Withdrawn
- 2006-07-06 TW TW095124623A patent/TWI299381B/zh not_active IP Right Cessation
Non-Patent Citations (1)
Title |
---|
See references of WO2007008372A1 * |
Also Published As
Publication number | Publication date |
---|---|
KR20080025754A (ko) | 2008-03-21 |
CN101243260A (zh) | 2008-08-13 |
JP4926170B2 (ja) | 2012-05-09 |
JP2009500583A (ja) | 2009-01-08 |
BRPI0612715A2 (pt) | 2010-11-30 |
TWI299381B (en) | 2008-08-01 |
WO2007008372A1 (en) | 2007-01-18 |
TW200714811A (en) | 2007-04-16 |
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