CN202399051U - Aviation casing part fixture - Google Patents

Aviation casing part fixture Download PDF

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Publication number
CN202399051U
CN202399051U CN2011204798633U CN201120479863U CN202399051U CN 202399051 U CN202399051 U CN 202399051U CN 2011204798633 U CN2011204798633 U CN 2011204798633U CN 201120479863 U CN201120479863 U CN 201120479863U CN 202399051 U CN202399051 U CN 202399051U
Authority
CN
China
Prior art keywords
base
anchor clamps
aviation casing
casing
aviation
Prior art date
Application number
CN2011204798633U
Other languages
Chinese (zh)
Inventor
冯守胜
陈要武
赵江涛
Original Assignee
沈阳黎明航空发动机(集团)有限责任公司
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 沈阳黎明航空发动机(集团)有限责任公司 filed Critical 沈阳黎明航空发动机(集团)有限责任公司
Priority to CN2011204798633U priority Critical patent/CN202399051U/en
Application granted granted Critical
Publication of CN202399051U publication Critical patent/CN202399051U/en

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Abstract

The utility model provides an aviation casing part fixture, which is characterized by mainly comprising a base, positioning blocks and pressure plates. Bolt holes, a center hole and a chute which are used for being connected with a machine tool are arranged on the base, and the positioning blocks and the pressure plates are respectively mounted on the base by sliders and connecting bolts. The aviation casing part fixture has the advantages of simple structure, convenience in clamping, low labor intensity of production workers and fine universality.

Description

A kind of aviation casing is used anchor clamps
Technical field
The utility model relates to jig.
Background technology
In batch process, use the existing universal fixturing clamping time long, labour intensity is big, and uses special fixture can increase the frock expense.
Summary of the invention
The purpose of the utility model is to provide a kind of jig that supplies aviation casing class part to use.
The utility model provides a kind of aviation casing to use anchor clamps; It is characterized in that: mainly comprise base, locating piece and pressing plate; The bolt hole, centre bore and the chute that are connected usefulness with lathe are arranged on the base, and locating piece and pressing plate are installed on the base with slide block and connecting bolt respectively.
Earlier base is fixed by bolts on the lathe during use, locating piece is fixed on forms seam on the base again, load onto work piece---behind the casing (as shown in Figure 5), it is clamped with pressing plate.
The aviation casing that the utility model provides is used anchor clamps, on its base the centering band can be arranged, so that the position of centering base on lathe.
The aviation casing that the utility model provides is used anchor clamps; It can be equipped with the location exemplar of band alignment pin, and alignment pin matches with the centre bore of base, and locating piece leans on exemplar outer end, location mutually; So that confirm the distance of locating piece rapidly, i.e. the radius of seam to the base center.
The aviation casing that the utility model provides is used anchor clamps, in its centre hole of base lining can be arranged, to increase the wearability of base.
The aviation casing that the utility model provides is used anchor clamps, and its pressing plate is with the work piece contact position soft foil metal being arranged, in order to avoid crush work piece.
The aviation casing that the utility model provides is used anchor clamps, and its advantage is: simple in structure, convenient mounting and clamping, and direct labor's labour intensity is low, and versatility is good.
Description of drawings
Fig. 1 is the structural representation of aviation casing with anchor clamps;
Fig. 2 is the A-A profile of aviation casing with anchor clamps;
Fig. 3 is the B-B profile of aviation casing with anchor clamps;
Fig. 4 is the sketch map of aviation casing with the anchor clamps pressing plate;
Fig. 5 is an aviation casing sketch map.
The specific embodiment
Embodiment 1
The aviation casing is used anchor clamps; Its structure is as shown in Figure 1; Comprise the location exemplar 3 and the pressing plate 4 of base 1, locating piece 2, band alignment pin, the bolt hole, centre bore, chute and the centering band that are connected usefulness with lathe are arranged on the base 1, locating piece 2 is installed on the base with slide block 5 and connecting bolt 6 respectively with pressing plate 4; The alignment pin of location exemplar 3 matches with the centre bore of base 1; Locating piece 2 leans on exemplar 3 outer ends, location mutually, and lining 8 is arranged in the centre hole of base, and pressing plate 4 is having soft foil metal with the work piece contact position---aluminium backing 7.

Claims (7)

1. an aviation casing is used anchor clamps, it is characterized in that: mainly comprise base, locating piece and pressing plate, the bolt hole, centre bore and the chute that are connected usefulness with lathe are arranged on the base, locating piece and pressing plate are installed on the base with slide block and connecting bolt respectively.
2. use anchor clamps according to the described aviation casing of claim 1, it is characterized in that: the centering band is arranged on the said base.
3. use anchor clamps according to the described aviation casing of claim 1, it is characterized in that: be equipped with the location exemplar of band alignment pin, alignment pin matches with the centre bore of base, and locating piece leans on exemplar outer end, location mutually.
4. use anchor clamps according to the described aviation casing of claim 2, it is characterized in that: be equipped with the location exemplar of band alignment pin, alignment pin matches with the centre bore of base, and locating piece leans on exemplar outer end, location mutually.
5. use anchor clamps according to the described aviation casing of claim 3, it is characterized in that: in the said centre hole of base lining is arranged.
6. use anchor clamps according to the described aviation casing of claim 4, it is characterized in that: in the said centre hole of base lining is arranged.
7. use anchor clamps according to the described aviation casing of one of claim 1 ~ 6, it is characterized in that: said pressing plate is having soft foil metal with the work piece contact position.
CN2011204798633U 2011-11-28 2011-11-28 Aviation casing part fixture CN202399051U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011204798633U CN202399051U (en) 2011-11-28 2011-11-28 Aviation casing part fixture

