CN220329738U - Punching device applied to machining of components of chassis of aircraft console - Google Patents

Punching device applied to machining of components of chassis of aircraft console Download PDF

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Publication number
CN220329738U
CN220329738U CN202321418334.1U CN202321418334U CN220329738U CN 220329738 U CN220329738 U CN 220329738U CN 202321418334 U CN202321418334 U CN 202321418334U CN 220329738 U CN220329738 U CN 220329738U
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CN
China
Prior art keywords
gear
lifting
punching
punching device
fixed mounting
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Application number
CN202321418334.1U
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Chinese (zh)
Inventor
张义鹏
陈昆
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Hanzhong Zhongwang Ruicheng Precision Machinery Co ltd
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Hanzhong Zhongwang Ruicheng Precision Machinery Co ltd
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Priority to CN202321418334.1U priority Critical patent/CN220329738U/en
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

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  • Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)

Abstract

The utility model relates to the technical field of machining of aircraft console cabinets and discloses a punching device applied to machining of aircraft console cabinet components. This be applied to punching device of aircraft control cabinet machine case spare part processing, through the fixed establishment that rises that sets up, in the use, promote the handle and make it near the material, can rotate with the hand after aiming at and shake the post, make the gear pole take spacing empty board gliding for fill up the floor contact ground and raise the device, accomplish with the fixed back on ground, through driving motor, make the threaded rod rotate, the lifting lifts empty box, make punching device adjust suitable height, improved punching device and adjusted the ability of punching position at will.

