CN201394603Y - Honeycomb material drawing machine - Google Patents
Honeycomb material drawing machine Download PDFInfo
- Publication number
- CN201394603Y CN201394603Y CN2009200571676U CN200920057167U CN201394603Y CN 201394603 Y CN201394603 Y CN 201394603Y CN 2009200571676 U CN2009200571676 U CN 2009200571676U CN 200920057167 U CN200920057167 U CN 200920057167U CN 201394603 Y CN201394603 Y CN 201394603Y
- Authority
- CN
- China
- Prior art keywords
- slide
- pulling claw
- cellular material
- supporting plate
- lamination
- 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.)
- Expired - Lifetime
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Abstract
The utility model discloses a honeycomb material drawing machine, comprising a machine body, a guide rail is arranged on the machine body, a slide is respectively installed at two ends of the guide rail. A motor is respectively arranged at two ends of the machine body, the motor is connected with a reducer. Two silk poles are respectively installed at the two ends of the machine body, a pulley isinstalled at one end of the two silk poles, the pulley is connected with the corresponded reducer through a timing belt. The other ends of the two silk poles are connected with slide threads at the corresponded ends, the slide is provided with a positioning device. A lamination support plate is arranged on the machine body, a drawing process support plate is symmetrically installed at two sides ofthe lamination support plate. The design can realize the drawing of lamination made of honeycomb materials effectively, and provide an equipment which has more perfect and mature technology and is used for drawing and forming process of aviation honeycomb materials.
Description
Technical field
The utility model relates to a kind of stretching-machine, particularly a kind of equipment that is used for air cellular material extending moulding process.
Background technology
Cellular material is widely used at aviation field, yet at present at home and abroad the process equipment that is used for the moulding of air cellular material extending is fewer, and function can not satisfy the more demand of people, and relevant technology prematurity still and perfect.
The utility model content
In order to overcome the deficiencies in the prior art, the utility model provides a kind of cellular material drawing mill that can be used for air cellular material extending moulding process.
The technical scheme that its technical problem that solves the utility model adopts is:
A kind of cellular material drawing mill comprises fuselage, and described fuselage is provided with guide rail, and the two ends of guide rail are separately installed with slide; The two ends of described fuselage are respectively equipped with motor, and motor is connected with reductor; The two ends of described fuselage are separately installed with two screw mandrels, and an end of two screw mandrels is equipped with belt pulley, connect by synchronous belt between belt pulley and the corresponding reductor, and the other end of two screw mandrels and be threaded with the slide of its corresponding end, described slide is provided with positioner; Described fuselage is provided with the lamination supporting plate, and the bilateral symmetry of lamination supporting plate is equipped with the drawing process supporting plate.
As further improvement of the utility model, described positioner comprises pulling claw on the some comb shapes that are movably arranged on slide top and is movably arranged on pulling claw under some comb shapes of slide bottom, on the described comb shape under pulling claw and the comb shape inboard of pulling claw be separately installed with the pulling claw connecting plate, be provided with the gap between described slide and the pulling claw connecting plate.
Further improve as of the present utility model, setting frock supporting plate is installed on the described fuselage.
The beneficial effects of the utility model are: the utility model can utilize the motor-driven reductor to drive synchronous belt, pulley movements, belt pulley moves horizontally on fuselage by screw mandrel drive slide then, and slide is provided with positioner, and this positioner can be promptly to be stretched the cellular material lamination, this moment, the design provided a kind of technology comparatively to improve and the ripe equipment that is used for air cellular material extending moulding process by the stretching that can effectively realize the cellular material lamination that moves horizontally of slide.
Description of drawings
Below in conjunction with drawings and Examples the utility model is further specified.
Fig. 1 is the first visual angle stereogram of the present utility model;
Fig. 2 is the second visual angle stereogram of the present utility model;
Fig. 3 is a upward view of the present utility model.
The specific embodiment
With reference to Fig. 1, Fig. 2, Fig. 3, a kind of cellular material drawing mill comprises fuselage 1, and described fuselage 1 is provided with guide rail 11, and the two ends of guide rail 11 are separately installed with slide 10; The two ends of described fuselage 1 are respectively equipped with motor 3, and motor 3 is connected with reductor 2; The two ends of described fuselage 1 are separately installed with two screw mandrels 5, one end of two screw mandrels 5 is equipped with belt pulley 42, connect by synchronous belt 41 between belt pulley 42 and the corresponding reductor 2, the other end of two screw mandrels 5 and be threaded with the slide 10 of its corresponding end, described slide 10 is provided with positioner; The utility model can utilize motor 3 to drive reductor 2 and drive synchronous belt 41, belt pulley 42 motions, belt pulley 42 moves horizontally on fuselage 1 by screw mandrel 5 drive slides 10 then, and the positioner on the slide 10 can be promptly to be stretched cellular material lamination 13, the move horizontally stretching that can effectively realize cellular material lamination 13 of this moment by slide 10.
