CN209937447U - Forming die for aircraft ventilation pipe - Google Patents

Forming die for aircraft ventilation pipe Download PDF

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Publication number
CN209937447U
CN209937447U CN201920793042.3U CN201920793042U CN209937447U CN 209937447 U CN209937447 U CN 209937447U CN 201920793042 U CN201920793042 U CN 201920793042U CN 209937447 U CN209937447 U CN 209937447U
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CN
China
Prior art keywords
module
ring
fixed
closed ring
groove
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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 - Fee Related
Application number
CN201920793042.3U
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Chinese (zh)
Inventor
孙建毅
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.)
Guizhou Anshun Longfei Auto Parts Co Ltd
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Guizhou Anshun Longfei Auto Parts Co Ltd
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Priority to CN201920793042.3U priority Critical patent/CN209937447U/en
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Publication of CN209937447U publication Critical patent/CN209937447U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses an aircraft ventilation pipe forming die, the on-line screen storage device comprises a base, fixation clamp of the anterior upper end fixedly connected with of base, solid fixed ring of upper portion front end fixedly connected with of base, gu the fixed ring front end is provided with a fixed arm, gu be provided with a moulding device between fixed ring and the fixed arm, the both ends of moulding device all are provided with a closed ring, be provided with a locking lid in the closed ring. An aircraft ventilation pipe forming die, through set up fixation clamp, solid fixed ring and fixed arm on the base, can effectively fix moulding device, through set up closed ring and locking lid and through threaded connection at moulding device both ends, can be fast and effectual moulding the material, through set up draw-in groove and buckle in last module and lower module both sides, and including the module both ends set up a connecting strip, improved in the past through the fixed loaded down with trivial details procedure of nut, improved work efficiency.

