Fixing tool for aluminum alloy hovercar mechanism part forging

Abstract

The utility model discloses a fixing tool for forging aluminum alloy hovercar mechanism parts, which belongs to the field of fixing tools and comprises a base, a placing plate is arranged on the base, a fixing seat is mounted on the placing plate, and an arc T-shaped groove is arranged on the fixing seat. The arc T-shaped groove is formed in the fixing base and used in cooperation with the sliding block, the fixing plate, the abutting assembly and the pressing assembly, the positions of the abutting assembly and the pressing assembly can be adjusted, adjustment can be conveniently conducted according to the shape of a component, the fixing adaptability is improved, the abutting assembly and the pressing assembly are used in cooperation, multi-direction clamping and fixing can be achieved, and the clamping efficiency is improved. The pressing assembly is installed on the abutting assembly through the locking rotary knob and can move along with the abutting assembly, the adjustment convenience can be guaranteed, the pressing assembly can be rotationally adjusted in the pressing process, the flexibility during component fixing is further improved, meanwhile, the pressing assembly can be rapidly disassembled and replaced, and maintenance is convenient and rapid.

Description

TECHNICAL FIELD

[0001] The utility model relates to the fixed frock field, especially in kind of aluminum alloy flying car mechanism piece forging fixed frock. BACKGROUND

[0002] Aluminum alloy is widely used in aerospace, automobile manufacturing and other fields due to its small density, high specific strength, corrosion resistance and impact resistance and a series of advantages. Aluminum alloy flying car mechanism piece is an important part of the flying car, and the aluminum alloy flying car mechanism piece mainly refers to various structural components made of aluminum alloy materials during the manufacturing process of the flying car. These components are important parts of the flying car and bear important functions such as support, connection and transmission. When the aluminum alloy flying car mechanism piece is processed and forged, some components need to be fixed during processing, so the fixed frock is used.

[0003] The existing fixed frock is used to place the components on the platform and fix them by using the clamping mechanism. However, the existing fixed frock can only be clamped horizontally or vertically, and cannot be fixed in multiple directions at the same time. Moreover, when clamping and fixing horizontally or vertically, the structure for clamping and fixing is fixed and cannot be adjusted according to the shape of the components, so the flexibility and adaptability of the use are general. UTILITY MODEL CONTENT

[0004] The main purpose of the utility model is to provide a kind of aluminum alloy flying car mechanism piece forging fixed frock, it can effectively solve the problems in the background art.

[0005] To achieve the above-mentioned purpose, the technical scheme adopted by the utility model is as follows:

[0006] A kind of aluminum alloy flying car mechanism piece forging fixed frock, including base, the base is equipped with placing plate, the placing plate is installed with fixed seat, and arc T slot is opened in fixed seat, and sliding block is equipped in arc T slot, the upper end of sliding block is installed with abutting assembly, and abutting assembly is installed with pressing assembly.

[0007] Preferably, the fixed seat is arranged in a ring array on the placing plate, the sliding block is provided with a fixed plate, and the fixed plate is provided with a fixed screw, the lower end of the fixed screw abuts on the fixed seat.

[0008] Preferably, the abutting assembly is provided with a locking knob, and the pressing assembly is fixedly installed on the abutting assembly by the locking knob.

[0009] Preferably, the abutting assembly comprises a fixed rod, a movable rod, an abutting rod, an adjusting bolt, a round block and a stud, the fixed rod is fixedly installed on the sliding block, the movable rod is connected to the fixed rod and penetrates the fixed rod, the end of the movable rod is provided with a limiting block, the abutting rod is installed at the end of the movable rod, the adjusting bolt is threadedly connected to the fixed rod, and the round block is fixedly connected with the stud and is installed on the abutting rod.

[0010] Preferably, the pressing assembly comprises a mounting rod, a round hole, a threaded rod and a pressing plate, the round hole is formed in the mounting rod, the mounting rod is installed on the round block of the abutting rod through the round hole, the end of the mounting rod is provided with a threaded hole, the threaded rod is installed in the threaded hole of the mounting rod, and the pressing plate is connected to the lower end of the threaded rod.

