CN105538553A - Die disassembly and assembly device and method for composite material cabin-type part - Google Patents
Die disassembly and assembly device and method for composite material cabin-type part Download PDFInfo
- Publication number
- CN105538553A CN105538553A CN201510918140.1A CN201510918140A CN105538553A CN 105538553 A CN105538553 A CN 105538553A CN 201510918140 A CN201510918140 A CN 201510918140A CN 105538553 A CN105538553 A CN 105538553A
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- China
- Prior art keywords
- patrix
- counterdie
- class part
- mobile liftable
- liftable mechanism
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- 239000002131 composite material Substances 0.000 title claims abstract description 38
- 238000000034 method Methods 0.000 title claims abstract description 16
- 230000007246 mechanism Effects 0.000 claims description 39
- 238000007514 turning Methods 0.000 claims description 24
- 239000000853 adhesive Substances 0.000 claims description 2
- 230000001070 adhesive effect Effects 0.000 claims description 2
- 238000003754 machining Methods 0.000 claims description 2
- 238000007493 shaping process Methods 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 15
- 238000005516 engineering process Methods 0.000 abstract description 3
- 230000007306 turnover Effects 0.000 description 5
- 235000004443 Ricinus communis Nutrition 0.000 description 2
- 230000001154 acute effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000003028 elevating effect Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/20—Opening, closing or clamping
- B29C33/26—Opening, closing or clamping by pivotal movement
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Mounting, Exchange, And Manufacturing Of Dies (AREA)
- Automobile Manufacture Line, Endless Track Vehicle, Trailer (AREA)
Abstract
The invention belongs to tool design technologies and relates to a die disassembly and assembly device and method for a composite material cabin-type part. When the composite material cabin-type part of an aircraft is manufactured and assembled, the composite material cabin-type part is divided into an upper half cabin body and a lower half cabin body to be subjected to composite material placement curing forming. The upper half cabin body, the lower half cabin body and components of the two half cabin bodies need to be overturned and then assembled and glued after split work, and reliable positioning and overturning die disassembly and assembly are required to be achieved. But no reliable overturning die disassembly and assembly methods and devices exist until now. The special overturning die disassembly and assembly device used for the composite material cabin-type part is developed, and convenient and effective working ways are provided for lot production and manufacturing of the composite material cabin-type part. According to the die disassembly and assembly device and method for the composite material cabin-type part, an overturning tool is simple in structure, convenient to operate, reliable in overturning, accurate in positioning and capable of meeting the requirement of overturning die disassembly and assembly of the cabin-type composite material part, and the manufacturing efficiency of the composite material cabin-type part can be better improved.
Description
Technical field
The invention belongs to Fixture Design technology, relate to the invention to a kind of Composite Cabin class part folding mould device and method.
Background technology
During the class part manufacture assembling of technique for aircraft composite cabin, upper and lower two and half cabin bodies are divided into carry out composite plys curing molding respectively, assembling after upper and lower two and half cabin bodies and fitting turnover thereof is needed to glued joint after dividing body running, require to realize reliably locating and rotating matched moulds, up to the present do not rotate closing method and device reliably.Develop and a kind ofly rotate matched moulds special purpose device for Composite Cabin class part, criticize the manufacturing for Composite Cabin class part and to provide convenience effective Working Means.
Summary of the invention
Technical problem to be solved by this invention is: provide a kind of Composite Cabin class part folding mould device and method, this upset tool structure is simple, easy to operate, upset reliable, accurate positioning and can meet cabin class composite material parts and rotate matched moulds requirement, is beneficial to improve Composite Cabin class part and manufacture efficiency.
Technical scheme of the present invention is: a kind of Composite Cabin class part folding mould device, for the formed machining of cabin class part, this device comprises main body rack, decelerator, patrix mobile liftable mechanism, patrix, hydraulic push rod, counterdie mobile liftable mechanism, counterdie, turning arm and the plate that is located by connecting, wherein
Described main body rack is the under(-)chassis be arranged in parallel, and comprises the position limiting structure of horizontally set;
Described patrix mobile liftable mechanism and counterdie mobile liftable mechanism comprise bottom roller respectively, and can push from two of a described main body rack porch;
Form switching mechanism by described decelerator, symmetrically arranged hydraulic push rod, turning arm and the plate that is located by connecting, one end of hydraulic push rod is hinged on main body rack porch, and the upside of the other end and turning arm is hinged; The downside end of turning arm is hinged near the position limiting structure of main body rack, upper side end is connected by the rotating shaft of bearing with the plate that is located by connecting, this plate that is located by connecting is connected with patrix by alignment pin, and decelerator is arranged on the upper end of turning arm, and the plate that is located by connecting described in can driving rotates;
Described patrix is placed in patrix mobile liftable mechanism, and described counterdie is placed in counterdie mobile liftable mechanism.