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2011204798633U CN202399051U (en) 2011-11-28 2011-11-28 Aviation casing part fixture

Publications (1)

Publication Number Publication Date
CN202399051U true CN202399051U (en) 2012-08-29

Family

ID=46696727

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2011204798633U CN202399051U (en) 2011-11-28 2011-11-28 Aviation casing part fixture

Country Status (1)

Country Link
CN (1) CN202399051U (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103481084A (en) * 2013-09-13 2014-01-01 沈阳黎明航空发动机(集团)有限责任公司 Multi-function positioning clamping method for machining receivers
CN103624596A (en) * 2013-12-09 2014-03-12 常州兰翔机械有限责任公司 Linear cutting clamp for starter front mounting side
CN103624352A (en) * 2013-12-09 2014-03-12 常州兰翔机械有限责任公司 Linear cutting clamp for mounting edge
CN104690569A (en) * 2013-12-10 2015-06-10 大连顺杰机械有限公司 Clamp of circular workpiece
CN105290737A (en) * 2015-11-20 2016-02-03 沈阳黎明航空发动机(集团)有限责任公司 Machining method for casing casting part
CN105290814A (en) * 2015-11-20 2016-02-03 沈阳黎明航空发动机(集团)有限责任公司 Rapid and universal positioning clamp and application method thereof
CN105397108A (en) * 2015-11-24 2016-03-16 沈阳黎明航空发动机(集团)有限责任公司 Method for turning large-diameter precision complex molded surface thin sheet part
CN105855961A (en) * 2016-06-01 2016-08-17 济南大学 Flexible fixture for case
CN106624300A (en) * 2015-10-28 2017-05-10 中航湖南通用航空发动机有限公司 Welding fixture for cartridge receiver
CN106624547A (en) * 2016-12-09 2017-05-10 成都发动机(集团)有限公司 Device for welding and assembling installation seats on aero-engine combustor diffuser case
CN108098585A (en) * 2017-12-18 2018-06-01 中国航发贵州黎阳航空动力有限公司 A kind of imperfect arc surface grinding measurement servicing unit and aligning method

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103481084A (en) * 2013-09-13 2014-01-01 沈阳黎明航空发动机(集团)有限责任公司 Multi-function positioning clamping method for machining receivers
CN103624596A (en) * 2013-12-09 2014-03-12 常州兰翔机械有限责任公司 Linear cutting clamp for starter front mounting side
CN103624352B (en) * 2013-12-09 2016-06-22 常州兰翔机械有限责任公司 A kind of installation limit linear cutting clamp
CN105108254A (en) * 2013-12-09 2015-12-02 常州兰翔机械有限责任公司 Line cutting fixture suitable for one-time machining forming of starter front flange
CN103624596B (en) * 2013-12-09 2015-12-09 常州兰翔机械有限责任公司 Mounting edge linear cutting clamp before starter
CN103624352A (en) * 2013-12-09 2014-03-12 常州兰翔机械有限责任公司 Linear cutting clamp for mounting edge
CN105108254B (en) * 2013-12-09 2017-11-07 中国航发常州兰翔机械有限责任公司 Suitable for installing side linear cutting clamp before the starter that is processed and formed at one time
CN104690569A (en) * 2013-12-10 2015-06-10 大连顺杰机械有限公司 Clamp of circular workpiece
CN106624300A (en) * 2015-10-28 2017-05-10 中航湖南通用航空发动机有限公司 Welding fixture for cartridge receiver
CN105290737A (en) * 2015-11-20 2016-02-03 沈阳黎明航空发动机(集团)有限责任公司 Machining method for casing casting part
CN105290814A (en) * 2015-11-20 2016-02-03 沈阳黎明航空发动机(集团)有限责任公司 Rapid and universal positioning clamp and application method thereof
CN105397108A (en) * 2015-11-24 2016-03-16 沈阳黎明航空发动机(集团)有限责任公司 Method for turning large-diameter precision complex molded surface thin sheet part
CN105397108B (en) * 2015-11-24 2018-09-04 沈阳黎明航空发动机(集团)有限责任公司 A kind of process of major diameter precision complex profile sheet parts Vehicle Processing
CN105855961A (en) * 2016-06-01 2016-08-17 济南大学 Flexible fixture for case
CN106624547A (en) * 2016-12-09 2017-05-10 成都发动机(集团)有限公司 Device for welding and assembling installation seats on aero-engine combustor diffuser case
CN108098585A (en) * 2017-12-18 2018-06-01 中国航发贵州黎阳航空动力有限公司 A kind of imperfect arc surface grinding measurement servicing unit and aligning method

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Date Code Title Description
GR01 Patent grant
C14 Grant of patent or utility model
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20120829

Termination date: 20161128

CF01 Termination of patent right due to non-payment of annual fee