Above-mentioned positioner comprises pulling claw 8 on the some comb shapes that are movably arranged on slide 10 tops and is movably arranged on pulling claw 12 under some comb shapes of slide 10 bottoms, on the described comb shape under pulling claw 8 and the comb shape inboard of pulling claw 12 be separately installed with pulling claw connecting plate 9, be provided with gap 18 between described slide 10 and the pulling claw connecting plate 9; Since on the comb shape under pulling claw 8 and the comb shape pulling claw 12 be to be movably arranged on the slide 10, so raise on the comb shape pulling claw 12 under the pulling claw 8 and comb shape during the cellular material that can stretch unclamping; Described fuselage 1 is provided with lamination supporting plate 14, the bilateral symmetry of lamination supporting plate 14 is equipped with drawing process supporting plate 15, setting frock supporting plate 16 is installed on the described fuselage 1, in use, lamination supporting plate 14 is provided with cellular material lamination 13 to be stretched, workpiece 7 is installed on the frock that formalizes the simultaneously supporting plate 16, and workpiece 7 is provided with setting frock 6, and workpiece 7 is provided with some ears 17 that draw; During work, motor 3 drives reductor 2, and drive slides 10 by synchronous belt 41, belt pulley 42, screw mandrel 5 and on fuselage 1, move horizontally, during drawing ear 17, place pin, the other end of this pin places gap 18 interior so that positioner stretching cellular material lamination 13; Utilize the compressed air-driven cylinder to drive positioner work, thereby cellular material lamination 13 is drawn into the honeycomb workpiece; Utilize compressed air-driven cylinder lamination supporting plate 14 to give the cellular material lamination 13 location; Utilize the compressed air-driven cylinder to drive drawing process supporting plate 15 and finish stretch forming with the interlock of slide 10; Utilizing the compressed air-driven cylinder to drive setting frock supporting plate 16 gives the setting frock 6 location; The design provides a kind of technology comparatively to improve and the ripe equipment that is used for air cellular material extending moulding process.
Certainly, the utility model is created and is not limited to above-mentioned embodiment, as long as it reaches technique effect of the present utility model with essentially identical means, all should belong to protection domain of the present utility model.
Claims (3)
1. a cellular material drawing mill comprises fuselage (1), it is characterized in that: described fuselage (1) is provided with guide rail (11), and the two ends of guide rail (11) are separately installed with slide (10); The two ends of described fuselage (1) are respectively equipped with motor (3), and motor (3) is connected with reductor (2); The two ends of described fuselage (1) are separately installed with two screw mandrels (5), one end of two screw mandrels (5) is equipped with belt pulley (42), connect by synchronous belt (41) between belt pulley (42) and the corresponding reductor (2), the other end of two screw mandrels (5) and be threaded with the slide (10) of its corresponding end, described slide (10) is provided with positioner; Described fuselage (1) is provided with lamination supporting plate (14), and the bilateral symmetry of lamination supporting plate (14) is equipped with drawing process supporting plate (15).
2. a kind of cellular material drawing mill according to claim 1, it is characterized in that: described positioner comprises pulling claw (8) on the some comb shapes that are movably arranged on slide (10) top and is movably arranged on pulling claw (12) under some comb shapes of slide (10) bottom, the inboard of pulling claw (12) is separately installed with pulling claw connecting plate (9) under pulling claw on the described comb shape (8) and the comb shape, is provided with gap (18) between described slide (10) and the pulling claw connecting plate (9).
3. a kind of cellular material drawing mill according to claim 1 is characterized in that: setting frock supporting plate (16) is installed on the described fuselage (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009200571676U CN201394603Y (en) | 2009-05-25 | 2009-05-25 | Honeycomb material drawing machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009200571676U CN201394603Y (en) | 2009-05-25 | 2009-05-25 | Honeycomb material drawing machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201394603Y true CN201394603Y (en) | 2010-02-03 |
Family
ID=41617094
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009200571676U Expired - Lifetime CN201394603Y (en) | 2009-05-25 | 2009-05-25 | Honeycomb material drawing machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201394603Y (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101569904B (en) * | 2009-05-25 | 2011-06-22 | 中山市科力高自动化设备有限公司 | Cellular material drawing mill |
| CN103736834A (en) * | 2014-01-10 | 2014-04-23 | 安徽长远绿色能源有限公司 | Device for stretching honeycomb core |
| JP2020015064A (en) * | 2018-07-25 | 2020-01-30 | 昭和飛行機工業株式会社 | Method for production of honeycomb core |
| CN110843225A (en) * | 2019-11-19 | 2020-02-28 | 胡国文 | Low-density honeycomb plate sandwich manufacturing, stretching and forming equipment and forming method |
-
2009
- 2009-05-25 CN CN2009200571676U patent/CN201394603Y/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101569904B (en) * | 2009-05-25 | 2011-06-22 | 中山市科力高自动化设备有限公司 | Cellular material drawing mill |
| CN103736834A (en) * | 2014-01-10 | 2014-04-23 | 安徽长远绿色能源有限公司 | Device for stretching honeycomb core |
| JP2020015064A (en) * | 2018-07-25 | 2020-01-30 | 昭和飛行機工業株式会社 | Method for production of honeycomb core |
| CN110843225A (en) * | 2019-11-19 | 2020-02-28 | 胡国文 | Low-density honeycomb plate sandwich manufacturing, stretching and forming equipment and forming method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: YICHANG HEDALI COMPOUND MATERIALS CO., LTD. Free format text: FORMER OWNER: ZHONGSHAN CLG AUTOMATION EQUIPMENT CO.LTD. Effective date: 20100702 Free format text: FORMER OWNER: LI YONG |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| COR | Change of bibliographic data |
Free format text: CORRECT: ADDRESS; FROM: 528400 SHENBAO ELECTRIAL APPARATUS PARK, GUANGFENG INDUSTRIAL PARK, SHALANG TOWN, WEST AREA, ZHONGSHAN CITY, GUANGDONG PROVINCE TO: 443006 LIJIAHE ROAD, JIANGNAN STREET, DIANJUN DISTRICT, YICHANG CITY |
|
| TR01 | Transfer of patent right |
Effective date of registration: 20100702 Address after: 443006 Li River Road, Jiangnan Road, Yichang Point Military Area Command Patentee after: Yichang Hedali Composite Materials Co., Ltd. Address before: 528400 Guangdong city of Zhongshan province Guangfeng Industrial Park West sirlon Shenbao electric appliance Park Co-patentee before: Li Yong Patentee before: Zhongshan Keligao Automation Equipment Co., Ltd. |
|
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20100203 |