CN201124253Y - Drilling mould for drilling rotating shaft hole of hinge - Google Patents

Drilling mould for drilling rotating shaft hole of hinge Download PDF

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Publication number
CN201124253Y
CN201124253Y CNU2007200825442U CN200720082544U CN201124253Y CN 201124253 Y CN201124253 Y CN 201124253Y CN U2007200825442 U CNU2007200825442 U CN U2007200825442U CN 200720082544 U CN200720082544 U CN 200720082544U CN 201124253 Y CN201124253 Y CN 201124253Y
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China
Prior art keywords
plate
drill
main body
hole
drilling
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Expired - Lifetime
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CNU2007200825442U
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Chinese (zh)
Inventor
傅盱成
谭华
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Chengdu Aircraft Industrial Group Co Ltd
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Chengdu Aircraft Industrial Group Co Ltd
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Priority to CNU2007200825442U priority Critical patent/CN201124253Y/en
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Publication of CN201124253Y publication Critical patent/CN201124253Y/en
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Abstract

The utility model discloses a drill hole die for drilling shaft holes of a hinge. The drill hole die comprises a baffle (1), a drill body (2), a drill plate (4), an end head drill plate (5), a bearing plate (6) and a set screw (7), wherein the drill plate (4) and the end head drill plate (5) are fastened on the drill body (2); one side of the drill plate (4) and the end head drill plate (5) is made into a group of concave-convex teeth engaged with grooves and bumps on hinge-like parts; lead holes are arranged on the group of concave-convex teeth; and a drill bit starts to drill from the lead hole of the end head drill plate (5) while drilling a shaft hole. By adopting module replaceable manner of the drill plate, the drill hole die may adopt a plurality of drill plates (4) based on the specific length of hinge-like parts to achieve combination positioning, thereby greatly improving the design of drill hole die and manufacture progress. The drill hole die is suitable for drilling holes of hinge-like parts of various lengths, one-way drilling hole or two-way drilling holes and can ensure the hole accuracy and coaxiality.

