CN217604526U - Processing equipment for producing aviation composite material component - Google Patents

Processing equipment for producing aviation composite material component Download PDF

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Publication number
CN217604526U
CN217604526U CN202220917984.XU CN202220917984U CN217604526U CN 217604526 U CN217604526 U CN 217604526U CN 202220917984 U CN202220917984 U CN 202220917984U CN 217604526 U CN217604526 U CN 217604526U
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CN
China
Prior art keywords
drying space
sliding
production
air guide
frame body
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CN202220917984.XU
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Chinese (zh)
Inventor
宋文娟
宋丹
徐冬梅
刘亭宇
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Jiangsu Hengmingda Aviation Equipment Co ltd
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Jiangsu Hengmingda Aviation Equipment Co ltd
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Priority to CN202220917984.XU priority Critical patent/CN217604526U/en
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Abstract

The utility model discloses a processing device for producing aviation composite materials, which comprises a drying space; the top of the drying space is detachably provided with a heating device; the bottom of the drying space is provided with an air guide structure; the drying space is communicated with the outside through an air guide structure and a heating device respectively; a support frame body is arranged in the bottom of the drying space; a sliding structure is arranged between the top of the drying space and the support frame body; a metal piece is placed on the support frame body; the sliding structure slides up and down in the drying space, and the air flow in the drying space blows over the metal piece. The utility model provides a processing equipment for production of aviation combined material subassembly can carry out quick stoving by effectual to the metalwork that needs the stoving during production for production efficiency.

