CN102554646B - A kind of five-axle linkage turn-milling complex machining center aero-engine casing processing flexible jig - Google Patents

A kind of five-axle linkage turn-milling complex machining center aero-engine casing processing flexible jig Download PDF

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Publication number
CN102554646B
CN102554646B CN201110462652.3A CN201110462652A CN102554646B CN 102554646 B CN102554646 B CN 102554646B CN 201110462652 A CN201110462652 A CN 201110462652A CN 102554646 B CN102554646 B CN 102554646B
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China
Prior art keywords
aero
engine casing
down mechanism
hold
machining center
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CN201110462652.3A
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Chinese (zh)
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CN102554646A (en
Inventor
郭世栋
严金龙
吴兴海
陈正峰
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HANGZHOU TIANYANG MACHINERY CO Ltd
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HANGZHOU TIANYANG MACHINERY CO Ltd
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Application filed by HANGZHOU TIANYANG MACHINERY CO Ltd filed Critical HANGZHOU TIANYANG MACHINERY CO Ltd
Priority to CN201610547049.8A priority Critical patent/CN106002386B/en
Priority to CN201110462652.3A priority patent/CN102554646B/en
Priority to CN201610543829.5A priority patent/CN106078268B/en
Publication of CN102554646A publication Critical patent/CN102554646A/en
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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23Q—DETAILS, 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
    • B23Q3/00—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
    • B23Q3/02—Devices 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
    • B23Q3/06—Work-clamping means
    • B23Q3/062—Work-clamping means adapted for holding workpieces having a special form or being made from a special material
    • B23Q3/065—Work-clamping means adapted for holding workpieces having a special form or being made from a special material for holding workpieces being specially deformable, e.g. made from thin-walled or elastic material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23Q—DETAILS, 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
    • B23Q3/00—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
    • B23Q3/02—Devices 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
    • B23Q3/06—Work-clamping means
    • B23Q3/062—Work-clamping means adapted for holding workpieces having a special form or being made from a special material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass

Abstract

A kind of five-axle linkage turn-milling complex machining center aero-engine casing processing flexible jig, it is used for five-axle linkage integration machining center, six pairs of ring-type equally distributed handles are connected with outside hold-down mechanism and are fixed on outer side compression support dish, ring-type equally distributed handle is connected with inner side hold-down mechanism and is fixed on interior side compression support dish by corresponding six therewith, outer side compression support dish and interior side compression support dish are respectively connected and fixed on base by six roots of sensation column, it is respectively arranged with a set of bottom hold-down mechanism between outside six roots of sensation column and base, column upper end, inner side connects a top cover plate.The present invention, by inwall and the clamping device of outer wall and adjustable mechanism, controls the deformation in the aero-engine casing course of processing, thus saves aero-engine casing process time, improves crudy and efficiency.