Description

A kind of boring mould that bores system hinge leaf shaft hole
Technical field
The utility model relates to a kind of boring mould that bores system hinge leaf shaft hole.
Background technology
The groove and the projection of two hinge leaf of hinge leaf class part are meshing with each other, and rotate around common rotating shaft, and hinge leaf class part is generally plate shaped, and length scale does not wait, from 200mm to 1000mm more than, its shaft hole is generally about Φ 4mm.The processing of this elongated hole adopts deep hole equipment to process at present abroad, and domestic use drilling machine or pneumatic drill are processed, the method that adopts two ends boring to connect, the hole precision that often gets out is not high, axiality can not reach requirement, the work in-process difficult quality guarantee is when shaft hole is very long even can't process.
Summary of the invention:
The technical problems to be solved in the utility model is to provide a kind of boring mould that bores system hinge leaf shaft hole, when adopting the method for two ends boring connection, the aperture can not misplace, and when the hinge leaf class part of processing different length, can use the boring mould of this kind structure.
For solving the problems of the technologies described above, the utility model provides a kind of boring mould that bores system hinge leaf shaft hole, comprise: baffle plate, the drill jig main body, bushing plate, the termination bushing plate, backing plate and holding screw, described bushing plate is fastened on the drill jig main body by two pins and a screw location, one side of bushing plate and termination bushing plate manufacture with hinge leaf class part on groove and the intermeshing one group of concavo-convex profile of tooth of projection, on the concavo-convex profile of tooth of this group, have the bullport of perforation, length according to hinge leaf class part, some bushing plates and a termination bushing plate are set, described baffle plate and backing plate are fixed tightly in the two ends of drill jig main body respectively, the width of baffle plate and backing plate is greater than the width of drill jig main body, stablize and have a screwed hole on the backing plate, holding screw can rotate advance and retreat in the screwed hole of backing plate, the one side of described drill jig main body is made step surface, have some groups of pin holes and screwed hole on the lower step surface, in order to fixedly bushing plate and termination bushing plate, also make some through holes and groove on the lower in addition step surface, during use, hinge leaf class part lies on the drill jig main body plane, clamp two ends by the holding screw on baffle plate and the backing plate, with general pressing plate or Pressing clamp hinge leaf class part is pressed on the drill jig main body, when boring shaft hole, drill bit begins the system of boring from termination bushing plate bullport.
The utility model has following good effect than prior art.Bushing plate adopts the interchangeable mode of modular, can adopt some bushing plates to carry out integrated positioning according to the length of concrete part, can improve the design and the manufacturing progress of boring mould greatly, adapt to the boring of all lengths hinge leaf class part, unidirectional boring or two ends boring are connected and all can be guaranteed hole precision and axiality.
Description of drawings
Fig. 1 is a kind of hinge leaf class part schematic diagram of boring mould processing of the present utility model.
Fig. 2 is a kind of boring mode structure schematic diagram that bores system hinge leaf shaft hole of the present utility model.
Fig. 3 is a kind of drill jig main body stereogram that bores the boring mould of system hinge leaf shaft hole of the present utility model.
Fig. 4 is a kind of bushing plate stereogram that bores the boring mould of system hinge leaf shaft hole of the present utility model.
Fig. 5 is a kind of termination bushing plate stereogram that bores the boring mould of system hinge leaf shaft hole of the present utility model.
The specific embodiment
Below in conjunction with embodiment the utility model is further described.
Fig. 1 shows a kind of hinge leaf class part, is " L " type, has the shaft hole that runs through on fluted limit.
Bushing plate 4 and termination bushing plate 5 are fastened on the drill jig main body 2 by two pins and a screw location among Fig. 2, one side of bushing plate 4 and bushing plate 5 manufacture with hinge leaf class part on groove and the intermeshing one group of concavo-convex profile of tooth of projection, on the concavo-convex profile of tooth of this group, have the bullport of perforation, length according to hinge leaf class part 3, some bushing plates 4 and a termination bushing plate 5 are set, described baffle plate 1 and backing plate 6 are fixed tightly in the two ends of drill jig main body 2 respectively, the width of baffle plate 1 and backing plate 6 is greater than the width of drill jig main body 2,6 have a screwed hole on the backing plate, holding screw 7 can rotate advance and retreat in the screwed hole of backing plate, during use, hinge leaf class part 3 lies on drill jig main body 2 planes, utilize the location, the inboard baseplane of groove on the bushing plate 4, clamp two ends by the holding screw on baffle plate 1 and the backing plate 67, by general pressing plate or Pressing clamp hinge leaf class part 3 and drill jig main body 2 are compressed together, when boring shaft hole, begin the system of boring from the bullport of termination bushing plate 5.
Among Fig. 3, the drill jig main body adopts the tool steel manufacturing, both ends of the surface have three screwed holes and two pin holes are used for fixing baffle plate and backing plate, the one side of drill jig main body is made step surface, when hinge leaf class part lies in two step surface intersections, hinge leaf class part shaft hole limit is unsettled, have some groups of pin holes and screwed hole on the lower step surface, in order to fixedly bushing plate and termination bushing plate, also make some tapped through holes and groove on the lower in addition step surface, compress the spacing of the pressing plate of product parts and pressing plate in order to installation.As clamp is installed then on main body, is made the respective threads installing hole.
Fig. 4 and Fig. 5 are the stereograms of bushing plate and front end bushing plate.

Claims (3)

1. one kind is bored the boring mould of making the hinge leaf shaft hole, comprise: baffle plate (1), drill jig main body (2), bushing plate (4), termination bushing plate (5), backing plate (6) and holding screw (7), described baffle plate (1) and backing plate (6) are fixed tightly in the two ends of drill jig main body (2) respectively, the width of baffle plate (1) and backing plate (6) is greater than the width of drill jig main body, have a screwed hole on the backing plate (6), holding screw (7) can rotate advance and retreat and hold out against product parts in the screwed hole of backing plate, described drill jig main body (2) has some groups of pin holes and screwed hole, in order to fixedly bushing plate (4) and termination bushing plate (5), it is characterized in that: described bushing plate (4) and termination bushing plate (5) are fastened on the drill jig main body, one side of bushing plate (4) and termination bushing plate (5) manufacture with hinge leaf class part on groove and the intermeshing one group of concavo-convex profile of tooth of projection, on the concavo-convex profile of tooth of this group, have the bullport of perforation.
2. a kind of boring mould that bores system hinge leaf shaft hole according to claim 1, it is characterized in that: the one side of described drill jig main body (2) is made step surface.
3. a kind of boring mould that bores system hinge leaf shaft hole according to claim 1, it is characterized in that: described bushing plate (4) can be provided with some according to the concrete length of hinge leaf class part.
CNU2007200825442U 2007-12-19 2007-12-19 Drilling mould for drilling rotating shaft hole of hinge Expired - Lifetime CN201124253Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNU2007200825442U CN201124253Y (en) 2007-12-19 2007-12-19 Drilling mould for drilling rotating shaft hole of hinge