Description

Processing equipment for producing aviation composite material component
Technical Field
The utility model relates to an aviation combined material subassembly production field.
Background
The production requirement of an aviation composite material assembly is high, some metal pieces need to be cleaned up during production and need to be dried, the metal pieces need to be dried for 1-1.5 hours at 55-65 ℃ during drying, then the metal pieces are kept still under the environment with required humidity and temperature, and after the static time is reached, film laying treatment is carried out; and the film sticking needs to be completed within required time, so that when the composite material component is produced, the metal part needs to be effectively and quickly dried, so that the film sticking treatment is facilitated, and the component meeting the requirements is produced.
Disclosure of Invention
The purpose of the invention is as follows: in order to overcome the not enough that exists among the prior art, the utility model provides a processing equipment for production of aviation combined material subassembly can carry out quick stoving by effectual metalwork that needs to dry during production for production efficiency.
The technical scheme is as follows: in order to achieve the above purpose, the technical scheme of the utility model is as follows:
a processing apparatus for aerospace composite production, comprising a drying space; the top of the drying space is detachably provided with a heating device; the bottom of the drying space is provided with an air guide structure; the drying space is communicated with the outside through an air guide structure and a heating device respectively; a support frame body is arranged in the bottom of the drying space; a sliding structure is arranged between the top of the drying space and the support frame body; a metal piece is placed on the support frame body; the sliding structure slides up and down in the drying space, and the air flow in the drying space blows over the metal piece.
Further, the top of the drying space is communicated with the outside through a heating device; the drying space is of a barrel-shaped structure; the support frame body comprises a fixed disc; the fixed disc is correspondingly arranged in the bottom of the drying space, and a plurality of vent holes are formed in the fixed disc in a penetrating manner; a plurality of the ventilation hole apertures gradually reduce from top to bottom.
Furthermore, bearing cross frames are arranged above the fixed disc at intervals; the bearing transverse frame is fixed on the fixed disc through a plurality of fixed blocks; the bearing cross frame is of a hollow structure.
Furthermore, the bottom of the drying space is supported by a plurality of support legs; the plurality of support legs are arranged at intervals in the circumferential direction; a cross bar is arranged between the opposite support legs; the middle part of the cross rod is provided with an air guide structure; the air guide structure is arranged right opposite to the bottom of the fixed disc.
Further, the wind guide structure comprises an exhaust fan: the driving end of the driving device on the middle part of the cross rod is in driving connection with the exhaust fan; the exhaust fan is arranged right opposite to the air outlet ends of the plurality of air vents.
Furthermore, a plurality of sliding rails which are arranged at intervals in the circumferential direction are vertically arranged on the inner wall of the drying space; a sliding block is arranged in the bottom end of the sliding rail, and a driving device at the bottom end of the sliding rail is in driving connection with the sliding block; the sliding structure is arranged in the drying space through the sliding block, and the sliding block drives the sliding structure to move up and down in the drying space.
Further, the sliding structure includes a ring block; the side wall of the annular block is correspondingly attached to the inner wall of the drying space in a sliding manner; the sliding blocks are correspondingly fixedly arranged on the side wall of the annular block in a surrounding manner; the middle part of the annular block is a through hole.
Furthermore, a movable groove is annularly formed in the inner wall of the through opening; the movable groove is filled with a movable arc plate; the arc-shaped plates are annularly filled in the movable grooves; the driving end of the telescopic device in the movable groove is in driving connection with one side of the arc-shaped plate; the corresponding motion protrusions of the arc-shaped plates are spliced into a ring shape in the movable groove.
Has the advantages that: in the utility model, heated gas is discharged from the vent hole after passing through the metal piece through the through hole, and the sliding block drives the annular block to move up and down, so that the gas in the drying space can be disturbed to form disordered wind flow, and the surface of the metal piece can be impacted in multiple directions instead of impacting the metal piece from the top only; simultaneously the outstanding movable slot concatenation of arc is in the same place, and the opening air volume reduces, and annular piece and arc up-and-down motion in-process, and the pressure increase of the wind current of drive forms turbulent wind current more easily to the velocity of flow is faster, contacts the metalwork surface more easily, makes the wind current can flow the metalwork more easily and bear between the support contact surface, and it is more even to dry.
Drawings
FIG. 1 is a diagram of a drying space;
FIG. 2 is a structural view of a support frame;
fig. 3 is a sliding structure view.
Detailed Description
The present invention will be further described with reference to the accompanying drawings.