Description

Punching device applied to machining of components of chassis of aircraft console
Technical Field
The utility model relates to the technical field of machining of aircraft console cabinets, in particular to a punching device applied to machining of components of an aircraft console cabinet.
Background
The punching device is a mechanical device for finishing punching by using a punching die to act on a material under the drive of a power mechanism after the raw material is installed. The punching device can perform operations of sheet processing, punching, die pressing, embossing and the like to force the metal into the die.
The utility model relates to a punching device described in a punching device (authorized bulletin number: CN 208977976U) disclosed in a patent net, which comprises a conveying frame, a punch and a collecting box, wherein the punch is arranged above the conveying frame, the collecting box is arranged below the conveying frame, the punching device comprises a balance block, a pulley and a connecting rope, one end of the connecting rope bypasses the pulley to be connected with the collecting box, the balance block is arranged at the other end of the connecting rope, a switch is arranged at the bottom of the conveying frame, the balance block is arranged below the switch, a collecting opening is arranged on the conveying frame, the collecting box is arranged below the collecting opening, and the punch is arranged above the collecting opening. The punching device provided by the utility model can automatically cut off the power supply after the collection box is full, and prompt a user to replace the collection box in time without manual operation, so that the production efficiency is improved.
With respect to the above description, the applicant believes that the following problems exist:
in the using process, the collecting box and the collecting opening are arranged, and in the using process, after punching is carried out by using the punching device, the collecting box can be automatically powered off after being fully stored, so that a person is reminded of replacing the collecting box.
Disclosure of Invention
The utility model aims to provide a punching device applied to machining of components of an aircraft console chassis, so as to solve the problems in the background art.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a be applied to punching device of aircraft control cabinet machine case spare part processing, includes the universal wheel, the top fixed mounting of universal wheel has the hollow piece, the right side fixed mounting of hollow piece has the handle, the top fixed mounting of hollow piece has rise fixed establishment, the top fixed mounting of rising fixed establishment has aircraft control cabinet machine case spare part processing punching mechanism.
The lifting fixing mechanism comprises a lifting assembly and a lifting assembly, and the lifting assembly is arranged at the top of the lifting assembly.
The processing and punching mechanism for the aircraft console chassis components comprises a punching fixing seat, wherein the punching fixing seat is fixedly arranged at the top of a lifting component, a hydraulic rod is fixedly arranged on the left side of the punching fixing seat, a punching rod is fixedly arranged on the left side of the hydraulic rod, a fixing base is fixedly arranged on the outer portion of the hydraulic rod, and the aircraft console chassis components are convenient to punch through the processing and punching mechanism.
Preferably, the bottom of unable adjustment base and lifting unit's top fixed mounting improves the fixed stability of aircraft control cabinet machine case spare part processing mechanism that punches a hole.
Preferably, the lifting assembly comprises a sliding column, the sliding column is slidably mounted in the hollow block, a limiting empty plate is fixedly mounted at the top of the sliding column, a floor pad is fixedly mounted at the bottom of the sliding column, a gear rod is fixedly mounted on the front face of the limiting empty plate, a first gear is meshed with the left side of the gear rod, a second gear is fixedly mounted on the front face of the first gear, a power gear is meshed with the left side of the second gear, a shaking column is rotatably mounted on the front face of the power gear, and a gear seat is rotatably mounted on the front face of the second gear, so that the device is conveniently lifted by the lifting assembly to lift the hollow block and is fixed at one place without sliding.
Preferably, the back of first gear and power gear all is provided with the gear seat, the bottom of the gear seat that first gear and power gear back set up and the inboard fixed mounting of bottom of hollow piece, the back of the positive rotation installation of second gear and the positive fixed mounting of hollow piece, be convenient for shake the post through the rotation and put down the floor pad.
Preferably, the sliding hole is formed in the position, corresponding to the sliding column, of the hollow block, and the sliding column is slidably mounted in the sliding hole formed in the hollow block, so that the lifting assembly can be conveniently used in a normal state.
Preferably, the lifting assembly comprises a motor box, the motor box is fixedly arranged on the inner side of the bottom of the hollow block, a motor is fixedly arranged in the motor box, a threaded rod is fixedly arranged at the top of the motor, a lifting empty box is slidably arranged outside the threaded rod, a limiting rod is slidably arranged in the lifting empty box, and the lifting punching device is convenient to lift through the lifting assembly.
Preferably, through holes are formed in the positions, corresponding to the threaded rods, of the hollow blocks and the lifting empty boxes, and the threaded rods are rotatably arranged in the through holes formed in the hollow blocks and the lifting empty boxes, so that the lifting assembly is driven by a motor conveniently.
Compared with the prior art, the utility model provides the punching device applied to the machining of the components of the chassis of the aircraft console, which has the following beneficial effects:
1. this be applied to punching device of aircraft control cabinet machine case spare part processing, in the use, when the punching device is used to needs, promote the handle and make it reach near the material, can rotate the column of shaking after aiming at, make power gear rotate, and drive second gear and first gear rotation, make the gear pole take spacing empty board gliding, make the floor of pad contact ground and raise the device, accomplish with the fixed back on ground, through driving motor, make the threaded rod rotate, and under the spacing of gag lever post, the lifting lifts empty box, make punching device adjust to suitable height, the ability of punching device adjusting the punching position at will has been improved.
2. This be applied to punching device of aircraft control cabinet machine case spare part processing, the mechanism of punching a hole is processed through the aircraft control cabinet machine case spare part that sets up, in the use, through driving the hydraulic stem, makes the hydraulic stem promote the pole of punching a hole forward for it punches the material, has realized punching device's function of punching a hole.
Drawings
For a clearer description of the technical solutions of the embodiments of the present utility model, the drawings that are needed in the description of the embodiments will be briefly described below, it will be apparent that the drawings in the description below are only some embodiments of the present utility model, and that other drawings can be obtained according to these drawings without inventive effort for a person skilled in the art:
FIG. 1 is a schematic view of the appearance structure of the present utility model;
FIG. 2 is a schematic view of the structure of the lifting fixing mechanism according to the present utility model;
FIG. 3 is a schematic view of the appearance of the lift assembly of the present utility model;
FIG. 4 is a schematic view of the structure of the lifting assembly according to the present utility model;
fig. 5 is a schematic view of an appearance and structure of a punching mechanism for machining components of an aircraft console. In the figure: 1. a universal wheel; 2. a hollow block; 3. a handle; 4. a lifting fixing mechanism; 41. a lifting assembly; 411. a sliding column; 412. a limiting empty plate; 413. a floor is padded; 414. a gear lever; 415. a first gear; 416. a second gear; 417. a power gear; 418. shaking the column; 419. a gear seat; 42. a lifting assembly; 421. a motor box; 422. a motor; 423. a threaded rod; 424. lifting the empty box; 425. a limit rod; 5. machining and punching mechanisms for components of the chassis of the aircraft console; 51. punching a fixed seat; 52. a hydraulic rod; 53. punching a hole rod; 54. and (5) fixing the base.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
In the present utility model, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. The specific meaning of the above terms in the present utility model can be understood by those of ordinary skill in the art according to the specific circumstances.
Embodiment one:
referring to fig. 1-4, the present utility model provides a technical solution: the utility model provides a be applied to punching device of aircraft control cabinet machine case spare part processing, includes universal wheel 1, and the top fixed mounting of universal wheel 1 has hollow piece 2, and the right side fixed mounting of hollow piece 2 has handle 3, and the top fixed mounting of hollow piece 2 has rise fixed establishment 4, and the top fixed mounting of rising fixed establishment 4 has aircraft control cabinet machine case spare part processing punching mechanism 5.
The lifting and fixing mechanism 4 includes a lifting assembly 41 and a lifting assembly 42, the lifting assembly 42 being provided on top of the lifting assembly 41.
Further, the lifting assembly 41 includes a sliding column 411, the sliding column 411 is slidably mounted in the hollow block 2, a limiting hollow plate 412 is fixedly mounted at the top of the sliding column 411, a floor pad 413 is fixedly mounted at the bottom of the sliding column 411, a gear rod 414 is fixedly mounted on the front surface of the limiting hollow plate 412, a first gear 415 is meshed with the left side of the gear rod 414, a second gear 416 is fixedly mounted on the front surface of the first gear 415, a power gear 417 is meshed with the left side of the second gear 416, a shaking column 418 is rotatably mounted on the front surface of the power gear 417, and a gear seat 419 is rotatably mounted on the front surface of the second gear 416, so that the hollow block 2 is lifted by the lifting assembly 41 to fix the device at one place without sliding.
Further, the back of the first gear 415 and the back of the power gear 417 are both provided with a gear seat 419, the bottom of the gear seat 419 arranged at the back of the first gear 415 and the back of the power gear 417 is fixedly installed at the inner side of the bottom of the hollow block 2, and the back of the gear seat 419 rotatably installed at the front of the second gear 416 is fixedly installed at the front of the hollow block 2, so that the floor pad 413 is conveniently put down by rotating the shaking column 418.
Further, the corresponding positions of the hollow block 2 and the sliding column 411 are provided with sliding holes, and the sliding column 411 is slidably mounted in the sliding holes provided in the hollow block 2, so that the lifting assembly 41 can be conveniently used in a normal state.
Further, the lifting assembly 42 comprises a motor box 421, the motor box 421 is fixedly mounted on the inner side of the bottom of the hollow block 2, a motor 422 is fixedly mounted in the motor box 421, a threaded rod 423 is fixedly mounted on the top of the motor 422, a lifting empty box 424 is slidably mounted on the outer portion of the threaded rod 423, and a limiting rod 425 is slidably mounted in the lifting empty box 424, so that the lifting punching device can be lifted through the lifting assembly 42.
Further, through holes are formed in positions, corresponding to the threaded rods 423, of the hollow blocks 2 and the lifting empty boxes 424, and the threaded rods 423 are rotatably installed inside the through holes formed in the hollow blocks 2 and the lifting empty boxes 424, so that the lifting assembly 42 is conveniently driven by the motor 422.
Embodiment two:
referring to fig. 5, in combination with the first embodiment, further obtaining the processing and punching mechanism 5 of the chassis component of the aircraft console includes a punching fixing seat 51, the punching fixing seat 51 is fixedly installed at the top of the lifting component 42, a hydraulic rod 52 is fixedly installed at the left side of the punching fixing seat 51, a punching rod 53 is fixedly installed at the left side of the hydraulic rod 52, and a fixing base 54 is fixedly installed at the outer part of the hydraulic rod 52, so that punching is performed by the processing and punching mechanism 5 of the chassis component of the aircraft console.
Further, the bottom of the fixed base 54 is fixedly mounted with the top of the lifting assembly 42, so that the stability of fixing the machining punching mechanism 5 of the aircraft console chassis component is improved.
In the actual operation process, when the device is used, the handle 3 is pushed to enable the punching device to reach a place where material processing is required, after a good position is selected, the shaking post 418 starts to rotate at the moment, the shaking post 418 drives the power gear 417 to rotate, the second gear 416 meshed with the power gear 417 reversely rotates under the action of the power gear 417 and drives the first gear 415 to reversely rotate, at the moment, the gear rod 414 meshed with the first gear 415 descends under the action of the first gear 415, the sliding post 411 slides in the hollow block 2, at the moment, the floor 413 starts to slide downwards under the rotation of the shaking post 418, and does not stop after contacting the ground until the hollow block 2 is lifted, so that the universal wheel 1 is isolated from the ground, after the fixing is completed, the motor 422 is driven, the transmission shaft of the motor 422 starts to rotate, the threaded rod 423 is driven to rotate, the empty box 424 starts to ascend under the limiting action of the limiting rod 425, at the step, when a proper position is reached, the operation liquid 52 capable of punching can be carried out, the punching device is driven to rotate downwards, the punching device is driven to rotate, and the punching device is enabled to rotate, and the base seat 53 is reversely punched, and the punching device is enabled to rotate, and the punching device is enabled to be fixed to be punched to be rotated.
It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising one does not exclude the presence of other like elements in a process, method, article, or apparatus that comprises an element.