Also comprise the electric hydraulic station be connected with the oil inlet and outlet of hydraulic push rod.
Patrix mobile liftable mechanism also comprises lifting handwheel, be used for adjustment level and height.
Described main body rack also comprises guide rail.
Counterdie mobile liftable mechanism also comprises adjustable supporter.
Worm reduction gear is linked together by output shaft, self-aligning bearing, supporting revolving shaft and the plate that is located by connecting by decelerator.
Described patrix mobile liftable mechanism also comprises the jack of location.
Utilize said apparatus to carry out a method for Composite Cabin class part folding mould, it is characterized in that: the method comprises following step:
Step one, enter and adjust location
Bonding first half cabin class part in the patrix of patrix mobile liftable mechanism, bonding Lower Half cabin class part in the counterdie of counterdie mobile liftable mechanism, push patrix mobile liftable mechanism and counterdie mobile liftable mechanism in two side entrances of main body rack respectively and adjust level, the height of adjustment patrix mobile liftable mechanism, to contour with the both sides plate that is located by connecting, connects be located by connecting plate and patrix;
Step 2, lifting patrix
The height that driving hydraulic push rod makes turning arm rotation can overturn around the rotating shaft of the plate that is located by connecting to part;
Step 3, patrix overturn
Drive decelerator progressively to overturn patrix, promote turning arm simultaneously and continue to rotate, until patrix can dock with counterdie;
Step 4, matched moulds are shaping
After patrix and counterdie being bolted, adhesive curing is carried out to Composite Cabin class part;
Step 5, die sinking
Open the bolt between patrix and counterdie, regain turning arm (7) thus patrix and counterdie are separated.
The invention has the beneficial effects as follows: this apparatus structure is simple, easy to operate, and safe and reliable efficiency is high.
Accompanying drawing explanation
Fig. 1 is the side shaft side figure of Composite Cabin class part folding mould device of the present invention;
Fig. 2 is the opposite side shaft side figure of Composite Cabin class part folding mould device of the present invention;
Fig. 3 is that Composite Cabin class part folding mould device of the present invention rotates matched moulds schematic diagram;
Fig. 4 is that Composite Cabin class part completes schematic diagram.
Detailed description of the invention
Below the present invention is described in further details.See Fig. 1, Fig. 2, Fig. 3, the present invention includes and design and manufacture 1 main body rack, design and select 2 decelerators, design and manufacture 3 patrix mobile liftable mechanisms, design and select 4 hydraulic push rods, design and manufacture 5 counterdie mobile liftable mechanisms, design and manufacture 6 electric hydraulic stations, design and manufacture 7 turning arms, design and manufacture 8 and to be located by connecting plate, design and manufacture 9 lifting handwheels, design and manufacture 10 guide rails, design and manufacture 11 adjustable supporter compositions.Wherein switching mechanism comprises 2 decelerators, 4 hydraulic push rods, 7 turning arms, 8 plate that is located by connecting is connected by revolute pair with output shaft, supporting revolving shaft, regulating center bearing base, and 6 electric hydraulic stations are connected with the oil inlet and outlet of 4 hydraulic push rods by 4 oil pipes.
Described main body rack 1 comprises main connection bracket, both sides auxiliary stand, is connected to one after adopting steel pipe and Plate Welding with bolt; Described decelerator 2 is linked together by output shaft, self-aligning bearing, supporting revolving shaft and 8 plate that is located by connecting by worm reduction gear, and self-aligning bearing compensates the concentricity of two ends positioning and clamping mechanism when rotating, and transmits outputting power by flat key; Described patrix mobile liftable mechanism 3 ensures the part initial position before beginning turning by castor, under(-)chassis, adjustable supports and jack, Moving caster adjustment X-axis horizontal level, lifting handwheel adjustment adjustable supports Y-axis upright position, jack is fixed spacing; Described hydraulic push rod 4, turning arm 7, the plate 8 that is located by connecting are connected by shaft seating with main body rack 1, and turning arm 7 rotates around main shaft, composition upset linkage; Described counterdie mobile liftable mechanism 5 ensures the fitting turnover end position before beginning turning by castor, under(-)chassis, adjustable supporter; Described electric hydraulic station 6 comprises electrical control cabinet and hydraulic power unit, is connected with hydraulic push rod 4 by oil pipe, and hydraulic control push rod 4 is retreated, and realizes the upset of Composite Cabin class part.