[0011] Compared with the prior art, the aluminum alloy flying car component forging fixing tool has the following beneficial effects: the arc T-shaped groove is formed in the fixed seat, the sliding block, the fixed plate, the abutting assembly and the pressing assembly are used in cooperation, the positions of the abutting assembly and the pressing assembly can be adjusted, the adjustment according to the shape of the component is facilitated, the fixing adaptability is increased, the abutting assembly and the pressing assembly are used in cooperation, multi-directional clamping and fixing can be realized, the fixing effect on the component is improved, the pressing assembly is installed on the abutting assembly by means of the locking knob, can move together with the abutting assembly, the adjustment convenience can be ensured, the pressing assembly can be rotated and adjusted during the pressing process, the flexibility during the fixing of the component is further increased, the pressing assembly can be quickly disassembled and replaced, and maintenance is convenient and fast. BRIEF DESCRIPTION OF DRAWINGS

[0012] Figure 1 It is a whole structure schematic view of the utility model;

[0013] Figure 2 It is a structure schematic view of the fixed seat of the utility model;

[0014] Figure 3 It is a structure schematic view of the abutting assembly of the utility model;

[0015] Figure 4 It is a structure schematic view of the pressing assembly of the utility model.

[0016] In the drawing: 1, base; 2, placing plate; 3, fixed seat; 4, arc T-shaped groove; 5, sliding block; 6, fixed plate; 7, abutting assembly; 701, fixed rod; 702, movable rod; 703, abutting rod; 704, adjusting bolt; 705, round block; 706, stud; 8, pressing assembly; 801, mounting rod; 802, round hole; 803, threaded rod; 804, pressing plate; 9, locking knob; 10, fixed screw. DETAILED DESCRIPTION

[0017] In order to make the technical means, creative features, objectives and effects achieved by the present invention easier to understand, the present invention is further described below in conjunction with specific implementation methods.

[0018] like Figures 1-4 As shown, a fixture for forging aluminum alloy flying car components comprises a base 1, with a placement plate 2 mounted on the placement plate 2, a fixing seat 3 mounted on the placement plate 2, and a circular arc T-shaped slot 4 defined in the fixing seat 3. A slider 5 is disposed within the circular arc T-shaped slot 4, with a clamping assembly 7 mounted on the upper end of the slider 5, and a pressing assembly 8 mounted on the clamping assembly 7. The fixing seats 3 are arranged in a circular array on the placement plate 2. The slider 5 is provided with a fixing plate 6, which is provided with a fixing screw 10, the lower end of which abuts the fixing seat 3. The pressing assembly 8 is fixed to the pressing assembly 7 via a locking knob 9. The circular arc T-shaped slot 4 defined in the fixing seat 3 is used in conjunction with the slider 5, the fixing plate 6, the pressing assembly 7, and the pressing assembly 8. The positions of the pressing and pressing assemblies 7 and 8 can be adjusted to suit the shape of the component and enhance the adaptability of the fixing. The fixing seats 3 are distributed in a circular array on the placement plate 2, which can ensure the clamping effect for regular components. At the same time, arc T-shaped grooves 4 are opened. After adjusting the positions of the clamping components 7 and the pressing components 8, they can also provide a fixing effect for irregular components, and are highly adaptable to use.

[0019] When forging aluminum alloy flying car components, for components that require fixed processing, a fixing fixture is used to secure the component. The placement plate 2 is stably placed on the base 1, and the structure for clamping and fixing is set on the placement plate 2. After the component is placed on the placement plate 2, the position of the clamping assembly 7 and the pressing assembly 8 are adjusted according to the shape of the component. During the adjustment process, the fixing screws 10 on the fixing plate 6 are loosened, and the clamping assembly 7 and the pressing assembly 8 are moved. The clamping assembly 7 and the pressing assembly 8 are moved within the arc T-slot 4 on the fixing seat 3 via the slider 5 until the clamping assembly 7 and the pressing assembly 8 are adjusted to the appropriate position. The fixing screws 10 are then turned to secure the slider 5. The clamping assembly 7 and the pressing assembly 8 are then used to secure the component. After the component is secured, the component can be processed. If necessary, a slider 5 with a clamping assembly 7 can be added to the arc T-slot 4 on the fixing seat 3 to improve flexibility and adaptability. The installation of the slider 5 does not affect other structures, making installation and removal convenient and quick.

[0020] By the above embodiment, the abutting assembly 7 comprises a fixed rod 701, a movable rod 702, an abutting rod 703, an adjusting bolt 704, a circular block 705 and a stud 706, the fixed rod 701 is fixedly installed on the sliding block 5, the movable rod 702 is connected to the fixed rod 701 and penetrates through the fixed rod 701, the end of the movable rod 702 is provided with a limiting block, the abutting rod 703 is installed at the end of the movable rod 702, the adjusting bolt 704 is threadedly connected to the fixed rod 701, the circular block 705 is fixedly connected with the stud 706, and the circular block 705 is installed on the abutting rod 703.

