CN109514300A - Cornual plate positions pilot hole binding clasp - Google Patents

Cornual plate positions pilot hole binding clasp Download PDF

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Publication number
CN109514300A
CN109514300A CN201811497803.7A CN201811497803A CN109514300A CN 109514300 A CN109514300 A CN 109514300A CN 201811497803 A CN201811497803 A CN 201811497803A CN 109514300 A CN109514300 A CN 109514300A
Authority
CN
China
Prior art keywords
pilot hole
activity
cornual plate
clamping
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.)
Granted
Application number
CN201811497803.7A
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Chinese (zh)
Other versions
CN109514300B (en
Inventor
符文科
熊千
杰小平
周松松
杜立斌
林松
龙昌鹏
毛晓东
孙梦龙
王亮
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.)
Jiangxi Hongdu Aviation Industry Group Co Ltd
Original Assignee
Jiangxi Hongdu Aviation Industry Group Co Ltd
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 Jiangxi Hongdu Aviation Industry Group Co Ltd filed Critical Jiangxi Hongdu Aviation Industry Group Co Ltd
Priority to CN201811497803.7A priority Critical patent/CN109514300B/en
Publication of CN109514300A publication Critical patent/CN109514300A/en
Application granted granted Critical
Publication of CN109514300B publication Critical patent/CN109514300B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23QDETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
    • B23Q3/00Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
    • B23Q3/02Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine for mounting on a work-table, tool-slide, or analogous part
    • B23Q3/06Work-clamping means
    • B23Q3/061Work-clamping means adapted for holding a plurality of workpieces

Abstract

Invention be related to a kind of cornual plate clamp, positioning and pilot hole installation tool, belong to assembled aircraft structure field.Cornual plate positions pilot hole binding clasp, including support portion, clamping feeding portion, activity pilot hole support portion and activity pilot hole portion;Cornual plate positioning head and clamping head are provided on support portion, clamping head clamps feeding portion for clamping;It clamps feeding portion to be slidably connected with clamping head, head end is opposite with cornual plate positioning head position, for positioning cornual plate;Activity pilot hole portion includes activity pilot hole portion I, activity pilot hole portion II, I one end of activity pilot hole portion is connect with activity pilot hole support portion, the other end and cornual plate positioning head are rotatablely connected, and II one end of activity pilot hole portion is slidably connected with activity pilot hole support portion, the other end and clamping feeding size end rotation connection.It the present invention and has the advantages that 1, realize the accurate aperture and positioning to cornual plate.2, tool making is simple, easy to operate, and operating effect is good.

