Airplane external equipment loading adaptation device

Abstract

The utility model discloses an aircraft external equipment loading adaptation device, which belongs to the field of aircraft equipment storage and loading, and comprises slide rails, connecting seats, reinforcing welding plates and a bottom plate, the slide rails are used in groups and are welded into a whole through the bottom plate, a plurality of groups of slide rails are welded into a whole through the reinforcing welding plates, the bottoms of the slide rails are screwed with the connecting seats, and the positions of the connecting seats are adjustable. Rapid connection with an aircraft missile hanging vehicle is achieved through the connecting base, and the missile hanging vehicle rapidly ascends and descends to be in butt joint with a sliding rail in a square cabin. The launching device lifting device is simple and practical in structure, solves the problems that in the prior art, a launching device can not be pushed into a cabin to be stored quickly in a labor-saving mode due to the fact that the launching device is lifted completely through manpower, has high practicability, convenience, accuracy and safety, and meanwhile can reduce safety risks caused by accidental falling due to inaccurate lifting and butt joint of operators and overweight misoperation.

Description

Technical Field

[0001] This utility model belongs to the field of aircraft equipment storage and loading, and particularly relates to an aircraft external equipment loading adapter, specifically an adapter for a fast and efficient aircraft external equipment loading container. Background Technology

[0002] After the various types of launchers of a certain type of aircraft are removed from the aircraft, they need to be stored in a container. Because the launchers are heavy, numerous, and the container is tall, the current method of manually lifting the launchers into the military container requires multiple people to work together to push the launchers into the container. This operation is complicated, time-consuming, and labor-intensive, and cannot be done quickly, labor-savingly, efficiently, or safely. Utility Model Content

[0003] This utility model provides an aircraft external equipment loading adapter that meets relevant requirements. It can be quickly locked in place with existing bomb-carrying vehicles. The trolley holding the launch device is pushed into the adapter, and the launch device is connected to the slide rail inside the container by lifting the bomb-carrying vehicle, which can achieve the purpose of quickly and labor-savingly pushing the launch device into the container.

[0004] To achieve the above objectives, the technical solution adopted by this utility model is as follows:

[0005] An aircraft external equipment loading adapter device, the loading adapter device including a slide rail 1, a connecting seat 2, a reinforcing welded plate 3, and a base plate 4.

[0006] The slide rails 1 are used in pairs symmetrically, and the bottom of each pair is welded together by the base plate 4. The lower part of the slide rail 1 is provided with a strip hole for installing the connecting seat 2; multiple sets of slide rails 1 are welded together by reinforcing welding plates 3.

[0007] The connecting seat 2 includes a connecting seat base 2-1, a polyurethane pad 2-2, a connecting seat bottom plate 2-3, and connecting seat stiffeners 2-4. The connecting seat bottom plate 2-3 is U-shaped with mounting holes on both sides for installation with the strip-shaped holes at the bottom of the slide rail 1. Three connecting seat stiffeners 2-4 are welded inside the connecting seat bottom plate 2-3 for reinforcement. The bottom has mounting holes for installing the connecting seat base 2-1. The connecting seat base 2-1 is a strip-shaped base with an n-shaped cross-section. It is used in pairs and arranged parallel to each other at the bottom of the connecting seat bottom plate 2-3. The top surface has mounting holes, and the bottom of the groove has polyurethane pads 2-2 for connection with the connecting seat bottom plate 2-3 by bolts. After installation, the connecting seat base 2-1 is parallel to the slide rail 1. The two side walls of the connecting seat base 2-1 have bolt holes for fixed connection with the aircraft bomb loading vehicle.

[0008] The beneficial effects of this utility model are as follows: This utility model has a simple and practical structure, which solves the problem that the existing technology cannot quickly and effortlessly push the launching device into the cabin for storage by relying entirely on manual lifting. It has high practicality, convenience, accuracy and safety, and can also reduce the safety risks caused by inaccurate lifting and docking by the operator, excessive weight and improper operation leading to accidental drop. Attached Figure Description

[0009] Figure 1 This is a three-dimensional schematic diagram of the overall structure of this utility model;

[0010] Figure 2 These are the three views of this utility model, wherein (a) is the front view, (b) is the side view, and (c) is the top view;

[0011] Figure 3 Here are the three views of the slide rail, where (a) is the front view, (b) is the side view, and (c) is the top view;

[0012] Figure 4 This is a 3D schematic diagram of the slide rail;

[0013] Figure 5 The three views of the connector are shown, where (a) is the front view, (b) is the side view, and (c) is the top view.

[0014] Figure 6 This is a three-dimensional schematic diagram of the connector.

[0015] Figure 7 The three views of the base of the connector are shown, where (a) is the front view, (b) is the side view, and (c) is the top view.