[0021] The pressing assembly 8 comprises a mounting rod 801, a circular hole 802, a threaded rod 803 and a pressing plate 804, the circular hole 802 is formed in the mounting rod 801, the mounting rod 801 is installed on the circular block 705 of the abutting rod 703 through the circular hole 802, the end of the mounting rod 801 is provided with a threaded hole, the threaded rod 803 is installed in the threaded hole of the mounting rod 801, and the pressing plate 804 is connected to the lower end of the threaded rod 803.

[0022] It should be noted that the abutting assembly 7 is used in cooperation with the pressing assembly 8, so that multi-directional clamping and fixing can be realized, the fixing effect on the component is improved, the pressing assembly 8 is installed on the abutting assembly 7 by means of the locking knob 9, can move together with the abutting assembly 7, so that the convenience of adjustment can be ensured, the pressing assembly 8 can be rotated and adjusted during the pressing process, the flexibility during the fixing of the component is further increased, and the pressing assembly 8 can be quickly disassembled and replaced, so that the maintenance is convenient and fast.

[0023] After the relative position adjustment of the abutting assembly 7 and the pressing assembly 8 is completed, the movable rod 702 on the fixed rod 701 is moved, the movable rod 702 moves with the abutting rod 703, until the abutting rod 703 abuts against the component, then the adjusting bolt 704 is rotated to abut and fix the abutting rod 703, so that the component is abutted in the horizontal direction. Then the locking knob 9 on the stud 706 is loosened, the mounting rod 801 in the pressing assembly 8 is rotated and adjusted, so that the pressing assembly 8 rotates on the circular block 705, after the adjustment is completed, the locking knob 9 is rotated to fix the pressing assembly 8. Then the threaded rod 803 is rotated, the threaded rod 803 rotates and descends with the pressing plate 804, until the pressing plate 804 presses on the component, so that the component is fixed in the vertical direction. After the whole component is fixed, the processing can be performed.

[0024] The above description describes the use principle, features and beneficial effects of the utility model. According to the above description, the related personnel in the field can understand that the above description does not limit the utility model, and the above embodiment and description describe the basic principle and features of the utility model, under the premise of meeting the utility model concept, the utility model can also be variously changed and improved, and these improvements should fall within the scope of the utility model claimed to be protected.

Claims

1. A fixture for forging aluminum alloy flying car components, comprising a base (1), a placement plate (2) being provided on the base (1), and characterized in that: A fixing seat (3) is installed on the placement plate (2), and a circular arc T-shaped groove (4) is provided on the fixing seat (3), and a slider (5) is provided in the circular arc T-shaped groove (4), and a tightening component (7) is installed on the upper end of the slider (5), and a pressing component (8) is installed on the tightening component (7).

2. The fixing fixture for forging aluminum alloy flying car components according to claim 1, characterized in that: The fixing seats (3) are distributed in a ring array on the placement plate (2); a fixing plate (6) is provided on the slider (5); and a fixing screw (10) is provided on the fixing plate (6); the lower end of the fixing screw (10) abuts against the fixing seat (3).

3. The fixing fixture for forging aluminum alloy flying car components according to claim 2, characterized in that: The pressing assembly (7) is provided with a locking knob (9), and the pressing assembly (8) is fixedly mounted on the pressing assembly (7) via the locking knob (9).

4. The fixing fixture for forging aluminum alloy flying car components according to claim 3, characterized in that: The tightening assembly (7) comprises a fixed rod (701), a movable rod (702), a tightening rod (703), an adjusting bolt (704), a round block (705) and a stud (706), wherein the fixed rod (701) is fixedly mounted on the slider (5), the movable rod (702) is connected to the fixed rod (701), and the movable rod (702) passes through the fixed rod (701), a limit block is provided at the end of the movable rod (702), the tightening rod (703) is mounted on the end of the movable rod (702), the adjusting bolt (704) is threadedly connected to the fixed rod (701), the round block (705) is fixedly connected to the stud (706), and the round block (705) is mounted on the tightening rod (703).

5. The fixing fixture for forging aluminum alloy flying car components according to claim 4, characterized in that: The clamping assembly (8) comprises a mounting rod (801), a circular hole (802), a threaded rod (803) and a pressure plate (804), wherein the circular hole (802) is provided on the mounting rod (801), and the mounting rod (801) is mounted on the round block (705) on the clamping rod (703) through the circular hole (802), a screw hole is provided at the end of the mounting rod (801), and the threaded rod (803) is mounted in the screw hole on the mounting rod (801), and the pressure plate (804) is connected to the lower end of the threaded rod (803).

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