As shown in figures 1-3: processing plant for the production of aeronautical composite materials, comprising a drying space 1; a heating device is detachably arranged on the top of the drying space 1; the bottom of the drying space 1 is provided with an air guide structure 2; the drying space 1 is communicated with the outside through an air guide structure 2 and a heating device respectively; a support frame body 3 is arranged in the bottom of the drying space 1; a sliding structure 4 is arranged between the top of the drying space 1 and the support frame body 3; a metal piece is placed on the support frame body 3; the sliding structure 4 slides up and down in the drying space 1, and the wind flow in the drying space 1 blows over the metal piece. When the air current passes through heating device, heating device heats the air current, and gas after the heating lets in the drying space, and air guide structure will pass through the air current discharge of metalwork again, and then makes gas flow, carries out the drying to the metalwork through the air current that flows for drying efficiency improves production efficiency.
The top of the drying space 1 is communicated with the outside through a heating device; the drying space 1 is of a barrel-shaped structure; the support frame body 3 comprises a fixed disc 31; the fixed disc 31 is correspondingly arranged in the bottom of the drying space 1, and a plurality of vent holes 32 are formed in the fixed disc 31 in a penetrating manner; the apertures of the plurality of ventilation holes 32 are arranged in a gradually decreasing manner from top to bottom. The air current that enters into in the drying space through heating device discharges to the external world from the through-hole, and the interior flowing gas of drying space passes through the metalwork surface, and then can carry out drying process to the metalwork, also carries out heating process to the metalwork simultaneously.
A bearing transverse frame 33 is arranged above the fixed disc 31 at intervals; the bearing transverse frame 33 is fixed on the fixed disc 31 through a plurality of fixed blocks 34; the bearing cross frame 33 is a hollow structure. The metal piece is correspondingly arranged on the bearing cross frame, when hot air flows through the metal piece from top to bottom, the metal piece can be dried and heated, and then the drying effect is achieved.
The bottom of the drying space 1 is supported by a plurality of support legs 11; the plurality of support legs 11 are arranged at intervals in the circumferential direction; a cross rod 111 is arranged between the opposite support legs 11; the middle part of the cross rod 111 is provided with an air guide structure 2; the air guide structure 2 is arranged right opposite to the bottom of the fixed disc 31. The air guide structure 2 includes an exhaust fan 21: the driving end of the driving device on the middle part of the cross rod 111 is in driving connection with the exhaust fan 21; the exhaust fan 21 is arranged right opposite to the air outlet ends of the plurality of air vents 32. Due to the action of the air exhaust fan, air in the drying space is promoted to flow from top to bottom, and the flowing hot air can heat and dry the metal piece.
A plurality of sliding rails 12 which are arranged at intervals in the circumferential direction are vertically arranged on the inner wall of the drying space 1; a sliding block 13 is arranged in the bottom end of the sliding rail 12, and a driving device at the bottom end of the sliding rail 12 is in driving connection with the sliding block 13; the sliding structure 4 is arranged in the drying space 1 through a sliding block 13, and the sliding block 13 drives the sliding structure 4 to move up and down in the drying space 1. Drive arrangement drive slider drives sliding structure and moves from top to bottom in dry space, and the air current in the corresponding upset dry space of sliding structure ability, and then make the air current disorderly, and the metalwork surface can be strikeed from a plurality of directions to disorderly air current, improves the stoving effect.
The sliding structure 4 comprises a ring block 41; the side wall of the annular block 41 is correspondingly attached to the inner wall of the drying space 1 in a sliding manner; a plurality of sliding blocks 13 are correspondingly fixedly arranged on the side wall of the annular block 41 in a surrounding manner; the middle part of the ring block 41 is provided with a through opening 411. The inner wall of the through opening 411 is annularly provided with a movable groove 42; an arc-shaped plate 43 is movably arranged in the movable groove 42; a plurality of arc-shaped plates 43 are annularly filled in the movable groove 42; the driving end of the telescopic device in the movable groove 42 is in driving connection with one side of the arc-shaped plate 43; the corresponding movement of the plurality of arc-shaped plates 43 protrudes from the movable slot 42 and is combined into a ring shape. The heated gas passes through the metal piece through the through hole and then is discharged from the vent hole, the sliding block drives the annular block to move up and down, and then the gas in the drying space can be disturbed to form disturbed wind flow, and the surface of the metal piece can be impacted in multiple directions instead of impacting the metal piece from the top only; simultaneously the outstanding movable slot concatenation of arc is in the same place, and the opening air volume reduces, and annular piece and arc up-and-down motion in-process, and the pressure increase of the wind current of drive forms turbulent wind current more easily to the velocity of flow is faster, contacts the metalwork surface more easily, makes the wind current can flow the metalwork more easily and bear between the support contact surface, and it is more even to dry.
The above is only a preferred embodiment of the present invention, and it should be noted that: for those skilled in the art, without departing from the above-mentioned principles of the present invention, several improvements and modifications can be made, and these improvements and modifications should also be considered as the protection scope of the present invention.

