Aero-launch type bullet pulling mechanism

Abstract

The aero-engine type bullet pulling mechanism comprises a shell, the inner wall of the shell is fixedly connected with an inner frame, the inner frame comprises a rack, the inner wall of the rack is rotationally connected with a transmission shaft, one end of the transmission shaft is fixedly connected with a small gear, and symmetrical bullet pressing mechanisms are arranged at the positions, located on the upper side and the lower side of the transmission shaft, of the rack. And the two bullet pressing mechanisms are in transmission connection through a pinion. When the transmission shaft is rotated, the two bullet pressing mechanisms can be rotated at the same time through the small gear, so that two sets of bullets can be machined at the same time on the original basis, the working efficiency is doubled, due to the fact that the equipment is provided with the two bullet pressing mechanisms, the weight is increased, and by adding the moving wheels at the bottom and adding the push handle on the side face, the working efficiency is improved. A user can conveniently move the equipment.

Description

Technical Field

[0001] The invention belongs to the technical field of bullet compression, and in particular relates to an aircraft-launched bullet extraction mechanism. Background Art

[0002] A bullet press is a device specially used for making ammunition. It can mix empty cartridge cases, bullets and gunpowder with a precise amount of powder, and combine them together under high pressure to form a complete ammunition. The existing bullet press only has one set of bullet pressing mechanisms, so it can only process one set of bullets at a time, so its efficiency is relatively low. For this reason, we propose an aircraft-type bullet extraction mechanism. Summary of the invention

[0003] In view of the deficiencies in the prior art, the present invention aims to provide an aircraft-generated bullet extraction mechanism which has the advantage of being easy to process.

[0004] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: an aircraft-generated bullet extraction mechanism, comprising an outer shell, the inner wall of the outer shell is fixedly connected to an inner frame, the inner frame comprises a frame, the inner wall of the frame is rotatably connected to a transmission shaft, one end of the transmission shaft is fixedly connected to a pinion, the frame is located on the upper and lower sides of the transmission shaft and is provided with symmetrical bullet pressing mechanisms, and the two bullet pressing mechanisms are connected by a pinion transmission.

[0005] The above technical solution can achieve the effect of fast loading. When the transmission shaft is rotated, the two bullet pressing mechanisms can be rotated at the same time through the small gear. In this way, two groups of bullets can be processed at the same time on the original basis, thereby doubling the work efficiency.

[0006] Preferably, the bottom outer wall of the shell is fixedly connected to a bottom vehicle, the bottom outer wall of the bottom vehicle is fixedly connected to a plurality of moving wheels, and the outer wall of the bottom vehicle is fixedly connected to a push handle.

[0007] The above technical solution can facilitate mobility. Since the device has two sets of spring-loaded mechanisms, its weight increases. In this way, by adding moving wheels at the bottom and a push handle on the side, users can move the device more conveniently.

[0008] Preferably, a detachable handle is provided at one end of the transmission shaft away from the pinion, a detachable motor is provided on the outer wall of the pinion, and a bullet feeding plate is fixedly connected to the frame at the entrance of the two bullet pressing mechanisms.

[0009] Through the above technical solution, the effect of having multiple starting modes can be achieved. Since the motor and the handle can be disassembled, the handle can continue to work after the motor is out of power.

[0010] Preferably, the outer wall of the shell is fixedly connected to the shell bottom, and the outer walls on both sides of the shell bottom are rotatably connected to door panels.

[0011] The above technical solution can achieve a sealing effect, and due to the installation of the door panel, the outer shell can be sealed after it is closed.

[0012] Preferably, two symmetrical side panels are fixedly connected to the outer walls on both sides of the shell bottom, and a top cover is fixedly connected to the top outer wall of the side panel.

[0013] Through the above technical solution, the top can be opened. The top of the shell is opened and closed by the top cover, so that the top of the shell can be opened.

[0014] Preferably, a through hole is formed on the outer wall of the side plate away from the push handle, and a motor seat is fixedly connected to the inner wall of the other side plate.

[0015] The above technical solution can facilitate the workmanship of the output device, the perforation allows the handle to pass through, thereby avoiding blocking the rotation of the handle, and the motor seat provides support for the motor, thereby stabilizing the output of the motor.

[0016] Compared with the prior art, the present invention has the following beneficial effects: 1. When rotating the transmission shaft, the two bullet pressing mechanisms can be rotated at the same time through the small gear, so that two groups of bullets can be processed at the same time on the original basis, thereby doubling the work efficiency. Since the equipment has two groups of bullet pressing mechanisms, the weight increases. In this way, by adding moving wheels at the bottom and push handles on the side, users can move the equipment more conveniently.

[0017] 2. Since the motor and the handle are detachable, the handle can continue to work even after the motor is out of power. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 It is a schematic diagram of the main structure of the present invention; Figure 2 It is a structural schematic diagram of the other side of the main body of the present invention; Figure 3 It is a schematic diagram of the push handle structure of the present invention; Figure 4 It is a schematic diagram of the inner frame structure of the present invention.

[0019] In the figure: 1, outer shell; 2, bottom car; 3, moving wheel; 4, push handle; 5, inner frame; 6, top cover; 100, shell bottom; 101, door panel; 102, side panel; 103, perforation; 104, motor seat; 500, frame; 501, transmission shaft; 502, pinion; 503, bullet pressing mechanism; 504, bullet feeding plate; 505, motor; 506, handle. DETAILED DESCRIPTION

[0020] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention. Embodiment 1:

[0021] See also Figure 1-Figure 4 The present invention provides a technical solution: an aircraft-type bullet extraction mechanism, comprising an outer shell 1, an inner frame 5 is fixedly connected to the inner wall of the outer shell 1, the inner frame 5 comprises a frame 500, the inner wall of the frame 500 is rotatably connected to a transmission shaft 501, one end of the transmission shaft 501 is fixedly connected to a pinion 502, the frame 500 is provided with symmetrical bullet pressing mechanisms 503 on the upper and lower sides of the transmission shaft 501, the two bullet pressing mechanisms 503 are connected by transmission via the pinion 502, the bottom outer wall of the outer shell 1 is fixedly connected to a bottom vehicle 2, the bottom outer wall of the bottom vehicle 2 is fixedly connected to a plurality of moving wheels 3, and the outer wall of the bottom vehicle 2 is fixedly connected to a push handle 4.

