公开(公告)号：US20230356288A1

公开(公告)日：2023-11-09

申请号：US18246236

申请日：2021-09-22

申请人： SAFRAN AIRCRAFT ENGINES

发明人： Claire Hélène ROUSSEAU ,  Eric Joseph GOOSSENS ,  Matthieu VIAL

IPC分类号： B21J15/14 ,  B21J15/02 ,  B21J15/32

CPC分类号： B21J15/142 ,  B21J15/02 ,  B21J15/32

摘要： A mechanical part includes a part body provided with a through-opening, and a through-fastening element including a rod engaged in the through-opening and connected to an inner surface of the through-opening by a support fastened to the rod of the through-fastening element and to the inner surface of the through-opening and configured to break the link between the rod of the through-fastening element and the inner surface of the through-opening, under the effect of a thrust applied on the through-fastening element so as to push the rod of the latter into the through-opening. Due to the fact that the through-fastening element is pre-integrated with the mechanical part, the logistical management prior to assembly of the mechanical part to another mechanical part is simplified, the risk of operator errors and loss of the fastening element are reduced.

公开(公告)号：US11724305B2

公开(公告)日：2023-08-15

申请号：US16284417

申请日：2019-02-25

申请人： The Boeing Company

发明人： Harinder S. Oberoi ,  Branko Sarh ,  Melissa Ann Findlay ,  Alan S. Draper ,  Jorge Alberto Arriaga ,  Richard Griffith Reese, IV ,  Alfredo Jose Gerosa ,  Kevin Marion Barrick ,  Michael J. Kozak ,  Quang T. Do ,  Jeffrey Lawrence Miller ,  Yuanxin Charles Hu

IPC分类号： B64F5/10 ,  B25J9/16 ,  B25J11/00 ,  B21J15/28 ,  B21J15/02 ,  B21J15/10 ,  B21J15/14 ,  B60G3/14 ,  B25J5/00 ,  B29C65/70 ,  F16B19/06 ,  B23P19/10 ,  B60G7/00 ,  B21J15/32 ,  B21J15/40 ,  G05B19/418 ,  B25B5/16 ,  B29C39/12 ,  B29C39/22 ,  B64C1/06 ,  G05D1/00 ,  G05D3/12 ,  B29C45/14 ,  B29C39/02 ,  B29C39/10 ,  B64F5/50 ,  B23P21/00 ,  B29L31/00 ,  B60P3/025

CPC分类号： B21J15/28 ,  B21J15/02 ,  B21J15/10 ,  B21J15/142 ,  B21J15/32 ,  B21J15/40 ,  B23P19/10 ,  B25B5/163 ,  B25J5/007 ,  B25J9/1682 ,  B25J9/1687 ,  B25J9/1697 ,  B25J11/005 ,  B25J11/007 ,  B29C39/026 ,  B29C39/10 ,  B29C39/123 ,  B29C39/22 ,  B29C45/14336 ,  B29C65/70 ,  B60G3/145 ,  B60G7/001 ,  B60G7/008 ,  B64C1/06 ,  B64F5/10 ,  B64F5/50 ,  F16B19/06 ,  G05B19/41805 ,  G05D1/0088 ,  G05D3/12 ,  B23P21/002 ,  B23P2700/00 ,  B23P2700/01 ,  B29C2045/14368 ,  B29C2793/0081 ,  B29K2715/00 ,  B29L2031/748 ,  B60G2204/143 ,  B60G2204/418 ,  B60G2206/8207 ,  B60G2300/60 ,  B60P3/025 ,  G05B2219/45071 ,  Y02P90/80 ,  Y10S901/01 ,  Y10S901/02 ,  Y10S901/41

摘要： A method and apparatus for building a fuselage assembly for an aircraft. A number of fixtures may be drive across a floor to an assembly area to form an assembly fixture. The fuselage assembly may be built on the assembly fixture.

