CN109532201A - A kind of blade laying positioning device - Google Patents

A kind of blade laying positioning device Download PDF

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Publication number
CN109532201A
CN109532201A CN201811322704.5A CN201811322704A CN109532201A CN 109532201 A CN109532201 A CN 109532201A CN 201811322704 A CN201811322704 A CN 201811322704A CN 109532201 A CN109532201 A CN 109532201A
Authority
CN
China
Prior art keywords
snap
gauge
bogusware
positioning
laying
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
CN201811322704.5A
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Chinese (zh)
Other versions
CN109532201B (en
Inventor
彭世林
叶强
彭广棚
江卫新
张亚龙
付柳勇
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.)
Changhe Aircraft Industries Group Co Ltd
Original Assignee
Changhe Aircraft Industries 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 Changhe Aircraft Industries Group Co Ltd filed Critical Changhe Aircraft Industries Group Co Ltd
Priority to CN201811322704.5A priority Critical patent/CN109532201B/en
Publication of CN109532201A publication Critical patent/CN109532201A/en
Application granted granted Critical
Publication of CN109532201B publication Critical patent/CN109532201B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/18Handling of layers or the laminate
    • B32B38/1825Handling of layers or the laminate characterised by the control or constructional features of devices for tensioning, stretching or registration
    • B32B38/1833Positioning, e.g. registration or centering
    • B32B38/1841Positioning, e.g. registration or centering during laying up

Landscapes

  • Jigs For Machine Tools (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

The present invention discloses a kind of blade laying positioning device, including die body (1), muti-piece snap-gauge (2) and bogusware (3), snap-gauge position line (1-1) on die body (1) carries out exhibition Xiang Dingwei to snap-gauge (2), snap-gauge positions side (2-2) and die body step (1-2) and cooperates to the tangential positioning of snap-gauge (2) progress, bogusware (3) is that the laying position line (2-1) and die body (1) cooperation in foundation snap-gauge (2) process, bogusware positions side (3-1) and die body step (1-2) fitting carries out tangential positioning to bogusware (3), snap-gauge (2) and bogusware boss (3-2) cooperation carry out exhibition Xiang Dingwei to bogusware (3) again, the positioning to laying (4) is realized in laying positioning side (3-3) of bogusware (3) after positioning.Blade laying positioning device of the invention is cooperated by snap-gauge and die body, is positioned to bogusware, and the bogusware after recycling positioning realizes the positioning to laying, in this way in batch production, it is not necessary to dimensional measurement is repeatedly carried out, so that laying efficiency can be improved.

Description

A kind of blade laying positioning device
Technical field
The invention belongs to technical field of composite material molding more particularly to a kind of blade laying positioning devices.
Background technique
Helicopter blade covering has compound glass cloth and carbon cloth laying, and each laying has different size and locations, therefore Need to position each laying position, common method be paving one layer generally have the cloth of 15mm surplus, then measure size into Row is cut, this laying method low efficiency.
Summary of the invention
In view of the above situation of the prior art, the object of the present invention is to provide a kind of blade laying positioning devices, to improve Laying efficiency.
Above-mentioned purpose of the invention is realized using technical solution below:
A kind of blade laying positioning device, including die body, muti-piece snap-gauge and bogusware, the snap-gauge position line on die body is to snap-gauge The exhibition of progress Xiang Dingwei, snap-gauge positions side and die body step cooperates to the tangential positioning of snap-gauge progress, and bogusware is according to the paving on snap-gauge What layer position line and die body cooperation processed.Bogusware positions side and the fitting of die body step and carries out tangential positioning to bogusware, snap-gauge and The cooperation of bogusware boss carries out exhibition Xiang Dingwei to bogusware again, and the positioning to laying is realized on the laying positioning side of the bogusware after positioning.
Further, the spacing of snap-gauge be 200~300mm, preferably 200mm, in this way, it is ensured that laying positioning side essence Degree.
Further, the material of snap-gauge is stainless steel plate, in this way, snap-gauge is unlikely to deform, it is easy to process.
Blade laying positioning device of the invention is cooperated by snap-gauge and die body, is positioned to bogusware, after recycling positioning Bogusware realizes the positioning to laying, in this way in batch production, it is not necessary to dimensional measurement is repeatedly carried out, so that laying effect can be improved Rate.
Detailed description of the invention
Fig. 1 is the axonometric drawing for indicating blade laying positioning device of the invention.
Specific embodiment
Below with reference to the accompanying drawings, in conjunction with the embodiments, blade laying positioning device of the invention is further illustrated.
Fig. 1 shows the structures of blade laying positioning device of the invention.As shown, blade laying of the invention positions dress It sets, including die body 1, the type face of muti-piece snap-gauge 2 and bogusware 3, die body 1 is consistent with blade profile, the snap-gauge position line on die body 1 The snap-gauge 2 that 1-1 is placed on die body 1 setting carries out exhibition Xiang Dingwei, and in the present specification, snap-gauge position line is referred to along mould Body 1 is opened up to distribution, and along the tangential a plurality of line portrayed on die body 1, the item number of snap-gauge position line is identical as the number of snap-gauge.
Snap-gauge positioning side 2-2 and die body step 1-2 cooperation on snap-gauge 2 carries out tangential positioning to snap-gauge 2, in this explanation In book, snap-gauge positioning side refers to the inside cell wall for the rectangular recess opened in snap-gauge lower edge, and recess width has no special requirements, The shape of snap-gauge lower edge is parallel with the type face of die body 1 of snap-gauge position, spaced apart, convenient for production bogusware, one As for 2mm or so.
It is indicated in the laying position line 2-1 and the processable bogusware 3 out of the cooperation of die body 1 of 2 lower edge of snap-gauge, in this specification In, bogusware refers to that shape is complementary with laying shape for positioning blade laying, cooperates with laying and constitutes blade profile shape Device, the corresponding bogusware of each blade laying, bogusware 3 is lain on die body 1, to the skill of aviation composite technical field For art personnel, bogusware is well known.Bogusware positioning side 3-1 and die body step 1-2 fitting carries out tangential positioning to bogusware 3, Snap-gauge 2 and bogusware boss 3-2 (bogusware 3 is arranged in close to the end of blade root in bogusware boss 3-2) cooperation again open up bogusware 3 To positioning, it is thus achieved that positioning of the bogusware 3 on die body 1.The laying positioning side 3-3 of bogusware 3 after positioning is realized to laying 4 positioning.
In the present embodiment, the spacing of snap-gauge 2 be 200~300mm, preferably 200mm, in this way, it is ensured that laying position side The precision of 3-3.In addition, the material of snap-gauge 2 is preferably stainless steel plate, in this way, snap-gauge is unlikely to deform, it is easy to process.
Blade laying positioning device of the invention is cooperated by snap-gauge and die body, is positioned to bogusware, after recycling positioning Bogusware realizes the positioning to laying, in this way in batch production, it is not necessary to dimensional measurement is repeatedly carried out, so that laying effect can be improved Rate.

