Auxiliary assembling mechanism for simulated bomb

Abstract

The utility model provides an auxiliary assembling mechanism for a simulated missile, which relates to the field of assembling tools and comprises a lifting component and two brackets mounted at the uppermost part of the lifting component, wherein each bracket is provided with a groove for accommodating a simulated bullet, and the bottom of the groove is provided with two pulleys for lifting the simulated bullet; the two brackets are provided with grooves, the two sides of the grooves are further provided with screw rods matched with the brackets in a threaded mode, the simulated bomb is located in the moving path of the screw rods, and after a fixing point used for the simulated bomb is adjusted to be over, the screw rods get close to and make contact with the simulated bomb, and the simulated bomb is locked in the two brackets. And the rubber head at the end part of the screw rod is contacted with the simulated bomb, so that the simulated bomb is locked in the two brackets, and the fixed point of the simulated bomb is always positioned right above.

Description

Technical Field

[0001] The utility model relates to the field of assembly tools, in particular to a simulated bullet auxiliary assembly mechanism. Background Art

[0002] At this stage, Figure 1 The simulated missile shown is transported to the bottom of the wing using a bracket, and then the bomb is lifted by a lifting mechanism and moved to the rack. This type of device, first, requires auxiliary installation of lifting mechanisms such as hydraulic lifts, and cannot operate the assembly height of the simulated missile by itself; second, the simulated missile is a columnar body, which has few effective fixing points in the bracket, and is easy to rotate and deviate under the influence of inertia or lateral forces, and is not easy to combine with the rack; third, when the simulated missile deviates in the bracket, in addition to being affected by inertia and other forces and lateral forces, it is difficult for personnel to actively control the movement of the simulated missile, which further amplifies the second problem mentioned above. Therefore, in view of the above situation, it is necessary to propose a simulated missile auxiliary assembly mechanism. Utility Model Content

[0003] The utility model aims to provide a simulated bullet auxiliary assembly mechanism to solve the above technical problems.

[0004] In order to solve the above technical problems, the utility model adopts the following technical solutions:

[0005] A simulated projectile auxiliary assembly mechanism, comprising a lifting assembly, and two brackets mounted on the uppermost part of the lifting assembly;

[0006] Each bracket has a slot for accommodating a dummy bullet, and the bottom of the slot has two pulleys for lifting the dummy bullet;

[0007] There are screws on both sides of the groove that cooperate with the bracket threads. The simulated bullet is located in the moving path of the screws. After the fixing point of the simulated bullet is adjusted to just above, the screws approach and contact the simulated bullet, locking the simulated bullet in the two brackets.

[0008] Preferably, the lifting assembly lifts the simulated missile and moves it upward to a hanging point under the wing.

[0009] Preferably, the lifting assembly includes a first plate on which the two brackets are mounted, a second plate located below the first plate, and a lifting portion between the first plate and the second plate.

[0010] Preferably, the lifting part comprises two first arms rotatably connected to the first plate, and two second arms rotatably connected to the second plate;

[0011] A first arm and an adjacent second arm form an X-shaped structure, the center of the X-shaped structure has an axis connected to the center of another X-shaped structure, a first roller located at the other end of the first arm and rollingly matched with the second plate, and a second roller located at the other end of the second arm and rollingly matched with the first plate;

[0012] There are also two hydraulic cylinders that are rotatably connected to the second plate and apply force to the shaft. The two hydraulic cylinders control the two X-shaped structures to adjust the relative height between the first plate and the second plate.

[0013] Preferably, it also includes four casters installed below the second plate.

[0014] Preferably, it also includes a first handle extending outward from the second plate.

[0015] Preferably, the bracket is provided with a second handle.

[0016] Preferably, the end of the screw rod in contact with the simulated bullet is provided with a rubber head.

[0017] The beneficial effects of the utility model are:

[0018] 1. In the utility model, there are two pulleys in the bracket, and the pulleys lift the simulated bullets in the two brackets so that the simulated bullets can rotate axially in the brackets, thereby adjusting the position of the fixed point of the simulated bullet.

[0019] 2. In the utility model, after the positions of the dummy bullets in the two brackets are determined, the screw can be screwed so that the rubber head at the end of the screw contacts the dummy bullets, thereby locking the dummy bullets in the two brackets, and keeping the fixed points of the dummy bullets always located directly above.

[0020] 3. The utility model is equipped with a lifting assembly, which can lift the locked simulated missile directly to the bottom of the wing, making it convenient for personnel to combine the simulated missile with the hanging point under the wing. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] Figure 1 A schematic diagram of a simulated projectile;

[0022] Figure 2 It is a structural schematic diagram of a simulated projectile auxiliary assembly mechanism;

[0023] Figure 3 for Figure 2 A schematic diagram of the structure of the lifting assembly in the middle part;

[0024] Figure 4 for Figure 1 The simulated projectile shown is Figure 2 The schematic diagram of the structure in the auxiliary assembly mechanism of the simulated projectile is shown;

[0025] Figure numerals: 1. first plate; 2. second plate; 3. lifting part; 4. first handle; 5. caster; 6. bracket; 7. second handle; 8. screw; 9. rubber head; 10. pulley; 31. first arm; 32. second arm; 33. shaft; 34. hydraulic cylinder; 35. first roller; 36. second roller; 37. first adapter; 38. second adapter. DETAILED DESCRIPTION

[0026] In order to make the technical means, creative features, objectives and effects of the present invention easy to understand, the present invention is further described below in conjunction with specific embodiments and drawings, but the following embodiments are only preferred embodiments of the present invention, not all. Based on the embodiments in the implementation mode, other embodiments obtained by those skilled in the art without creative work are all within the protection scope of the present invention.