公开(公告)号：US11717896B2

公开(公告)日：2023-08-08

申请号：US17169986

申请日：2021-02-08

申请人： JR Automation Technologies, LLC

发明人： Joseph Robert Russell ,  Jason R. Turman ,  Ryan Nathan Anderson ,  Marcos Merino ,  Gabriel C. Van't Land

IPC分类号： B23B31/02 ,  B23B39/16 ,  B23Q17/00 ,  B23Q17/22 ,  B23B31/107 ,  B23Q3/18 ,  B23B51/10 ,  B21J15/14 ,  B23P23/04 ,  B21J15/02 ,  B21J15/30 ,  B21J15/32 ,  B23B35/00 ,  B23Q15/007 ,  B23Q16/00

CPC分类号： B23B31/028 ,  B21J15/14 ,  B23B31/1075 ,  B23B39/161 ,  B23B51/107 ,  B23P23/04 ,  B23Q3/18 ,  B23Q3/183 ,  B23Q17/006 ,  B23Q17/2216 ,  B21J15/02 ,  B21J15/30 ,  B21J15/32 ,  B23B35/00 ,  B23Q15/0075 ,  B23Q16/00

摘要： A lower drill tool that is structurally configured to receive a bracket, and, to cooperate with an upper drill tool having a pair of spaced apart drill bits. The lower drill tool has part receiving surface, a pair of spaced apart drill bores, a central bore, a centering nub and a biasing member. The drill bores extend downwardly away from the part receiving surface. The central bore is between the drill bores and extends downwardly away from the part receiving surface. The centering nub is slidable within the central bore, and has an upper tip extendable beyond the part receiving surface, positionable between an extended position and a partially retracted position. The upper tip has a conical configuration. The biasing member is positioned within the central bore and biases the centering nub toward the extended position. A drill system and a method are also disclosed.

公开(公告)号：US20190184447A1

公开(公告)日：2019-06-20

申请号：US16284417

申请日：2019-02-25

申请人： The Boeing Company

发明人： Harinder S. Oberoi ,  Branko Sarh ,  Melissa Ann Findlay ,  Alan S. Draper ,  Jorge Alberto Arriaga ,  Richard Griffith Reese, IV ,  Alfredo Jose Gerosa ,  Kevin Marion Barrick ,  Michael J. Kozak ,  Quang T. Do ,  Jeffrey Lawrence Miller ,  Yuanxin Charles Hu

IPC分类号： B21J15/28 ,  B21J15/40 ,  B29C39/02 ,  B29C39/10 ,  B60G7/00 ,  B29C39/22 ,  B29C39/12 ,  B64F5/50 ,  B25J9/16 ,  B25J11/00 ,  F16B19/06 ,  B23P19/10 ,  B21J15/32 ,  B64F5/10 ,  B25J5/00 ,  B60G3/14 ,  B21J15/14 ,  B21J15/10 ,  B21J15/02 ,  G05D3/12 ,  G05D1/00 ,  B64C1/06 ,  B25B5/16 ,  G05B19/418 ,  B29C45/14

CPC分类号： B21J15/28 ,  B21J15/02 ,  B21J15/10 ,  B21J15/142 ,  B21J15/32 ,  B21J15/40 ,  B23P19/10 ,  B23P21/002 ,  B23P2700/00 ,  B23P2700/01 ,  B25B5/163 ,  B25J5/007 ,  B25J9/1682 ,  B25J9/1687 ,  B25J9/1697 ,  B25J11/005 ,  B25J11/007 ,  B29C39/026 ,  B29C39/10 ,  B29C39/123 ,  B29C39/22 ,  B29C45/14336 ,  B29C2045/14368 ,  B29C2793/0081 ,  B29K2715/00 ,  B29L2031/748 ,  B60G3/145 ,  B60G7/001 ,  B60G7/008 ,  B60G2204/143 ,  B60G2204/418 ,  B60G2206/8207 ,  B60G2300/60 ,  B60P3/025 ,  B64C1/06 ,  B64F5/10 ,  B64F5/50 ,  F16B19/06 ,  G05B19/41805 ,  G05B2219/45071 ,  G05D1/0088 ,  G05D3/12 ,  Y02P90/86 ,  Y10S901/01 ,  Y10S901/02 ,  Y10S901/41

摘要： A method and apparatus for building a fuselage assembly for an aircraft. A number of fixtures may be drive across a floor to an assembly area to form an assembly fixture. The fuselage assembly may be built on the assembly fixture.