Claims (7)

1. Be applied to punching device of aircraft control cabinet machine case spare part processing, including universal wheel (1), its characterized in that: the top of the universal wheel (1) is fixedly provided with a hollow block (2), the right side of the hollow block (2) is fixedly provided with a handle (3), the top of the hollow block (2) is fixedly provided with a lifting fixing mechanism (4), and the top of the lifting fixing mechanism (4) is fixedly provided with an aircraft console case component processing punching mechanism (5);
the lifting fixing mechanism (4) comprises a lifting assembly (41) and a lifting assembly (42), wherein the lifting assembly (42) is arranged at the top of the lifting assembly (41);
the machining and punching mechanism (5) for the components of the aircraft console comprises a punching fixing seat (51), the punching fixing seat (51) is fixedly arranged at the top of the lifting component (42), a hydraulic rod (52) is fixedly arranged on the left side of the punching fixing seat (51), a punching rod (53) is fixedly arranged on the left side of the hydraulic rod (52), and a fixing base (54) is fixedly arranged on the outer portion of the hydraulic rod (52).
2. The punching device for machining components of an aircraft console chassis according to claim 1, wherein: the bottom of the fixed base (54) is fixedly arranged with the top of the lifting component (42).
3. The punching device for machining components of an aircraft console chassis according to claim 1, wherein: lifting subassembly (41) are including slip post (411), slip post (411) slidable mounting is in the inside of hollow piece (2), the top fixed mounting of slip post (411) has spacing blank (412), the bottom fixed mounting of slip post (411) has cushioned plate (413), the front fixed mounting of spacing blank (412) has gear pole (414), the left side meshing of gear pole (414) has first gear (415), the front fixed mounting of first gear (415) has second gear (416), the left side meshing of second gear (416) has power gear (417), the front rotation of power gear (417) is installed and is waved post (418), the front rotation of second gear (416) is installed gear seat (419).
4. A punching device for machining components of an aircraft console chassis according to claim 3, wherein: the back of first gear (415) and power gear (417) all is provided with gear seat (419), the bottom of gear seat (419) that first gear (415) and power gear (417) back set up and the inboard fixed mounting of bottom of hollow block (2), the back of gear seat (419) of second gear (416) openly rotation installation and the front fixed mounting of hollow block (2).
5. The punching device for machining components of an aircraft console chassis according to claim 4, wherein: slide holes are formed in the corresponding positions of the hollow blocks (2) and the slide columns (411), and the slide columns (411) are slidably mounted in the slide holes formed in the hollow blocks (2).
6. The punching device for machining components of an aircraft console chassis according to claim 1, wherein: lifting assembly (42) are including motor box (421), motor box (421) fixed mounting is inboard in the bottom of hollow piece (2), the inside fixed mounting of motor box (421) has motor (422), the top fixed mounting of motor (422) has threaded rod (423), the outside slidable mounting of threaded rod (423) has lifting empty box (424), the inside slidable mounting of lifting empty box (424) has gag lever post (425).
7. The punching device for machining components of an aircraft console chassis according to claim 6, wherein: through holes are formed in the positions, corresponding to the threaded rods (423), of the hollow blocks (2) and the lifting empty boxes (424), and the threaded rods (423) are rotatably installed inside the through holes formed in the hollow blocks (2) and the lifting empty boxes (424).
CN202321418334.1U 2023-06-05 2023-06-05 Punching device applied to machining of components of chassis of aircraft console Active CN220329738U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202321418334.1U CN220329738U (en) 2023-06-05 2023-06-05 Punching device applied to machining of components of chassis of aircraft console

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202321418334.1U CN220329738U (en) 2023-06-05 2023-06-05 Punching device applied to machining of components of chassis of aircraft console

Publications (1)

Publication Number Publication Date
CN220329738U true CN220329738U (en) 2024-01-12

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ID=89458381

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202321418334.1U Active CN220329738U (en) 2023-06-05 2023-06-05 Punching device applied to machining of components of chassis of aircraft console

Country Status (1)

Country Link
CN (1) CN220329738U (en)

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