[0022] In this embodiment, when the transmission shaft 501 is rotated, the two bullet pressing mechanisms 503 can be rotated simultaneously through the small gear 502, so that two groups of bullets can be processed simultaneously on the original basis, thereby doubling the work efficiency. Since the equipment has two groups of bullet pressing mechanisms 503, the weight is increased. In this way, by adding a moving wheel 3 at the bottom and a push handle 4 on the side, it can be convenient for users to move the equipment. Embodiment 2:

[0023] See also Figure 4 On the basis of the first embodiment, the present invention provides a technical solution: a detachable handle 506 is provided at one end of the transmission shaft 501 away from the pinion 502, a detachable motor 505 is provided on the outer wall of the pinion 502, and a feeding plate 504 is fixedly connected to the frame 500 at the entrance of the two bullet pressing mechanisms 503.

[0024] In this embodiment, since the motor 505 and the handle 506 are detachable, the handle 506 can continue to work even after the motor 505 runs out of power. Embodiment three:

[0025] See also Figure 3 On the basis of Embodiment 1 and Embodiment 2, the present invention provides a technical solution: the outer wall of the outer shell 1 is fixedly connected to the shell bottom 100, the outer walls on both sides of the shell bottom 100 are rotatably connected to the door panels 101, the outer walls on both sides of the shell bottom 100 are fixedly connected to two symmetrical side panels 102, the top outer wall of the side panel 102 is fixedly connected to the top cover 6, the outer wall of the side panel 102 away from the push handle 4 is provided with a through hole 103, and the inner wall of the other side panel 102 is fixedly connected to the motor seat 104.

[0026] In this embodiment, due to the installation of the door panel 101, the outer shell 1 can be sealed after it is closed, and the top of the outer shell 1 can be opened and closed by the top cover 6, so that the top of the outer shell 1 can be opened. The perforation 103 allows the handle 506 to pass through, thereby avoiding blocking the rotation of the handle 506. The motor base 104 provides support for the motor 505, thereby stabilizing the output of the motor 505.

[0027] The working principle and use process of the present invention are as follows: when the transmission shaft 501 is rotated, the two bullet pressing mechanisms 503 can be rotated simultaneously through the small gear 502, so that two groups of bullets can be processed at the same time on the original basis, thereby doubling the work efficiency. Since the equipment has two groups of bullet pressing mechanisms 503, the weight is increased. In this way, by adding a moving wheel 3 at the bottom and a push handle 4 at the side, it is convenient for users to move the equipment. Since the motor 505 and the handle 506 are detachable, the handle 506 can continue to work after the motor 505 is out of power. Due to the installation of the door panel 101, the outer shell 1 can be sealed after it is closed, and the top of the outer shell 1 can be opened and closed through the top cover 6, so as to achieve the effect of opening the top of the outer shell 1. The perforation 103 allows the handle 506 to pass through, thereby avoiding blocking the handle 506 from rotating. The motor base 104 provides support for the motor 505, thereby stabilizing the output of the motor 505.

[0028] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An aircraft-generated bullet extraction mechanism, comprising a housing (1), characterized in that: The inner wall of the outer shell (1) is fixedly connected to an inner frame (5), the inner frame (5) comprises a frame (500), the inner wall of the frame (500) is rotatably connected to a transmission shaft (501), one end of the transmission shaft (501) is fixedly connected to a pinion (502), the frame (500) is provided with symmetrical spring-loaded mechanisms (503) located on the upper and lower sides of the transmission shaft (501), and the two spring-loaded mechanisms (503) are connected in transmission via the pinion (502).

2. The aircraft-generated bullet extraction mechanism according to claim 1, characterized in that: The bottom outer wall of the housing (1) is fixedly connected to a bottom vehicle (2), the bottom outer wall of the bottom vehicle (2) is fixedly connected to a plurality of moving wheels (3), and the outer wall of the bottom vehicle (2) is fixedly connected to a push handle (4).

3. The aircraft-launched bullet extraction mechanism according to claim 1, characterized in that: A detachable handle (506) is provided at one end of the transmission shaft (501) away from the pinion gear (502), a detachable motor (505) is provided on the outer wall of the pinion gear (502), and a bullet feeding plate (504) is fixedly connected to the frame (500) at the entrance of the two bullet pressing mechanisms (503).

4. The aircraft-launched bullet extraction mechanism according to claim 1, characterized in that: The outer wall of the outer shell (1) is fixedly connected to the shell bottom (100), and the outer walls on both sides of the shell bottom (100) are rotatably connected to the door panels (101).

5. The aircraft-launched bullet extraction mechanism according to claim 4, characterized in that: Two symmetrical side panels (102) are fixedly connected to the outer walls on both sides of the shell bottom (100), and a top cover (6) is fixedly connected to the top outer walls of the side panels (102).

6. The aircraft-generated bullet extraction mechanism according to claim 1, characterized in that: The outer wall of the side plate (102) away from the push handle (4) is provided with a through hole (103), and the inner wall of the other side plate (102) is fixedly connected to a motor seat (104).

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