Description

Cornual plate positions pilot hole binding clasp
Technical field
The present invention relates to a kind of clamping of cornual plate, positioning and pilot hole installation tools, belong to assembled aircraft structure field.
Background technique
Aircraft fills assembling stage in portion, often there is a large amount of cornual plates clampings, positioning and pilot hole, however most cornual plate is pacified Dress is often in small space or the more complicated region of structure of aircraft component.It is existing to be limited and tied by space for these The cornual plate positioning in the more complex region of structure is clamped and is riveted and generally installed using multiple auxiliary tools, first with traditional Scribing line positioning method carries out aperture to cornual plate and the component connected;Secondly it is limited by component space, cornual plate can only be held to it It is positioned and is riveted.Finally check riveting quality and product surface quality.Cornual plate installation is carried out in the above manner often to deposit In following main problem:
1, cornual plate installation is done over again, and phenomenon is frequent, and product installation quality is lower, is specifically mainly manifested in the following aspects:
(1) it in cornual plate Tapping procedures, can only with the naked eye be determined, cause that the degree of deviation angle of aperture is big, back gauge is inadequate, cornual plate is fixed Position is uncoordinated, clamps relaxation, causes cornual plate installation inclination.
(2) in cornual plate riveting process, limited by space, riveting quality is unqualified and easy scuffing around product surface.
2, labor intensity of workers is high, needs by multiple auxiliary tools.Lack specification, dedicated tool.
3, component installation effectiveness is restricted, and then influences the aircraft whole delivery time.
Summary of the invention
Present invention aim to address problems of the prior art, provide that a kind of accurate positioning, structure is simple and grasps Make convenient cornual plate positioning pilot hole binding clasp.
To achieve the goals above, the present invention adopts the following technical scheme: cornual plate positions pilot hole binding clasp, including support Portion clamps feeding portion, activity pilot hole support portion and activity pilot hole portion;Cornual plate positioning head and clamping head are provided on support portion, Clamping head clamps feeding portion for clamping;It clamps feeding portion to be slidably connected with clamping head, head end and cornual plate positioning head position phase It is right, for positioning cornual plate;Activity pilot hole portion includes activity pilot hole portion I, activity pilot hole portion II, I one end of activity pilot hole portion and activity The connection of pilot hole support portion, the other end and cornual plate positioning head are rotatablely connected, and II one end of activity pilot hole portion and activity pilot hole support portion are sliding Dynamic connection, the other end and clamping feeding size end rotation connection, the corresponding position phase in activity pilot hole portion I, activity pilot hole portion II To being provided with pilot hole connector.
Preferably, the support portion further includes support rod, and support rod is connected and fixed cornual plate positioning head and clamping head, is being clamped The axial direction of head, which is provided with to hold, clamps the through-hole that feeding portion passes through.
Preferably, the clamping feeding portion includes clamping feed bar, hand-held feeding swingle;It wears the end for clamping feed bar Cross clamping head, and can under the action of hand-held feeding swingle sliding axially along clamping head.
Preferably, the hand-held feeding swingle is across the rod-like element for clamping feed bar radial direction.
Preferably, it is provided with external screw thread on clamping the body of rod between feed bar and hand-held feeding swingle, and be set to The internal screw thread of clamping head matches.
Preferably, the polyhedron of the cornual plate positioning head and the head end in clamping feeding portion by axis on same straight line It is formed with rotary table, and the upper bottom surface of rotary table is opposite.
Preferably, ears piece is provided on certain polyhedral one side, activity pilot hole portion I, activity pilot hole portion II divide It is not rotatablely connected with ears piece.
Preferably, the activity pilot hole support portion includes spring, spring loop bar and pilot hole boom, and spring is placed in spring loop bar Interior, pilot hole boom is placed in the both ends of spring, and for limiting the movement of spring, free end is pierced by spring loop bar and draws respectively with activity Hole portion I, activity pilot hole portion II connect, and the sliding axially along spring loop bar under the action of activity pilot hole portion II.
Preferably, activity pilot hole portion I includes crank, pilot hole handle and pilot hole connector, and one end of crank and cornual plate position Head rotation connection, the other end and pilot hole handle are rotatablely connected, and pilot hole connector and the other end of pilot hole handle are connected and fixed;Activity pilot hole portion II includes crank, pilot hole handle, pilot hole major joint and pilot hole bar, and one end of crank and cornual plate positioning head are rotatablely connected, the other end with The rotation connection of pilot hole handle, pilot hole major joint and the other end of pilot hole handle are slidably connected, and are gap-matched with pilot hole bar, and Sliding of the pilot hole major joint in pilot hole handle is realized under the action of pilot hole bar.
Preferably, activity pilot hole portion II further includes spring, and spring pocket is limited at pilot hole handle and draws on pilot hole bar Between the tail portion of vent stem.
Compared with the prior art, the invention has the following advantages:
1, the accurate aperture and positioning to cornual plate are realized, cornual plate peripheral member product surface quality will not be interfered and influence.
2, tool making is simple, easy to operate, and operating effect is good, can substantially reduce labor intensity of workers, improves product dress With efficiency, and then shorten product delivery cycle.
Detailed description of the invention
Fig. 1 is 1 axonometric drawing of the embodiment of the present invention;
Fig. 2 is front view of the embodiment of the present invention;