公开(公告)号：US10005119B2

公开(公告)日：2018-06-26

申请号：US15155461

申请日：2016-05-16

申请人： Henrob Limited

发明人： Roger Stanton Doo ,  Stuart Edmond Blacket ,  Wojciech Gostylla ,  Neal Sean Williams

IPC分类号： B21J15/02 ,  B21J15/10 ,  B21J15/28 ,  B21J15/36 ,  B23P19/02

CPC分类号： B21J15/02 ,  B21J15/025 ,  B21J15/10 ,  B21J15/28 ,  B21J15/36 ,  B23P19/02 ,  Y10T29/49943 ,  Y10T29/49947 ,  Y10T29/49956 ,  Y10T29/5148 ,  Y10T29/53 ,  Y10T29/5343 ,  Y10T29/53539 ,  Y10T29/5377 ,  Y10T29/53774

摘要： A fastening method comprising using a control apparatus to select a first upsetting volume of an upsetting die, using a punch to push a first fastener into a workpiece and using the upsetting die to upset the first fastener, then using the control apparatus to select a second upsetting volume of the upsetting die, using the punch to push a second fastener into a workpiece and using the upsetting die to upset the second fastener, or using the punch and the upsetting die to form a clinch joint.

公开(公告)号：US09909605B2

公开(公告)日：2018-03-06

申请号：US14437402

申请日：2013-10-21

申请人： BAE SYSTEMS plc

发明人： David Baker ,  Amir Rezai ,  Andrew David Wescott ,  Daniel Peter Graham

IPC分类号： F16B5/00 ,  F16B5/04 ,  B29C65/00 ,  B21J15/02 ,  B29C65/64 ,  B21K25/00 ,  B21J15/00 ,  B21J15/14 ,  F16B17/00 ,  B29C65/56 ,  B29C65/60

CPC分类号： F16B5/045 ,  B21J15/00 ,  B21J15/02 ,  B21J15/147 ,  B21K25/00 ,  B29C65/567 ,  B29C65/606 ,  B29C65/607 ,  B29C65/64 ,  B29C66/1122 ,  B29C66/21 ,  B29C66/43 ,  B29C66/721 ,  B29C66/72141 ,  B29C66/742 ,  B29C66/81419 ,  B29C66/81423 ,  B29C66/81429 ,  B29C66/81431 ,  B29C66/8322 ,  B29C66/8432 ,  F16B17/008 ,  Y10T29/49938 ,  Y10T403/4966

摘要： A method for forming a joint between a fiber reinforced composite component and a metallic component and a joint are provided. The metallic component and the composite component each define a joint surface for mating with the joint surface of the other to join the two components together and the composite component defines a free surface opposed to the joint surface thereof. The joint surface of the metallic component defines an array of pins extending therefrom with each pin defining a pin head at an end distal from the joint surface. The method includes the steps of pressing together the joint surfaces of the two components whereby to cause the array of pins to penetrate through the fiber reinforcing material, and modifying the effective cross sectional shape of the pin heads whereby to increase the constraint applied to the composite component against peeling of the composite component from the joint surface of the metallic component.

公开(公告)号：US20180036790A1

公开(公告)日：2018-02-08

申请号：US15782495

申请日：2017-10-12

申请人： PROFIL Verbindungstechnik GmbH & Co. KG

发明人： Oliver Diehl ,  Richard Humpert ,  Andreas Lembach

IPC分类号： B21J15/02 ,  F16B5/04 ,  B29C65/00 ,  B21J15/36 ,  B23P19/06 ,  B29C65/56 ,  F16B19/08 ,  B21J15/14

CPC分类号： B21J15/02 ,  B21J15/025 ,  B21J15/147 ,  B21J15/36 ,  B23P19/063 ,  B29C65/562 ,  B29C65/568 ,  B29C66/1122 ,  B29C66/21 ,  B29C66/41 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/72143 ,  B29C66/7392 ,  B29C66/7394 ,  B29C66/742 ,  B29C66/81423 ,  B29C66/81431 ,  B29C66/8322 ,  F16B5/04 ,  F16B19/086 ,  Y10T29/49943 ,  Y10T29/5377 ,  B29K2277/10 ,  B29K2307/04 ,  B29K2309/08

摘要： A punch rivet for the attachment of individual components to one another of which at least one component is formed by a workpiece of composite material, the punch rivet having a flange of larger diameter, a rivet section of smaller diameter and a ring-like component contact surface at the side of the flange adjacent to the rivet section and surrounding the rivet section, wherein the rivet section has a ring surface at its free end for the piercing of the two workpieces, with the punch rivet having a central passage which extends over the full length of the punch rivet and wherein the punch rivet has an inwardly directed projection in the region of the rivet section 14.

