Supporting pillow special for airplane external equipment

Abstract

The utility model discloses a special supporting pillow for airplane external equipment, which belongs to the field of airplane equipment storage and loading and comprises two front plates arranged in parallel, an inner plate, an upper plate, side plates and a reinforcing plate are connected and supported between the two front plates to improve the supporting strength, the upper plate serves as a supporting profile and is provided with a polyurethane pad, and the upper plate is provided with a lower plate. Bolt connecting plates are installed on the ground of the two front plates so that the two front plates can be fixed to an externally-hung equipment trolley, and stainless steel pin shafts are arranged on the two sides of the two front plates so that binding bands can be installed to fasten externally-hung equipment. The device is simple and practical in structure, solves the problems that in the prior art, rapid and labor-saving placement cannot be achieved, firm and stable placement of external equipment cannot be guaranteed, the device is prone to abrasion, and the device is heavy, has high practicability, convenience, accuracy and safety, and meanwhile can reduce safety risks caused by accidental falling.

Description

Technical Field

[0001] This utility model belongs to the field of aircraft equipment storage and loading, and relates to a special support pillow for aircraft external equipment, specifically a support pillow for storing a certain external equipment of an aircraft. Background Technology

[0002] After a certain type of launcher from a certain aircraft is removed from the aircraft, it needs to be stored in a container or on a rack. Current storage methods for external equipment are simple, typically involving placing it directly on a rack. However, due to the irregular size and shape of the external equipment, it is prone to falling and cannot be placed quickly and effortlessly, failing to guarantee secure, stable, and wear-resistant storage. Therefore, a custom-designed support is needed, which can be installed on a container trolley or fixed rack to ensure secure, stable, and wear-resistant storage of the external equipment. Utility Model Content

[0003] This utility model provides a special support pillow for aircraft external equipment, which can be installed on a container trolley or fixed frame to ensure that the external equipment is secure, stable and not easily worn when stored.

[0004] The present invention adopts the following technical solution:

[0005] A special support pillow for aircraft external equipment, the special support pillow includes an inner panel 1, a front panel 2, an upper panel 5, a side panel 6, a reinforcing plate 7, and a bolt connection plate 8.

[0006] The front plate 2 has two identical structures, with a large square hole in the middle and a concave shape at the top as a support surface. The two front plates 2 are placed opposite each other, and the inner plate 1, the upper plate 5 and the side plate 6 are fixedly supported between the two front plates 2.

[0007] The upper plate 5 is a plate surface bent according to the upper surface of the front plate 2. It is fixedly installed between the upper edges of the two front plates 2 as the main part of the supporting surface. At the position where it contacts the supported external equipment, polyurethane pads 3 are installed using cross countersunk screws to avoid abrading the paint surface of the aircraft external equipment.

[0008] The inner plate 1 is a plate surface bent according to the large square hole in the middle of the front plate 2, and is fixedly installed between the two front plates 2 around the edge of the large square hole.

[0009] The side plate 6 is a strip plate, and there are two of them, which are fixedly installed between the two sides of the two front plates 2 respectively.

[0010] Several reinforcing plates 7 are provided and are fixedly installed between the two front plates 2 as needed to increase the support strength.

[0011] Two bolt connection plates 8 are provided and are installed in parallel at the bottom of the two front plates 2, used to fix the entire special support pillow to the external equipment trolley by bolts.

[0012] The two front plates 2 have corresponding pin holes on their upper sides for inserting stainless steel pins 4 to install straps to secure the external equipment.

[0013] The special support pillow is made of 7-series aerospace aluminum, which ensures strength while reducing weight.

[0014] At least two of the special support pillows are used simultaneously, and the special support pillows are arranged in parallel.