Description

A kind of five-axle linkage turn-milling complex machining center aero-engine casing processing flexible jig
[technical field]
The present invention relates to a kind of aero-engine casing processing equipment, be specifically related to a kind of five-axle linkage turn-milling complex machining center aero-engine casing processing flexible jig.
[background technology]
Aero-engine casing processing belongs to most advanced and sophisticated precision equipment manufacture field, and the precision to equipment, processing technique has the highest requirement.Existing technique uses the process route of the multiple stage lathe compositions such as vertical car, sleeping carriage, machining center to be processed during processing aero-engine casing, and this manufacturing procedure is more complicated, and production efficiency reduces the most greatly simultaneously.The most complicated manufacturing procedure increases production cost, simultaneously because whole aero-engine casing is found the process route that the multiple stage lathes such as car, sleeping carriage, machining center form by multiple differences, by operating technology, personnel proficiency level is affected, and causes the decrease in yield of aero-engine casing.
[summary of the invention]
Overcome above deficiency, one five-axle linkage turn-milling complex machining center aero-engine casing of the present invention processing flexible jig, this fixture is in the aero-engine casing course of processing, utilize turn-milling complex machining center and five-axle linkage technology and adjustable clamp once to complete the course of processing, production cost is greatly reduced and improves production efficiency.
The technical problem to be solved is: prior art device is complex procedures during processing aero-engine casing, and production efficiency is low, how by the production equipment of equipment improvement aero-engine casing, improves its production efficiency.
The technical solution adopted in the present invention is: a kind of five-axle linkage turn-milling complex machining center aero-engine casing processing flexible jig, it is used for five-axle linkage integration machining center, six pairs of ring-type equally distributed handles are connected with outside hold-down mechanism and are fixed on outer side compression support dish, ring-type equally distributed handle is connected with inner side hold-down mechanism and is fixed on interior side compression support dish by corresponding six therewith, outer side compression support dish and interior side compression support dish are respectively connected and fixed on base by six roots of sensation column, it is respectively arranged with a set of bottom hold-down mechanism between outside six roots of sensation column and base, column upper end, inner side connects a top cover plate.
A kind of five-axle linkage turn-milling complex machining center aero-engine casing processing flexible jig, it is processing the inner side of aero-engine casing when, hold-down mechanism, inner side hold-down mechanism inside assembly are propped up support plate, top cover plate removal, then prop up support plate, base, bottom hold-down mechanism by outside hold-down mechanism, aero-engine casing is flown part and is clamped and positions.
When needs are to the when of being processed outside aero-engine casing, bottom hold-down mechanism, column, outside hold-down mechanism are propped up support plate, outside hold-down mechanism removal, props up support plate, inner side hold-down mechanism by top cover plate, inner side hold-down mechanism and aero-engine casing is flown part be clamped and position.
The method have the benefit that the present invention passes through inwall and the clamping device of outer wall and adjustable mechanism, control the deformation in the aero-engine casing course of processing, thus save aero-engine casing process time, improve crudy and efficiency.
For making to be further understood that inventive feature and technology contents, refer to embodiment of the present invention, but institute's embodiment is only for reference and explanation use, is not to be any limitation as the present invention.
[accompanying drawing explanation]
Fig. 1 is present configuration schematic diagram；
Fig. 2 is A-A ' sectional view of the present invention；
In figure, 1-handle；Hold-down mechanism outside 2-；Hold-down mechanism inside 3-；4-base；Hold-down mechanism bottom 5-；6-column；Outside 7-, hold-down mechanism props up support plate；Inside 8-, hold-down mechanism props up support plate；9-top cover plate.
[detailed description of the invention]
Below in conjunction with specific embodiment, the present invention is elaborated:
As shown in the figure, a kind of five-axle linkage turn-milling complex machining center aero-engine casing processing flexible jig, it is used for five-axle linkage integration machining center, six pairs of ring-type equally distributed handles 1 are connected with outside hold-down mechanism 2 and are fixed on outer side compression support dish 7, ring-type equally distributed handle 1 is connected with inner side hold-down mechanism 3 and is fixed on interior side compression support dish 8 by corresponding six therewith, outer side compression support dish 3 and interior side compression support dish 8 are respectively connected and fixed on base 4 by six roots of sensation column 6, it is respectively arranged with a set of bottom hold-down mechanism 5 between outside six roots of sensation column 6 and base 4, column 6 upper end, inner side connects a top cover plate 9.
Embodiment 1, a kind of five-axle linkage turn-milling complex machining center aero-engine casing processing flexible jig, it is processing the inner side of aero-engine casing when, hold-down mechanism, inner side hold-down mechanism inside assembly are propped up support plate, top cover plate removal, then prop up support plate, base, bottom hold-down mechanism by outside hold-down mechanism, aero-engine casing is flown part and is clamped and positions.
Embodiment 2, when needs are to the when of being processed outside aero-engine casing, bottom hold-down mechanism, column, outside hold-down mechanism are propped up support plate, outside hold-down mechanism removal, props up support plate, inner side hold-down mechanism by top cover plate, inner side hold-down mechanism and aero-engine casing is flown part be clamped and position.
The present invention, by inwall and the clamping device of outer wall and adjustable mechanism, controls the deformation in the aero-engine casing course of processing, thus saves aero-engine casing process time, simplifies manufacturing procedure, improves crudy and efficiency.
But the embodiment that the above-mentioned only present invention is the most feasible, non-therefore limit to scope, made various deformation according to above-described embodiment or apply mechanically all within this technical scheme protection domain.

Claims (1)

1. a five-axle linkage turn-milling complex machining center aero-engine casing processing flexible jig, it is characterized in that, including six ring-type equally distributed handle it is connected with outside hold-down mechanism and is fixed on outer side compression support dish, ring-type equally distributed handle is connected with inner side hold-down mechanism and is fixed on interior side compression support dish by corresponding six therewith, outer side compression support dish and interior side compression support dish are respectively connected and fixed on base by six roots of sensation column, being respectively arranged with a set of bottom hold-down mechanism between outside six roots of sensation column and base, column upper end, inner side connects a top cover plate.
CN201110462652.3A 2011-12-23 2011-12-23 A kind of five-axle linkage turn-milling complex machining center aero-engine casing processing flexible jig Active CN102554646B (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CN201610547049.8A CN106002386B (en) 2011-12-23 2011-12-23 Controllable machining deformation, the processing method of the aero-engine casing of saving process time
CN201110462652.3A CN102554646B (en) 2011-12-23 2011-12-23 A kind of five-axle linkage turn-milling complex machining center aero-engine casing processing flexible jig
CN201610543829.5A CN106078268B (en) 2011-12-23 2011-12-23 The method that five-axle linkage turn-milling complex machining center processes aero-engine casing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201110462652.3A CN102554646B (en) 2011-12-23 2011-12-23 A kind of five-axle linkage turn-milling complex machining center aero-engine casing processing flexible jig