公开(公告)号：US09844810B2

公开(公告)日：2017-12-19

申请号：US14476369

申请日：2014-09-03

申请人： PROFIL Verbindungstechnik GmbH & Co. KG

发明人： Oliver Diehl ,  Richard Humpert ,  Andreas Lembach

IPC分类号： B21J15/02 ,  F16B5/04 ,  F16B19/08 ,  B23P19/06 ,  B21J15/14 ,  B21J15/36 ,  B29C65/56 ,  B29C65/00

CPC分类号： B21J15/02 ,  B21J15/025 ,  B21J15/147 ,  B21J15/36 ,  B23P19/063 ,  B29C65/562 ,  B29C65/568 ,  B29C66/1122 ,  B29C66/21 ,  B29C66/41 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/72143 ,  B29C66/7392 ,  B29C66/7394 ,  B29C66/742 ,  B29C66/81423 ,  B29C66/81431 ,  B29C66/8322 ,  F16B5/04 ,  F16B19/086 ,  Y10T29/49943 ,  Y10T29/5377 ,  B29K2277/10 ,  B29K2307/04 ,  B29K2309/08

摘要： A hollow punch rivet is described having a flange and a rivet section. Furthermore, a method for the attachment of individual components to one another using a punch rivet is described, with at least one of the components being formed by a material of the composite material. The method includes the following steps: a) arrangement of the die button against one of the two components to be secured to one another, which are placed on one another, wherein the die button has a bore which is dimensioned to receive the rivet section, b) carrying out a relative movement of the punch rivet with the free end of the rivet section to the fore towards the components arranged on one another and in the direction of the die button, c) piercing of the components with the free end of the rivet section and introduction of the rivet section into the bore of the die button until the component contact surface comes into contact and the component adjacent to the flange, d) using a plunger in order to dilate the punch rivet at least locally and e) forming a rivet bead by reshaping the free end region of the rivet section.

公开(公告)号：US09737969B2

公开(公告)日：2017-08-22

申请号：US15124322

申请日：2015-01-27

申请人： C. & E. Fein GmbH

发明人： Fabian Bek ,  Markus Knecht ,  Thomas Weber ,  Rainer Mann

IPC分类号： B23D23/04 ,  B24B23/04 ,  B21K25/00 ,  B21J15/02 ,  B23D61/02 ,  F16B5/04 ,  B23D61/00

CPC分类号： B24B23/04 ,  B21J15/02 ,  B21K25/00 ,  B23D61/006 ,  B23D61/026 ,  F16B5/045

摘要： An electric power tool is disclosed. In an embodiment, the electric power tool includes a tool, a tool holder part and a main body with a plurality of rivets integrated with the main body. The rivets include rivet shafts of a cross section for producing a positive-locking rivet joint of the tool with the tool holder part, wherein the tool and the tool holder part have circular openings which are aligned with each other, and wherein the rivet shafts are positioned aligned with the openings on the main body and protrude through the aligned openings.

公开(公告)号：US09682419B2

公开(公告)日：2017-06-20

申请号：US13810574

申请日：2011-08-24

申请人： Heiko Schmidt

发明人： Heiko Schmidt

IPC分类号： B21D9/05 ,  B21J15/02 ,  B23P11/00 ,  B21J15/28 ,  B25B27/00 ,  B21J15/10 ,  B21J15/04

CPC分类号： B21J15/02 ,  B21J15/04 ,  B21J15/043 ,  B21J15/10 ,  B21J15/28 ,  B21J15/285 ,  B25B27/0014 ,  Y10T29/49956 ,  Y10T29/5377

摘要： A method for setting blind rivet elements in which the setting of the respective blind rivet element introduced into a pre-hole of the work piece and/or the formation of a rivet collar takes place in a setting stroke (SH) through the permanent deformation of a section of the blind rivet element by subjecting an end of the blind rivet element to a traction force by a traction element of a setting tool while simultaneously supporting another end of the blind rivet element on a support part of the setting tool counter to the traction force.