Fig. 3 is the bottom view of Fig. 2;
Fig. 4 is clamping feeding portion structural schematic diagram in Fig. 1;
Fig. 5 is activity pilot hole tube-in-tube structure schematic diagram in Fig. 1;
Fig. 6 is activity pilot hole handle and pilot hole pin shaft mapping a;
Fig. 7 is activity pilot hole handle and pilot hole pin shaft mapping b;
Fig. 8 is supporting part structure schematic diagram in Fig. 1;
In figure, 1, clamping feeding portion;2, activity pilot hole sleeve;3, activity pilot hole handle and pilot hole pin;4, support member;1-1, clamping Feed bar;1-2, hand-held feeding swingle;1-3, external screw thread region;2-1, spring;2-2, spring loop bar;2-3, pilot hole boom; 2-4, pilot hole boom;3-1, crank;3-2, crank;3-3, crank;3-4, crank;3-5, pilot hole connector;3-6, pilot hole are main to be connect Head;3-7, spring;3-8, pilot hole bar;4-1, support rod;4-2, support rod;4-3, head is fixed to clamp;4-4, portion of the handle.
Specific embodiment
1-8 is further described the present invention with reference to the accompanying drawing: as shown in Figure 1-3, cornual plate position pilot hole binding clasp by It clamps feed bar 1, activity pilot hole sleeve 2, activity pilot hole handle and pilot hole pin 3 and support member 4 is constituted.
As shown in figure 4, clamping feeding portion 1 by clamping feed bar 1-1, hand-held feeding swingle 1-2 and external screw thread region 1-3 It constitutes.The head end for clamping feed bar 1-1 is made of coaxial regular octahedron and rotary table, the bottom surface of rotary table and the bottom of regular octahedron Face partially overlaps;It is provided with ears piece on one of side of regular octahedron, corresponding through-hole is set in ears on piece, is led to The axis in hole is consistent with the axis direction of feed bar 1-1 is clamped;Hand-held feeding swingle 1-2 is close to the tail for clamping feed bar 1-1 Portion, for across the rod-like element for clamping feed bar 1-1 radial through-hole;External screw thread region 1-3, which is set to, to be clamped feed bar 1-1, holds It feeds on the body of rod between swingle 1-2.
As shown in figure 5, activity pilot hole sleeve 2 is by spring 2-1, spring loop bar 2-2, pilot hole boom 2-3 and pilot hole boom 2-4 It constitutes.Spring 2-1 is placed in spring loop bar 2-2;Pilot hole boom 2-3, pilot hole boom 2-4 are placed in the both ends of spring, for limiting The movement of spring, one end are matched with the internal diameter of spring loop bar 2-2, and the other end is pierced by spring loop bar, i.e. pilot hole boom 2-3, draw The axis of hole boom 2-4 is vertical with the axis of spring loop bar 2-2;It is sliding that appearance pilot hole boom 2-4 is opened up along the axial direction of spring loop bar 2-2 Dynamic sliding slot.
As shown in Fig. 3,6-7, activity pilot hole handle and pilot hole pin 3 are by crank 3-1, crank 3-2, pilot hole handle 3-3, pilot hole handle 3- 4, pilot hole connector 3-5, pilot hole major joint 3-6, spring 3-7 and pilot hole bar 3-8 are constituted.Crank 3-2, pilot hole handle 3-3 and pilot hole connect Head 3-5 constitutes the motionless activity pilot hole handle in one of position and pilot hole pin 3;Crank 3-1, pilot hole handle 3-4, pilot hole major joint 3-6, Spring 3-7 and pilot hole bar 3-8 constitutes another position-movable activity pilot hole handle and pilot hole pin 3, pilot hole handle 3-3,3-4 difference It is connected with crank 3-2,3-1 using movable bolt, pilot hole connector 3-5 and crank 3-3 are connected, and pilot hole bar 3-8 and pilot hole handle 3-4 are adopted With clearance fit, pilot hole major joint 3-6 is connected and fixed on the end of pilot hole bar 3-8, and spring 3-7 is covered on pilot hole bar 3-8, limited It is scheduled between pilot hole handle 3-4 and the tail portion of pilot hole bar 3-8.
As shown in figure 8, support member 4 by support rod 4-1, support rod 4-2, fix to clamp a 4-3 and portion of the handle 4-4 (internal screw thread).Support rod 4-1, support rod 4-2 are fixed together by rod-like element, and the axis of rod-like element and support rod 4-1, support The axis of bar 4-2 is vertical, fixes to clamp a 4-3 and portion of the handle 4-4(internal screw thread) it is separately connected and is fixed on support rod 4-2 and branch The end of strut 4-1;It fixes to clamp a 4-3 to be made of coaxial regular octahedron and rotary table, the bottom surface and regular octahedron of rotary table Bottom surface portions be overlapped;It is provided with ears piece on one of side of regular octahedron, it is corresponding logical in the setting of ears on piece Hole, the axis of through-hole and the axis direction of rod-like element are consistent;Portion of the handle 4-4 is hollow regular octahedron, in internal setting Screw thread.
As shown in Figure 1-3, clamp feed bar 1-1 pass through portion of the handle 4-4 through-hole so that its head end with auricle with Fix to clamp that a 4-3 is opposite, one end of crank 3-2 is connect with the auricle fixed to clamp on a 4-3 using movable bolt, pilot hole handle 3-4 is threadedly coupled with pilot hole boom 2-3, and one end of crank 3-1 is tethered with the auricle clamped on feed bar 1-1 using movable screw It connects, pilot hole handle 3-4 is threadedly coupled with pilot hole boom 2-4;Clamp feed bar 1-1 external screw thread region 1-3 and support member hand-held part Divide 4-4(internal screw thread) cooperate for giving clamping force.
As shown in Fig. 1,2,3,4,6,7, cornual plate position pilot hole binding clasp by it is axial promote hand-held feeding swingle 1-2 and Workpiece fitting, the hand-held feeding swingle 1-2 of radial rotary keep cornual plate positioning pilot hole binding clasp and workpiece in clamped condition, according to Workpiece structure feature adjustment activity pilot hole handle angle, θ1、θ2, pilot hole connector 3-5 and pilot hole major joint 3-6 is made to be resisted against workpiece two sides Relative position, pressing pilot hole bar 3-8 complete workpiece pilot hole effect.
During the work time according to design feature flexibly changing activity pilot hole handle angle, θ1、θ2To adapt to complex part behaviour Make.
Spring 2-1 and spring 3-7 is respectively used to clamping feed bar 1-1, the automatic of pilot hole bar 3-8 after pilot hole and answers Position.
Above-described embodiment is only preferred embodiments of the invention, is not construed as limiting the invention.This is not being departed from On the basis of the technical solution of invention, any amplification that those of ordinary skill in the art are done, deformation are in protection of the invention In range.