Description

Forming die for aircraft ventilation pipe
Technical Field
The utility model relates to a mould field, in particular to aircraft ventilation pipe forming die.
Background
The forming die of the airplane vent pipe is a die manufactured according to the shape and the structure of a real object in proportion, a pressing or pouring method is used for enabling materials to be tools with certain shapes, different plastic forming methods require forming dies with different principles and structural characteristics, the forming dies mainly comprise an injection forming die, an extrusion forming die, a blow molding die of a hollow product, a vacuum or compressed air forming die, a press forming die and a die-casting forming die, although the existing forming die of the airplane vent pipe has high precision, the procedure is complex during the use, nuts need to be repeatedly tightened or finely adjusted, the work efficiency is reduced, and the abrasion of the die is accelerated.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a main aim at provides an aircraft ventilation pipe forming die can effectively solve the problem in the background art.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an aircraft ventilation pipe forming die, includes the base, a fixation clamp of base front portion upper end fixedly connected with, solid fixed ring of upper portion front end fixedly connected with of base, gu the fixed ring front end is provided with a fixed arm, gu be provided with a moulding device between fixed ring and the fixed arm, the both ends of moulding device all are provided with a closed ring, be provided with a locking lid in the closed ring.
Preferably, the lower extreme of locking lid opens there is a bar groove, the outside surface of locking lid is opened has a spacing groove, be provided with a spacing ring on the inner wall of closed ring the spacing ring is structure as an organic whole with the closed ring, be carved with the screw thread on the lower part outer wall of closed ring, the closed ring is covered through spacing ring and spacing groove movable mounting locking.
Preferably, moulding device includes module, lower module and interior module, it has a U type groove to go up the module and respectively open at the both ends of module down, be carved with the screw thread on the U type inslot wall, it has a fixed slot to go up respectively to open on the both ends inner wall of module and lower module, the both ends surface of interior module respectively is equipped with a connecting strip, the connecting strip passes through screwed connection with interior module and is in the same place, the lower extreme of connecting strip is located the fixed slot at module both ends and is in the same place interior module and last module swing joint in the fixed slot at module both ends, and the upper end of connecting strip is located module both ends down and is in the same place interior module and lower module swing joint in the fixed slot.
Preferably, the both ends left and right sides of going up the module respectively is provided with a fixed block, a fixed block and last module structure as an organic whole, the middle part of a fixed block is provided with a draw-in groove that link up from top to bottom, the both ends left and right sides of module respectively is provided with a fixed block No. two down, No. two fixed blocks and module structure as an organic whole down, No. two buckle of fixed block upper end fixedly connected with, the buckle passes the draw-in groove and will go up module and module fixed mounting down and be in the same place.
Preferably, the connecting strip is located in a strip-shaped groove, and the lower part of the closed ring is located in a U-shaped groove at two ends of the upper module and the lower module, and the closed ring is installed at two ends of the shaping device through threads.
Preferably, the left part of solid fixed ring is provided with a loose axle, the loose axle will be fixed the ring and the left part swing joint of fixed arm together, the right part of fixed arm is provided with a lock nut, lock nut alternates to be connected on solid fixed ring and link together the right part of solid fixed ring and fixed arm, the upper portion of moulding device is arranged in solid fixed ring and fixed arm and the lower part is arranged in the fixation clamp and with moulding device movable mounting on the base.
Compared with the prior art, the utility model discloses following beneficial effect has:
the utility model discloses in, through set up the fixation clamp on the base, gu fixed ring and fixed arm, can strengthen the steadiness during operation, improve the off-the-shelf precision, through set up the fixed slot at last module and lower module both ends, also can be firm when realizing easy operation fix the interior module at last module under with on the module, set up draw-in groove and buckle through the left and right sides at last module and lower module both ends, alternate through buckle and draw-in groove and connect, realize installing and dismantling moulding device fast simple and convenient during the use, the work efficiency is improved, through setting up closed ring and locking lid at moulding device both ends, can effectively protect the material of pouring into during the use, moulding.
Drawings
Fig. 1 is a front view of an aircraft ventilation pipe forming mold of the present invention;
fig. 2 is a schematic diagram of the internal structures of an upper module and a lower module of the aircraft ventilation pipe forming mold of the present invention;
fig. 3 is a schematic structural view of a closing ring and a locking cover of the aircraft ventilation pipe forming mold according to the present invention;
fig. 4 is the utility model relates to an overall structure schematic diagram of module in aircraft ventilation pipe forming die.
In the figure: 1. a base; 2. a fixing clip; 3. a fixing ring; 4. a fixed arm; 5. a lower module; 6. an upper module; 7. a second fixed block; 8. a closed ring; 9. a locking cover; 10. a movable shaft; 11. a first fixed block; 12. a card slot; 13. buckling; 14. a U-shaped groove; 15. fixing grooves; 16. a limiting groove; 17. a strip-shaped groove; 18. a limiting ring; 19. an inner module; 20. a connecting strip; 21. a locking nut; 22. and (5) a shaping device.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
As shown in fig. 1-4, an aircraft ventilation elbow forming die comprises a base 1, a fixing clamp 2 is fixedly connected to the upper end of the front portion of the base 1, a fixing ring 3 is fixedly connected to the front end of the upper portion of the base 1, a fixing arm 4 is arranged at the front end of the fixing ring 3, a shaping device 22 is arranged between the fixing ring 3 and the fixing arm 4, a closed ring 8 is arranged at each of two ends of the shaping device 22, and a locking cover 9 is arranged in the closed ring 8.
The lower end of the locking cover 9 is provided with a strip-shaped groove 17, the outer side surface of the locking cover 9 is provided with a limit groove 16, the inner wall of the closed ring 8 is provided with a limit ring 18, the limit ring 18 and the closed ring 8 are integrated, the outer wall of the lower part of the closed ring 8 is carved with threads, and the closed ring 8 is movably arranged on the locking cover 9 through the limit ring 18 and the limit groove 16; the shaping device 22 comprises an upper module 6, a lower module 5 and an inner module 19, wherein two ends of the upper module 6 and the lower module 5 are respectively provided with a U-shaped groove 14, threads are carved on the inner wall of the U-shaped groove 14, two end inner walls of the upper module 6 and the lower module 5 are respectively provided with a fixing groove 15, two end surfaces of the inner module 19 are respectively provided with a connecting strip 20, the connecting strips 20 and the inner module 19 are connected together through screws, the lower ends of the connecting strips 20 are positioned in the fixing grooves 15 at the two ends of the upper module 6 to movably connect the inner module 19 and the upper module 6 together, and the upper ends of the connecting strips 20 are positioned in the fixing grooves 15 at the two ends of the lower module 5 to movably connect the inner module 19 and the lower module 5; the left and right sides of the two ends of the upper module 6 are respectively provided with a first fixing block 11, the first fixing block 11 and the upper module 6 are of an integral structure, the middle part of the first fixing block 11 is provided with a clamping groove 12 which is communicated up and down, the left and right sides of the two ends of the lower module 5 are respectively provided with a second fixing block 7, the second fixing block 7 and the lower module 5 are of an integral structure, the upper end of the second fixing block 7 is fixedly connected with a buckle 13, and the buckle 13 penetrates through the clamping groove 12 to fixedly install the upper module 6 and the lower module 5 together; the connecting strip 20 is positioned in the strip-shaped groove 17, and the lower part of the closed ring 8 is positioned in the U-shaped groove 14 at the two ends of the upper module 6 and the lower module 5 to install the closed ring 8 at the two ends of the shaping device 22 through threads; the left part of solid fixed ring 3 is provided with a loose axle 10, loose axle 10 will be fixed ring 3 and fixed arm 4's left part swing joint together, the right part of fixed arm 4 is provided with a lock nut 21, lock nut 21 alternates to be connected on solid fixed ring 3 and link together solid fixed ring 3 and fixed arm 4's right part, moulding device 22's upper portion is arranged in solid fixed ring 3 and fixed arm 4 and the lower part is arranged in fixation clamp 2 and with moulding device 22 movable mounting on base 1.
It should be noted that, the utility model relates to an aircraft ventilation pipe forming die, through set up solid fixed ring 3, fixed arm 4 and fixation clamp 2 on base 1, during the use, can place the lower part of moulding device 22 in fixation clamp 2 and the upper portion place with between solid fixed ring 3 and the fixed arm 4, play the fixed action, simultaneously with rotatory tightening of lock nut 21, realize the fixed action to moulding device 22, through respectively set up a closed ring 8 and locking lid 9 and pass through screw thread swivelling joint with moulding device 22 at the both ends of moulding device 22, when using, revolve the closed ring 8 and revolve and screw down, inject moulding material into, through the screw thread revolve closed ring 8 and screw down, connecting strip 20 at the both ends of inner mould 19 is located in bar groove 17 simultaneously, can effectively carry out the moulding while closing to the inner material, after finishing the moulding, open fixed arm 4 through revolving lock nut 21, take off moulding device 22, open the closed ring 8 at both ends, through pressing buckle 13, open upper module 6 and lower module 5, just can take out the finished product after taking off connecting strip 20 through rotatory screw simultaneously, realize the effect of quick simple dismantlement.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (6)