Present invention also offers a kind of Composite Cabin class fitting turnover folding modeling method, comprise following step:
Step one, enter fast, adjust location, its program is: by 3 patrix mobile elevating machines by first half cabin class part place and along X-axis 10 guide rail guiding enter on the left of 1 main body rack, adjustment 9 lifting handwheel makes planar horizontal on part, simultaneous altitude and both sides 8 plate that is located by connecting is contour, and the 8 both sides plate that is located by connecting is fixed fast along Y-axis locating clip gripping members.
Step 2, turn clockwise α angle to part around main shaft can rotation location, its program is: beginning first half cabin class fitting turnover, 6 electric hydraulic stations provide hydraulic system power, 4 hydraulic push rods extend, pull switching mechanism part, rotate hinge around main shaft place and rotate rising α angle, it is suitable for countershaft position of rotation that first half cabin class part arrives, turning arm and horizontal plane angle (acute angle) when θ initial angle is initial.
Step 3, around countershaft, (runing rest axis of rotation θ initial angle+θ terminates angle, angle to be made part flats down, its program is: drive deceleration device by the motor (or manual) of 2 decelerators, drives top rotating mechanism to rotate θ initial angle+θ by rotating shaft around countershaft place regulating center bearing base and terminates angle, angle.θ terminates angle for turning arm and horizontal plane angle (acute angle) at the end of upset
Step 4, around main shaft turn clockwise β angle to upset end position make part flats down matched moulds, namely suppressed by 6 electric hydraulic stations, when 4 hydraulic push rods extend and reach the longest position that β angle requires, first half cabin class part horizontal plane, is elevated 11 adjustable supporter adjustment opposite side 5 counterdie mobile liftable mechanisms, by the class part horizontal plane leveling of Lower Half cabin down, touch first half cabin class part horizontal plane and complete turnover mould-matching process, complete location matched moulds assembling.β angle=180 °-θ terminates angle-θ initial angle+α).
Step 5, exits after work fast, and its program is: the gluing work of Composite Cabin class part is complete, and unclamp 8 and to be located by connecting plate place locating clip gripping members, matched moulds rear deck class part exits along X-axis guide rail, and matched moulds body opening process in contrast.
Claims (8)
1. a Composite Cabin class part folding mould device, for the formed machining of cabin class part, it is characterized in that: this device comprises main body rack (1), decelerator (2), patrix mobile liftable mechanism (3), patrix, hydraulic push rod (4), counterdie mobile liftable mechanism (5), counterdie, turning arm (7) and the plate that is located by connecting (8), wherein
Described main body rack (1) under(-)chassis for be arrangeding in parallel, and comprise the position limiting structure of horizontally set;
Described patrix mobile liftable mechanism (3) and counterdie mobile liftable mechanism (5) comprise bottom roller respectively, and can push from two porch of described main body rack (1);
Switching mechanism is formed by described decelerator (2), symmetrically arranged hydraulic push rod (4), turning arm (7) and the plate that is located by connecting (8), one end of hydraulic push rod (4) is hinged on main body rack (1) porch, and the upside of the other end and turning arm (7) is hinged; The downside end of turning arm (7) is hinged near the position limiting structure of main body rack (1), upper side end is connected by the rotating shaft of bearing with the plate that is located by connecting (8), this plate that is located by connecting (8) is connected with patrix by alignment pin, decelerator (2) is arranged on the upper end of turning arm (7), and the plate (8) that is located by connecting described in can driving rotates;
Described patrix is placed in patrix mobile liftable mechanism (3), and described counterdie is placed in counterdie mobile liftable mechanism (5).
2. Composite Cabin class part folding mould device according to claim 1, is characterized in that: also comprise the electric hydraulic station (6) be connected with the oil inlet and outlet of hydraulic push rod (4).
3. Composite Cabin class part folding mould device according to claim 1, is characterized in that: patrix mobile liftable mechanism (3) also comprise lifting handwheel (9), be used for adjustment level and height.
4. the Composite Cabin class part folding mould device according to any one of claim 1-3, is characterized in that: described main body rack (1) also comprises guide rail (10).
5. the Composite Cabin class part folding mould device according to any one of claim 1-3, is characterized in that: counterdie mobile liftable mechanism (5) also comprises adjustable supporter (11).
6. the Composite Cabin class part folding mould device according to any one of claim 1-3, is characterized in that: worm reduction gear is linked together by output shaft, self-aligning bearing, supporting revolving shaft and the plate that is located by connecting (8) by decelerator (2).
7. the Composite Cabin class part folding mould device according to any one of claim 1-3, is characterized in that: described patrix mobile liftable mechanism (3) also comprises the jack of location.