Claims (10)

1. cornual plate positions pilot hole binding clasp, it is characterised in that: including support portion, clamp feeding portion, activity pilot hole support portion and work Dynamic pilot hole portion;Cornual plate positioning head and clamping head are provided on support portion, clamping head clamps feeding portion for clamping;Clamp feeding Portion is slidably connected with clamping head, and head end is opposite with cornual plate positioning head position, for positioning cornual plate;Activity pilot hole portion includes activity Pilot hole portion I, activity pilot hole portion II, I one end of activity pilot hole portion are connect with activity pilot hole support portion, and the other end and cornual plate positioning head turn Dynamic connection, II one end of activity pilot hole portion are slidably connected with activity pilot hole support portion, and the other end and clamping feeding size end rotation connect It connects, is relatively set with pilot hole connector in the corresponding position in activity pilot hole portion I, activity pilot hole portion II.
2. cornual plate according to claim 1 positions pilot hole binding clasp, it is characterised in that: the support portion further includes support Bar, support rod are connected and fixed cornual plate positioning head and clamping head, the axial direction of clamping head be provided with hold clamp feeding portion pass through it is logical Hole.
3. cornual plate according to claim 1 positions pilot hole binding clasp, it is characterised in that: the clamping feeding portion includes clamping Feed bar, hand-held feeding swingle;The end for clamping feed bar passes through clamping head, and can be under the action of hand-held feeding swingle Along sliding axially for clamping head.
4. cornual plate according to claim 3 positions pilot hole binding clasp, it is characterised in that: the hand-held feeding swingle is to wear Cross the rod-like element for clamping feed bar radial direction.
5. cornual plate according to claim 3 or 4 positions pilot hole binding clasp, it is characterised in that: clamping feed bar and holding It is provided with external screw thread on the body of rod between feeding swingle, is matched with the internal screw thread for being set to clamping head.
6. cornual plate according to claim 1 positions pilot hole binding clasp, it is characterised in that: the cornual plate positioning head and clamp into It is made of to the head end in portion polyhedron of the axis on same straight line and rotary table, and the upper bottom surface of rotary table is opposite.
7. cornual plate according to claim 6 positions pilot hole binding clasp, it is characterised in that: on certain polyhedral one side It is provided with ears piece, activity pilot hole portion I, activity pilot hole portion II are rotatablely connected with ears piece respectively.
8. cornual plate according to claim 1 positions pilot hole binding clasp, it is characterised in that: the activity pilot hole support portion includes Spring, spring loop bar and pilot hole boom, spring are placed in spring loop bar, and pilot hole boom is placed in the both ends of spring, for limiting bullet The movement of spring, free end are pierced by spring loop bar and connect respectively with activity pilot hole portion I, activity pilot hole portion II, and in activity pilot hole Sliding axially along spring loop bar under the action of portion II.
9. cornual plate according to claim 1 positions pilot hole binding clasp, it is characterised in that: activity pilot hole portion I includes song Handle, pilot hole handle and pilot hole connector, one end of crank and cornual plate positioning head are rotatablely connected, and the other end and pilot hole handle are rotatablely connected, and are drawn The other end of hole connector and pilot hole handle is connected and fixed;Activity pilot hole portion II includes crank, pilot hole handle, pilot hole major joint and pilot hole Bar, one end of crank and cornual plate positioning head are rotatablely connected, and the other end and pilot hole handle are rotatablely connected, pilot hole major joint and pilot hole handle The other end is slidably connected, and is gap-matched with pilot hole bar, and realizes pilot hole major joint in pilot hole under the action of pilot hole bar Sliding in handle.
10. cornual plate according to claim 1 positions pilot hole binding clasp, it is characterised in that: activity pilot hole portion II is also wrapped Spring is included, spring pocket is limited between pilot hole handle and the tail portion of pilot hole bar on pilot hole bar.
CN201811497803.7A 2018-12-07 2018-12-07 Corner piece positioning hole-leading clamp Active CN109514300B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811497803.7A CN109514300B (en) 2018-12-07 2018-12-07 Corner piece positioning hole-leading clamp