1. An aircraft ventilation pipe forming die which characterized in that: including base (1), base (1) anterior upper end fixedly connected with fixation clamp (2), the upper portion front end fixedly connected with of base (1) is solid fixed ring (3), gu fixed ring (3) front end is provided with one fixed arm (4), gu be provided with one moulding device (22) between fixed ring (3) and fixed arm (4), the both ends of moulding device (22) all are provided with one closed ring (8), be provided with one locking lid (9) in closed ring (8).
2. An aircraft vent forming mold as defined in claim 1, wherein: the lower extreme of locking lid (9) is opened there is a bar groove (17), the outside surface of locking lid (9) is opened has a spacing groove (16), be provided with a spacing ring (18) on the inner wall of closed ring (8) spacing ring (18) and closed ring (8) structure as an organic whole, be carved with the screw thread on the lower part outer wall of closed ring (8), closed ring (8) are through spacing ring (18) and spacing groove (16) movable mounting on locking lid (9).
3. An aircraft vent forming mold as defined in claim 1, wherein: the shaping device (22) comprises an upper module (6), a lower module (5) and an inner module (19), two ends of the upper module (6) and the lower module (5) are respectively provided with a U-shaped groove (14), the inner wall of the U-shaped groove (14) is carved with screw threads, the inner walls of the two ends of the upper module (6) and the lower module (5) are respectively provided with a fixed groove (15), the two end surfaces of the inner module (19) are respectively provided with a connecting strip (20), the connecting strip (20) is connected with the inner module (19) through screws, the lower ends of the connecting strips (20) are positioned in the fixing grooves (15) at the two ends of the upper module (6) to movably connect the inner module (19) and the upper module (6) together, and the upper ends of the connecting strips (20) are positioned in the fixing grooves (15) at the two ends of the lower module (5) to movably connect the inner module (19) and the lower module (5) together.
4. An aircraft vent forming mold as defined in claim 3, wherein: go up the both ends left and right sides of module (6) and respectively be provided with fixed block (11) No. one, fixed block (11) and last module (6) structure as an organic whole, the middle part of fixed block (11) is provided with draw-in groove (12) that link up from top to bottom, the both ends left and right sides of module (5) respectively is provided with fixed block (7) No. two down, No. two fixed block (7) and module (5) structure as an organic whole down, No. two fixed block (7) upper end fixedly connected with buckle (13), buckle (13) pass draw-in groove (12) will go up module (6) and module (5) fixed mounting down and be in the same place.
5. An aircraft vent forming mold as defined in claim 3, wherein: the connecting strip (20) is positioned in the strip-shaped groove (17), and the lower part of the closed ring (8) is positioned in the U-shaped grooves (14) at the two ends of the upper module (6) and the lower module (5) and is used for installing the closed ring (8) at the two ends of the shaping device (22) through threads.
6. An aircraft vent forming mold as defined in claim 1, wherein: the left part of solid fixed ring (3) is provided with a loose axle (10), loose axle (10) will be fixed the left part swing joint of solid fixed ring (3) and fixed arm (4) together, the right part of fixed arm (4) is provided with a lock nut (21), lock nut (21) alternate the connection on solid fixed ring (3) with the right part of solid fixed ring (3) and fixed arm (4) link together, the upper portion of moulding device (22) is arranged in solid fixed ring (3) and fixed arm (4) and the lower part is arranged in fixation clamp (2) and with moulding device (22) movable mounting on base (1).
CN201920793042.3U 2019-05-29 2019-05-29 Forming die for aircraft ventilation pipe Expired - Fee Related CN209937447U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920793042.3U CN209937447U (en) 2019-05-29 2019-05-29 Forming die for aircraft ventilation pipe

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920793042.3U CN209937447U (en) 2019-05-29 2019-05-29 Forming die for aircraft ventilation pipe

Publications (1)

Publication Number Publication Date
CN209937447U true CN209937447U (en) 2020-01-14

Family

ID=69134608

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920793042.3U Expired - Fee Related CN209937447U (en) 2019-05-29 2019-05-29 Forming die for aircraft ventilation pipe

Country Status (1)

Country Link
CN (1) CN209937447U (en)

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Granted publication date: 20200114