Related Child Applications (2)

Application Number Title Priority Date Filing Date
CN201610547049.8A Division CN106002386B (en) 2011-12-23 2011-12-23 Controllable machining deformation, the processing method of the aero-engine casing of saving process time
CN201610543829.5A Division CN106078268B (en) 2011-12-23 2011-12-23 The method that five-axle linkage turn-milling complex machining center processes aero-engine casing

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CN102554646A CN102554646A (en) 2012-07-11
CN102554646B true CN102554646B (en) 2016-08-03

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CN201610543829.5A Active CN106078268B (en) 2011-12-23 2011-12-23 The method that five-axle linkage turn-milling complex machining center processes aero-engine casing
CN201610547049.8A Active CN106002386B (en) 2011-12-23 2011-12-23 Controllable machining deformation, the processing method of the aero-engine casing of saving process time
CN201110462652.3A Active CN102554646B (en) 2011-12-23 2011-12-23 A kind of five-axle linkage turn-milling complex machining center aero-engine casing processing flexible jig

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CN201610543829.5A Active CN106078268B (en) 2011-12-23 2011-12-23 The method that five-axle linkage turn-milling complex machining center processes aero-engine casing
CN201610547049.8A Active CN106002386B (en) 2011-12-23 2011-12-23 Controllable machining deformation, the processing method of the aero-engine casing of saving process time

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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
CN103639751B (en) * 2013-11-26 2016-01-20 沈阳黎明航空发动机(集团)有限责任公司 A kind of fixture of built-in compression link gear
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
CN103878604A (en) * 2014-02-21 2014-06-25 杭州天扬机械有限公司 Quick precise combined clamp for blisk processing
US20170056980A1 (en) * 2015-08-24 2017-03-02 General Electric Company Fixture for securing component to be drilled and method of drilling same
CN106624848A (en) * 2015-10-28 2017-05-10 中航湖南通用航空发动机有限公司 Thin-wall casing clamping fixture and machining method
CN105290836B (en) * 2015-11-23 2017-07-28 沈阳黎明航空发动机(集团)有限责任公司 A kind of big overhanging casing part processing clamp of narrow space
CN105817929B (en) * 2016-04-20 2019-02-12 北京航空航天大学 A kind of revolving body casing chucking appliance system and its application method
CN108262591A (en) * 2017-01-04 2018-07-10 东北林业大学 A kind of five shaft vertical turning-milling complex processing method of aero-engine casing
CN107649709B (en) * 2017-08-31 2019-03-01 中国航发航空科技股份有限公司 For containing the device of the split binding face processing of casing outside aero-engine
CN107937693A (en) * 2017-11-23 2018-04-20 中国航发沈阳黎明航空发动机有限责任公司 A kind of heat treatment deformation controls fixture
CN108637273A (en) * 2018-08-01 2018-10-12 湖南南方通用航空发动机有限公司 A kind of fixture and process of rotary part facing processing
CN109128914A (en) * 2018-10-19 2019-01-04 中国航发航空科技股份有限公司 A kind of deformation controller in hole for processing aero-engine casing end face lace structure
CN110774002A (en) * 2019-11-27 2020-02-11 中国航发贵州黎阳航空动力有限公司 Device and method for machining double-layer casing of aircraft engine
CN113561073B (en) * 2020-04-29 2022-07-05 中国航发商用航空发动机有限责任公司 Sand blasting tool for disc ring type parts
CN112276267B (en) * 2020-10-16 2022-09-27 长春理工大学 Titanium alloy weak-rigidity part precision linear cutting clamping device and working method thereof
CN113478263B (en) * 2021-07-20 2022-12-09 中国航发航空科技股份有限公司 Machining clamp for rectifying cone of aero-engine exhaust device and clamping method of machining clamp

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Also Published As

Publication number Publication date
CN106002386A (en) 2016-10-12
CN106078268A (en) 2016-11-09
CN106078268B (en) 2017-11-28
CN102554646A (en) 2012-07-11
CN106002386B (en) 2017-12-01

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Inventor after: Guo Shidong

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Inventor after: Wu Xinghai

Inventor after: Chen Zhengfeng

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