[0027] The specific embodiments of the present utility model are described below in conjunction with the accompanying drawings.

[0028] Example 1

[0029] In this embodiment, a simulated bullet auxiliary assembly mechanism is proposed. Figure 1 For reference, see Figure 2-Figure 4 The simulated projectile auxiliary assembly mechanism includes a lifting component, which can be generally divided into a first plate 1, a second plate 2 located below the first plate 1, and a lifting part 3 arranged in the interlayer between the first plate 1 and the second plate 2.

[0030] Further explanation, such as Figure 2 As shown, the lifting part 3 includes two first arms 31 rotatably connected to the first plate 1 and two second arms 32 rotatably connected to the second plate 2. The two first arms 31 are arranged side by side with a gap, and the two second arms 32 are also arranged side by side with a gap.

[0031] To further illustrate, a first arm 31 and an adjacent second arm 32 form an X-shaped structure, the center of the X-shaped structure has an axis 33 connected to the center of the other X-shaped structure, a first roller 35 located at the other end of the first arm 31 and rollingly engaged with the second plate 2, and a second roller 36 located at the other end of the second arm 32 and rollingly engaged with the first plate 1;

[0032] There are also two hydraulic cylinders 34 that are rotationally connected to the second plate 2 and apply force to the shaft 33. The two hydraulic cylinders 34 combine with the shaft 33 to apply force to the two X-shaped structures to adjust the relative height between the first plate 1 and the second plate 2.

[0033] See also Figure 3 The first arm 31 is rotatably connected to the first plate 1 via the second adapter seat 38 , and the second arm 32 is rotatably connected to the second plate 2 via the first adapter seat 37 .

[0034] Please continue reading Figure 3 In order to cooperate with the first roller 35 set at the end of the first arm 31, a linear groove is set on the surface of the second plate 2. Of course, in order to cooperate with the second roller 36 set at the end of the second arm 32, a linear groove is also set on the surface of the first plate 1. In this way, the roller enters the linear groove to constrain the movement direction of the X-shaped structure.

[0035] See also Figure 1 Two brackets 6 are arranged on the top of the first plate 1, wherein each bracket 6 has a groove for accommodating a simulated bullet, and the bottom of the groove has two pulleys 10 for lifting the simulated bullet;

[0036] Further explanation, there are screw rods 8 on both sides of the groove that are threadedly matched with the bracket 6, and the simulated bullet is located in the moving path of the screw rods 8. Figure 1 After the fixing point of the simulated bullet is adjusted to the top, the simulated bullet is locked in the two brackets 6 by approaching the screw rod 8 and contacting the simulated bullet. The effect after locking is as follows: Figure 4 shown.

[0037] To further explain, the above-mentioned lifting mechanism can lift the simulated missile upward to the hanging point under the wing.

[0038] In this embodiment, the following additional contents are required:

[0039] First, the second plate 2 has a first handle 4 extending outward, and the first handle 4 is a force-carrying part for a person to control the movement of the entire mechanism.

[0040] Secondly, the bracket 6 is provided with a second handle 7 .

[0041] Third, the end of the screw rod 8 that contacts the simulated bullet is provided with a rubber head 9, and the rubber head 9 will replace the end of the screw rod 8 to contact the simulated bullet body.

[0042] Fourth, in order to facilitate the movement of the mechanism, four casters 5 are provided at the bottom of the mechanism.

Claims

1. A simulated projectile auxiliary assembly mechanism, characterized in that: It includes a lifting assembly and two brackets mounted on the uppermost part of the lifting assembly; Each bracket has a slot for accommodating a dummy bullet, and the bottom of the slot has two pulleys for lifting the dummy bullet; There are screws on both sides of the groove that cooperate with the bracket threads. The simulated bullet is located in the moving path of the screws. After the fixing point of the simulated bullet is adjusted to just above, the screws approach and contact the simulated bullet, locking the simulated bullet in the two brackets.

2. The simulated projectile auxiliary assembly mechanism according to claim 1, characterized in that: The lifting assembly lifts the simulated missile upward to the hanging point under the wing.

3. The simulated projectile auxiliary assembly mechanism according to claim 2, characterized in that: The lifting assembly includes a first plate on which the two brackets are mounted, a second plate located below the first plate, and a lifting portion between the first plate and the second plate.

4. The simulated projectile auxiliary assembly mechanism according to claim 3, characterized in that: The lifting part includes two first arms rotatably connected to the first plate and two second arms rotatably connected to the second plate; A first arm and an adjacent second arm form an X-shaped structure, the center of the X-shaped structure has an axis connected to the center of another X-shaped structure, a first roller located at the other end of the first arm and rollingly matched with the second plate, and a second roller located at the other end of the second arm and rollingly matched with the first plate; There are also two hydraulic cylinders that are rotatably connected to the second plate and apply force to the shaft. The two hydraulic cylinders control the two X-shaped structures to adjust the relative height between the first plate and the second plate.

5. The simulated projectile auxiliary assembly mechanism according to claim 3, characterized in that: Also included are four casters mounted below the second plate.

6. The simulated projectile auxiliary assembly mechanism according to claim 3, characterized in that: Also included is a first handle extending outwardly from the second plate.

7. The simulated projectile auxiliary assembly mechanism according to claim 1, characterized in that: The bracket is equipped with a second grip.

8. The simulated projectile auxiliary assembly mechanism according to claim 1, characterized in that: The end of the screw rod that contacts the simulated bullet is provided with a rubber head.

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