[0016] Figure 8 This is a three-dimensional schematic diagram of the connector base;

[0017] Figure 9 This is a schematic diagram of a polyurethane pad, where (a) is the front view and (b) is the side view;

[0018] Figure 10 The three views of the base plate of the connecting seat are shown, where (a) is the front view, (b) is the side view, and (c) is the top view.

[0019] Figure 11 To enhance the schematic diagram of the welding plate, (a) is the front view and (b) is the side view;

[0020] Figure 12 This is a schematic diagram of the base plate, where (a) is the front view and (b) is the top view;

[0021] In the diagram: 1. Slide rail, 2. Connecting seat, 2-1. Connecting seat base, 2-2. Polyurethane pad, 2-3. Connecting seat bottom plate, 2-4. Connecting seat stiffener, 3. Reinforcing welded plate, 4. Base plate. Detailed Implementation

[0022] To make the objectives, technical solutions, and advantages of this utility model clearer, the specific embodiments of this utility model will be described in detail below.

[0023] An aircraft external equipment loading adapter device includes a slide rail 1, a connecting seat 2, a reinforcing welded plate 3, and a base plate 4, such as... Figure 1 and Figure 2 .

[0024] like Figure 3 and Figure 4 The slide rails 1 are used in pairs symmetrically, and the bottoms of the two pairs are welded together as one piece through the base plate 4 (e.g. Figure 12 The lower part of the slide rail 1 is provided with a slot for installing the connecting seat 2; the two sets of a total of 4 slide rails 1 are welded together as one piece by a reinforcing welding plate 3 (e.g. Figure 11 ).

[0025] like Figure 5 and Figure 6 The connecting seat 2 includes a connecting seat base 2-1, a polyurethane pad 2-2, a connecting seat bottom plate 2-3, and a connecting seat stiffener 2-4; the connecting seat bottom plate 2-3 is generally U-shaped (e.g., Figure 10 The slide rail 1 has mounting holes on both sides for installation via M10 hexagonal head bolts that mate with the strip holes at its lower part. The mounting position can be adjusted. Three connecting seat stiffeners 2-4 are welded inside the connecting seat base plate 2-3 for reinforcement. Mounting holes are provided at the bottom for installing the connecting seat base 2-1. The connecting seat base 2-1 is a strip base with an n-shaped cross-section (e.g., ...). Figure 7 and Figure 8 They are used in pairs and arranged parallel to each other at the bottom of the connecting seat base plate 2-3. Mounting holes are made on their top surfaces, and polyurethane pads 2-2 are installed at the bottom of the groove (e.g., Figure 9 The connector is connected to the base plate 2-3 of the connecting seat using M5 socket head cap screws. After installation, the base plate 2-1 of the connecting seat is parallel to the slide rail 1. Bolt holes are made on both sides of the base plate 2-1 of the connecting seat for fixing with the aircraft bomb loading vehicle using M10 hex head bolts. The bomb loading vehicle can be quickly lifted and lowered to dock with the slide rail inside the container, which can quickly, accurately and labor-savingly pick up and put down the trolley loaded with external equipment inside the container, avoiding the need for manual lifting of the trolley. The trolley moves forward on the slide rail, achieving the purpose of speed, accuracy, labor saving and safety.

Claims

1. An aircraft external equipment loading adapter, characterized in that, The loading adapter includes a slide rail (1), a connecting seat (2), and a base plate (4); The slide rails (1) are used in pairs symmetrically, and the bottom of each pair is welded together by the base plate (4). The lower part of the slide rail (1) is provided with a strip hole for installing the connecting seat (2). The connecting seat (2) includes a connecting seat base (2-1), a connecting seat bottom plate (2-3), and a connecting seat stiffener (2-4). The connecting seat bottom plate (2-3) is U-shaped in general, with mounting holes on both sides for installation with the strip holes at the bottom of the slide rail (1). The bottom has mounting holes for installing the connecting seat base (2-1). The connecting seat base (2-1) is a strip base with an n-shaped cross section. They are used in pairs and are arranged in parallel at the bottom of the connecting seat bottom plate (2-3). The top surface has mounting holes for connection with the connecting seat bottom plate (2-3). After installation, the connecting seat base (2-1) is parallel to the slide rail (1). The connecting seat base (2-1) has bolt holes on both sides for fixed connection with the aircraft bomb carrier.

2. The aircraft external equipment loading adapter according to claim 1, characterized in that, Multiple sets of slide rails (1) are welded together as one unit by reinforcing welding plates (3).

3. The aircraft external equipment loading adapter according to claim 1, characterized in that, The connecting seat base plate (2-3) is internally welded with three connecting seat stiffeners (2-4) to achieve a reinforcement effect.

4. The aircraft external equipment loading adapter according to claim 1, characterized in that, A polyurethane pad (2-2) is installed at the bottom of the groove of the mounting connector base (2-1).

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