Claims (8)

1. A processing equipment for production of aviation combined material subassembly which characterized in that: comprising a drying space (1); the top of the drying space (1) is detachably provided with a heating device; the bottom of the drying space (1) is provided with an air guide structure (2); the drying space (1) is communicated with the outside through an air guide structure (2) and a heating device respectively; a support frame body (3) is arranged in the bottom of the drying space (1); a sliding structure (4) is arranged between the top of the drying space (1) and the support frame body (3); a metal piece is placed on the support frame body (3); the sliding structure (4) slides up and down in the drying space (1), and the air flow in the drying space (1) blows over the metal piece.
2. The tooling apparatus for the production of aerospace composite components according to claim 1, wherein: the top of the drying space (1) is communicated with the outside through a heating device; the drying space (1) is of a barrel-shaped structure; the support frame body (3) comprises a fixed disc (31); the fixed disc (31) is correspondingly arranged in the bottom of the drying space (1), and a plurality of ventilation holes (32) are formed in the fixed disc (31) in a penetrating manner; the hole diameters of the plurality of ventilation holes (32) are gradually reduced from top to bottom.
3. The tooling apparatus for the production of aerospace composite components according to claim 2, wherein: a bearing cross frame (33) is arranged above the fixed disc (31) at a distance; the bearing transverse frame (33) is fixed on the fixed disc (31) through a plurality of fixed blocks (34); the bearing transverse frame (33) is of a hollow structure.
4. The tooling apparatus for the production of aerospace composite components according to claim 3, wherein: the bottom of the drying space (1) is supported by a plurality of support legs (11); the plurality of support legs (11) are arranged at intervals in the circumferential direction; a cross rod (111) is arranged between the opposite support legs (11); the middle part of the cross rod (111) is provided with an air guide structure (2); the air guide structure (2) is arranged right opposite to the bottom of the fixed disc (31).
5. The tooling apparatus for the production of aerospace composite components according to claim 4, wherein: the air guide structure (2) comprises an exhaust fan (21): the driving end of the driving device on the middle part of the cross rod (111) is in driving connection with the exhaust fan (21); the exhaust fan (21) is arranged right opposite to the air outlet ends of the plurality of air vents (32).
6. The tooling apparatus for the production of aerospace composite components according to claim 5, wherein: a plurality of sliding rails (12) which are arranged at intervals in the circumferential direction are vertically arranged on the inner wall of the drying space (1); a sliding block (13) is arranged in the bottom end of the sliding rail (12), and a driving device at the bottom end of the sliding rail (12) is in driving connection with the sliding block (13); the sliding structure (4) is arranged in the drying space (1) through a sliding block (13), and the sliding block (13) drives the sliding structure (4) to move up and down in the drying space (1).
7. The tooling apparatus for the production of aerospace composite components according to claim 6, wherein: the sliding structure (4) comprises an annular block (41); the side wall of the annular block (41) is correspondingly attached to the inner wall of the drying space (1) in a sliding manner; the sliding blocks (13) are correspondingly fixedly arranged on the side wall of the annular block (41) in a surrounding manner; the middle part of the annular block (41) is provided with a through hole (411).
8. The tooling apparatus for the production of aerospace composite components according to claim 7, wherein: the inner wall of the through opening (411) is annularly provided with a movable groove (42); an arc-shaped plate (43) is movably arranged in the movable groove (42); the arc-shaped plates (43) are filled in the movable groove (42) in the circumferential direction; the driving end of the telescopic device in the movable groove (42) is in driving connection with one side of the arc-shaped plate (43); the corresponding movement projections of the arc-shaped plates (43) are spliced into a ring shape through the movable groove (42).
CN202220917984.XU 2022-04-20 2022-04-20 Processing equipment for producing aviation composite material component Active CN217604526U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202220917984.XU CN217604526U (en) 2022-04-20 2022-04-20 Processing equipment for producing aviation composite material component

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202220917984.XU CN217604526U (en) 2022-04-20 2022-04-20 Processing equipment for producing aviation composite material component

Publications (1)

Publication Number Publication Date
CN217604526U true CN217604526U (en) 2022-10-18

Family

ID=83564747

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202220917984.XU Active CN217604526U (en) 2022-04-20 2022-04-20 Processing equipment for producing aviation composite material component

Country Status (1)

Country Link
CN (1) CN217604526U (en)

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Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of utility model: Processing equipment for aviation composite component production

Effective date of registration: 20230609

Granted publication date: 20221018

Pledgee: Agricultural Bank of China Limited by Share Ltd. Wuxi Huishan branch

Pledgor: JIANGSU HENGMINGDA AVIATION EQUIPMENT Co.,Ltd.

Registration number: Y2023980043123

PE01 Entry into force of the registration of the contract for pledge of patent right