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNU2007200825442U CN201124253Y (en) 2007-12-19 2007-12-19 Drilling mould for drilling rotating shaft hole of hinge

Publications (1)

Publication Number Publication Date
CN201124253Y true CN201124253Y (en) 2008-10-01

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Family Applications (1)

Application Number Title Priority Date Filing Date
CNU2007200825442U Expired - Lifetime CN201124253Y (en) 2007-12-19 2007-12-19 Drilling mould for drilling rotating shaft hole of hinge

Country Status (1)

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CN (1) CN201124253Y (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102284723A (en) * 2011-08-12 2011-12-21 贵阳国威机械有限公司 Drilling jig clamp for assembly hole of motorcycle camshaft fixed seat
CN102476207A (en) * 2010-11-25 2012-05-30 中国商用飞机有限责任公司 Processing fixture and assembling method for long-hinge part
CN102649173A (en) * 2012-04-28 2012-08-29 苏州金牛精密机械有限公司 Flange plane drilling jig
CN102699387A (en) * 2012-06-06 2012-10-03 沈阳飞机工业(集团)有限公司 Hinge drill jig for drilling small holes on long-shaft parts, and processing method of hinge drill jig
CN103769798A (en) * 2014-01-27 2014-05-07 哈尔滨飞机工业集团有限责任公司 Manufacturing technique of main inspection drill jig
CN104259524A (en) * 2014-10-17 2015-01-07 无锡市宏源弹性器材有限公司 Jack indexing jig
CN105014123A (en) * 2015-07-06 2015-11-04 中国人民解放军第五七〇六工厂 Hinge type part drilling clamp
CN104259524B (en) * 2014-10-17 2017-01-04 无锡市宏源弹性器材有限公司 Jack indexing jig
CN112621106A (en) * 2020-12-29 2021-04-09 中国航发湖南南方宇航工业有限公司 Groove machining method
CN113369530A (en) * 2021-06-23 2021-09-10 成都飞机工业(集团)有限责任公司 Device for making holes in aircraft skin and using method thereof
CN113618101A (en) * 2021-08-18 2021-11-09 成都飞机工业(集团)有限责任公司 Drilling device and drilling method for upper skin of closed box structure on wing

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102476207A (en) * 2010-11-25 2012-05-30 中国商用飞机有限责任公司 Processing fixture and assembling method for long-hinge part
CN102284723A (en) * 2011-08-12 2011-12-21 贵阳国威机械有限公司 Drilling jig clamp for assembly hole of motorcycle camshaft fixed seat
CN102649173A (en) * 2012-04-28 2012-08-29 苏州金牛精密机械有限公司 Flange plane drilling jig
CN102699387A (en) * 2012-06-06 2012-10-03 沈阳飞机工业(集团)有限公司 Hinge drill jig for drilling small holes on long-shaft parts, and processing method of hinge drill jig
CN103769798A (en) * 2014-01-27 2014-05-07 哈尔滨飞机工业集团有限责任公司 Manufacturing technique of main inspection drill jig
CN103769798B (en) * 2014-01-27 2016-01-20 哈尔滨飞机工业集团有限责任公司 A kind of main inspection drill jig method of manufacturing technology
CN104259524B (en) * 2014-10-17 2017-01-04 无锡市宏源弹性器材有限公司 Jack indexing jig
CN104259524A (en) * 2014-10-17 2015-01-07 无锡市宏源弹性器材有限公司 Jack indexing jig
CN105014123A (en) * 2015-07-06 2015-11-04 中国人民解放军第五七〇六工厂 Hinge type part drilling clamp
CN105014123B (en) * 2015-07-06 2018-01-23 中国人民解放军第五七〇六工厂 A kind of hinge-type part drilling clamp
CN112621106A (en) * 2020-12-29 2021-04-09 中国航发湖南南方宇航工业有限公司 Groove machining method
CN112621106B (en) * 2020-12-29 2022-02-15 中国航发湖南南方宇航工业有限公司 Groove machining method
CN113369530A (en) * 2021-06-23 2021-09-10 成都飞机工业(集团)有限责任公司 Device for making holes in aircraft skin and using method thereof
CN113618101A (en) * 2021-08-18 2021-11-09 成都飞机工业(集团)有限责任公司 Drilling device and drilling method for upper skin of closed box structure on wing

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Granted publication date: 20081001