Claims (4)

1. a kind of blade laying positioning device, including die body (1), muti-piece snap-gauge (2) and bogusware (3), the snap-gauge on die body (1) is fixed Bit line (1-1) carries out exhibition Xiang Dingwei to snap-gauge (2), and snap-gauge positions side (2-2) and die body step (1-2) and cooperates to snap-gauge (2) Tangential positioning is carried out, bogusware (3) is that the laying position line (2-1) and die body (1) cooperation in foundation snap-gauge (2) process, false Part positions side (3-1) and die body step (1-2) fitting carries out tangential positioning, snap-gauge (2) and bogusware boss (3- to bogusware (3) 2) cooperation carries out exhibition Xiang Dingwei to bogusware (3) again, and laying positioning side (3-3) of the bogusware (3) after positioning is realized to laying (4) Positioning.
2. blade laying positioning device described in accordance with the claim 1, wherein the spacing of snap-gauge (2) is 200~300mm.
3. blade laying positioning device described in accordance with the claim 1, wherein the spacing of snap-gauge (2) is 200mm.
4. blade laying positioning device described in accordance with the claim 1, wherein the material of snap-gauge (2) is stainless steel plate.
CN201811322704.5A 2018-11-07 2018-11-07 Paddle laying layer positioning device Active CN109532201B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811322704.5A CN109532201B (en) 2018-11-07 2018-11-07 Paddle laying layer positioning device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811322704.5A CN109532201B (en) 2018-11-07 2018-11-07 Paddle laying layer positioning device

Publications (2)

Publication Number Publication Date
CN109532201A true CN109532201A (en) 2019-03-29
CN109532201B CN109532201B (en) 2020-07-31

Family

ID=65845344

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811322704.5A Active CN109532201B (en) 2018-11-07 2018-11-07 Paddle laying layer positioning device

Country Status (1)

Country Link
CN (1) CN109532201B (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3740285A (en) * 1968-03-01 1973-06-19 W Goldsworthy Method and apparatus for filament winding about three axes of a mandrel and products produced thereby
US6117376A (en) * 1996-12-09 2000-09-12 Merkel; Michael Method of making foam-filled composite products
CN103507277A (en) * 2013-10-23 2014-01-15 连云港中复连众复合材料集团有限公司 Improved method for layering of root of blade of wind driven generator
CN104416923A (en) * 2013-08-28 2015-03-18 上海艾郎风电科技发展有限公司 Method for paving fiber clothes
CN108215248A (en) * 2017-12-14 2018-06-29 中航复合材料有限责任公司 A kind of positioning of Varying-thickness precast body and the device and method of Thickness sensitivity
CN108284620A (en) * 2017-11-30 2018-07-17 江西洪都航空工业集团有限责任公司 A kind of composite material multi-wall type co-curing integral panel shaping dies

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3740285A (en) * 1968-03-01 1973-06-19 W Goldsworthy Method and apparatus for filament winding about three axes of a mandrel and products produced thereby
US6117376A (en) * 1996-12-09 2000-09-12 Merkel; Michael Method of making foam-filled composite products
CN104416923A (en) * 2013-08-28 2015-03-18 上海艾郎风电科技发展有限公司 Method for paving fiber clothes
CN103507277A (en) * 2013-10-23 2014-01-15 连云港中复连众复合材料集团有限公司 Improved method for layering of root of blade of wind driven generator
CN108284620A (en) * 2017-11-30 2018-07-17 江西洪都航空工业集团有限责任公司 A kind of composite material multi-wall type co-curing integral panel shaping dies
CN108215248A (en) * 2017-12-14 2018-06-29 中航复合材料有限责任公司 A kind of positioning of Varying-thickness precast body and the device and method of Thickness sensitivity

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