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811497803.7A CN109514300B (en) 2018-12-07 2018-12-07 Corner piece positioning hole-leading clamp

Publications (2)

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CN109514300A true CN109514300A (en) 2019-03-26
CN109514300B CN109514300B (en) 2020-11-24

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113305494A (en) * 2021-06-11 2021-08-27 贵州永红航空机械有限责任公司 Special positioning and rotating welding tool and welding method for bobbin assembly

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU557855A1 (en) * 1975-02-18 1977-05-15 Всесоюзный заочный машиностроительный институт Riveting device
DE29910335U1 (en) * 1999-06-14 1999-09-16 Emhart Inc Device for performing mechanical work on components by means of tool elements, which are arranged on a, preferably C-shaped, tool holder
CN201324812Y (en) * 2008-09-23 2009-10-14 山东科技大学 Manually-controlled suspended hydraulic self-piercing riveting machine
JP3161632U (en) * 2010-05-24 2010-08-05 株式会社 三協 Rivet tool
CN201693217U (en) * 2010-03-16 2011-01-05 沈阳飞机工业(集团)有限公司 Arch-shaped hole digger
CN202367476U (en) * 2011-12-23 2012-08-08 杨俊华 Corner drilling fixing device
CN104439016A (en) * 2014-11-28 2015-03-25 马瑞利汽车零部件(芜湖)有限公司 Rivet installation device
CN104890892A (en) * 2015-04-24 2015-09-09 江西洪都航空工业集团有限责任公司 Mechanical aircraft rudder surface structure clamping tool

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU557855A1 (en) * 1975-02-18 1977-05-15 Всесоюзный заочный машиностроительный институт Riveting device
DE29910335U1 (en) * 1999-06-14 1999-09-16 Emhart Inc Device for performing mechanical work on components by means of tool elements, which are arranged on a, preferably C-shaped, tool holder
CN201324812Y (en) * 2008-09-23 2009-10-14 山东科技大学 Manually-controlled suspended hydraulic self-piercing riveting machine
CN201693217U (en) * 2010-03-16 2011-01-05 沈阳飞机工业(集团)有限公司 Arch-shaped hole digger
JP3161632U (en) * 2010-05-24 2010-08-05 株式会社 三協 Rivet tool
CN202367476U (en) * 2011-12-23 2012-08-08 杨俊华 Corner drilling fixing device
CN104439016A (en) * 2014-11-28 2015-03-25 马瑞利汽车零部件(芜湖)有限公司 Rivet installation device
CN104890892A (en) * 2015-04-24 2015-09-09 江西洪都航空工业集团有限责任公司 Mechanical aircraft rudder surface structure clamping tool

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113305494A (en) * 2021-06-11 2021-08-27 贵州永红航空机械有限责任公司 Special positioning and rotating welding tool and welding method for bobbin assembly

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Address after: Nanchang high tech Industrial Development Zone, Jiangxi Province

Patentee after: JIANGXI HONGDU AVIATION INDUSTRY GROUP Co.,Ltd.

Address before: 330000 Jiangxi city in Nanchang Province, the new bridge box 460 box 5001

Patentee before: JIANGXI HONGDU AVIATION INDUSTRY GROUP Co.,Ltd.