8. utilize device described in claim 1-7 to carry out a method for Composite Cabin class part folding mould, it is characterized in that: the method comprises following step:
Step one, enter and adjust location
Bonding first half cabin class part in the patrix of patrix mobile liftable mechanism (3), bonding Lower Half cabin class part in the counterdie of counterdie mobile liftable mechanism (5), push patrix mobile liftable mechanism (3) and counterdie mobile liftable mechanism (5) in two side entrances of main body rack (1) respectively and adjust level, the height of adjustment patrix mobile liftable mechanism (3), to contour with the both sides plate (8) that is located by connecting, connects be located by connecting plate (8) and patrix;
Step 2, lifting patrix
The height that driving hydraulic push rod (4) makes turning arm (7) rotation can overturn around the rotating shaft of the plate that is located by connecting (8) to part;
Step 3, patrix overturn
Drive decelerator (2) progressively to overturn patrix, promote turning arm (7) simultaneously and continue to rotate, until patrix can dock with counterdie;
Step 4, matched moulds are shaping
After patrix and counterdie being bolted, adhesive curing is carried out to Composite Cabin class part;
Step 5, die sinking
Open the bolt between patrix and counterdie, regain turning arm (7) thus patrix and counterdie are separated.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510918140.1A CN105538553B (en) | 2015-12-11 | 2015-12-11 | A kind of Composite Cabin class part folding mould device and method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510918140.1A CN105538553B (en) | 2015-12-11 | 2015-12-11 | A kind of Composite Cabin class part folding mould device and method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105538553A true CN105538553A (en) | 2016-05-04 |
| CN105538553B CN105538553B (en) | 2017-10-13 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510918140.1A Active CN105538553B (en) | 2015-12-11 | 2015-12-11 | A kind of Composite Cabin class part folding mould device and method |
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| Country | Link |
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| CN (1) | CN105538553B (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107791496A (en) * | 2017-11-20 | 2018-03-13 | 常州市新创智能科技有限公司 | A kind of sliding turnover mechanism of stringer production equipment |
| CN109277226A (en) * | 2017-07-20 | 2019-01-29 | 上海交通大学 | Flexible positioning and attitude adjustment device and method for spraying thin-walled parts |
| CN112743868A (en) * | 2020-12-15 | 2021-05-04 | 西安飞机工业(集团)有限责任公司 | Overturning mold closing device and using method |
| CN112847741A (en) * | 2021-01-08 | 2021-05-28 | 南京理工大学 | Overturning die and method for preparing inorganic composite material section |
| CN113263751A (en) * | 2021-05-29 | 2021-08-17 | 航天海鹰(镇江)特种材料有限公司 | Mold overturning device for manufacturing composite material and using method thereof |
| EP4326518A4 (en) * | 2022-07-15 | 2024-06-12 | Gurit Tooling (Taicang) Co., Ltd. | WIND TURBINE BLADE MOLD STRUCTURE |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101304858A (en) * | 2005-11-08 | 2008-11-12 | Lm玻璃纤维制品有限公司 | Mould assembly with hinge mechanism and method for closing mould assembly |
| WO2010028613A1 (en) * | 2008-09-10 | 2010-03-18 | Aerodyn Enigineering Gmbh | Molding tool for rotor blades of a wind power plant |
-
2015
- 2015-12-11 CN CN201510918140.1A patent/CN105538553B/en active Active
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101304858A (en) * | 2005-11-08 | 2008-11-12 | Lm玻璃纤维制品有限公司 | Mould assembly with hinge mechanism and method for closing mould assembly |
| WO2010028613A1 (en) * | 2008-09-10 | 2010-03-18 | Aerodyn Enigineering Gmbh | Molding tool for rotor blades of a wind power plant |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109277226A (en) * | 2017-07-20 | 2019-01-29 | 上海交通大学 | Flexible positioning and attitude adjustment device and method for spraying thin-walled parts |
| CN107791496A (en) * | 2017-11-20 | 2018-03-13 | 常州市新创智能科技有限公司 | A kind of sliding turnover mechanism of stringer production equipment |
| CN112743868A (en) * | 2020-12-15 | 2021-05-04 | 西安飞机工业(集团)有限责任公司 | Overturning mold closing device and using method |
| CN112847741A (en) * | 2021-01-08 | 2021-05-28 | 南京理工大学 | Overturning die and method for preparing inorganic composite material section |
| CN112847741B (en) * | 2021-01-08 | 2022-08-09 | 南京理工大学 | Overturning die and method for preparing inorganic composite material section |
| CN113263751A (en) * | 2021-05-29 | 2021-08-17 | 航天海鹰(镇江)特种材料有限公司 | Mold overturning device for manufacturing composite material and using method thereof |
| EP4326518A4 (en) * | 2022-07-15 | 2024-06-12 | Gurit Tooling (Taicang) Co., Ltd. | WIND TURBINE BLADE MOLD STRUCTURE |
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| Publication number | Publication date |
|---|---|
| CN105538553B (en) | 2017-10-13 |
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