[0015] The beneficial effects of this utility model are:

[0016] This utility model has a simple and practical structure, which solves the problems of existing technologies such as the inability to place quickly and effortlessly, the inability to ensure the stable and secure placement of external devices, easy wear and tear, and heavy weight. It has high practicality, convenience, accuracy and safety, and can also reduce the safety risks caused by accidental drops. Attached Figure Description

[0017] Figure 1 This is a schematic diagram of the overall structure of the present invention, wherein (a) is a three-dimensional structural diagram and (b) is a schematic diagram of the combination of various components;

[0018] Figure 2 This is a schematic diagram of the present invention installed on an external equipment trolley;

[0019] Figure 3 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;

[0020] Figure 4 This is a schematic diagram of the inner panel, where (a) is the front view and (b) is the side view;

[0021] Figure 5 This is a schematic diagram of the front panel, where (a) is the front view and (b) is the side view;

[0022] Figure 6 This is a schematic diagram of a polyurethane pad, where (a) is the front view and (b) is the side view;

[0023] Figure 7 This is a schematic diagram of the upper plate, where (a) is the front view and (b) is the side view;

[0024] Figure 8 This is a schematic diagram of the side panel, where (a) is the front view and (b) is the side view;

[0025] Figure 9 This is a schematic diagram of the reinforcing plate, where (a) is the front view and (b) is the side view;

[0026] Figure 10 This is a schematic diagram of a bolted connection plate, where (a) is the front view and (b) is the side view;

[0027] In the diagram: 1 Inner plate, 2 Front plate, 3 Polyurethane pad, 4 Stainless steel pin, 5 Top plate, 6 Side plate, 7 Reinforcing plate, 8 Bolt connection plate. Detailed Implementation

[0028] 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.

[0029] A special support pillow for aircraft external equipment, comprising an inner panel 1, a front panel 2, an upper panel 5, a side panel 6, a reinforcing plate 7, and a bolt-connecting plate 8, as shown below. Figure 1 and Figure 3 .

[0030] like Figure 5 The front plate 2 has two identical structures. It is a square plate with a large square hole in the middle and a concave shape resembling a deer antler at the top as a support surface. The specific shape of the support surface is set according to the support position of the external device being supported. The two front plates 2 are placed opposite each other, and the inner plate 1, the upper plate 5 and the side plate 6 are fixedly supported between the two front plates 2.

[0031] like Figure 7 The upper plate 5 is a plate surface bent according to the upper surface of the front plate 2, and is fixedly installed between the upper edges of the two front plates 2, serving as the main part of the supporting surface. A polyurethane pad 3 is installed at the contact point with the supported external equipment using Phillips head countersunk screws. Figure 6 To avoid damaging the paint on the aircraft's external equipment.

[0032] like Figure 4 The inner plate 1 is a plate surface bent according to the large square hole in the middle of the front plate 2, and is fixedly installed between the two front plates 2 around the large square hole.

[0033] like Figure 8 The side plate 6 is a strip plate, and there are two of them, which are fixedly installed between the two sides of the two front plates 2.

[0034] like Figure 9 Several reinforcing plates 7 are provided and are fixedly installed between the two front plates 2 as needed to increase the support strength.

[0035] like Figure 10 Two bolt connection plates 8 are provided and are installed in parallel at the bottom of the two front plates 2, which are used to fix the entire special support pillow to the external equipment trolley by bolts.

[0036] The two front plates 2 have corresponding pin holes on their upper sides for inserting stainless steel pins 4 to install straps to secure the external equipment.

[0037] At least two of the aforementioned special support pillows are used simultaneously, arranged in parallel, and installed on an external equipment trolley to achieve the goals of speed, precision, labor-saving, safety, and stability. Figure 2 .

Claims

1. A special support pillow for aircraft external equipment, characterized in that, The special support pillow includes an inner panel (1), a front panel (2), an upper panel (5), a side panel (6), and a bolt connection plate (8); The front plate (2) has two identical structures. The middle part has a large square hole and the upper end has a concave shape as a support surface. The two front plates (2) are placed opposite each other, and the inner plate (1), the upper plate (5) and the side plate (6) are fixedly supported between the two front plates (2). The upper plate (5) is a plate surface bent according to the upper surface of the front plate (2), and is fixedly installed between the upper edges of the two front plates (2) as the main part of the supporting surface; The inner plate (1) is a plate surface bent according to the large square hole in the middle of the front plate (2), and is fixedly installed between the two front plates (2) around the edge of the large square hole; The side plate (6) is a strip plate, and there are two of them, which are fixedly installed between the two sides of the two front plates (2); Two bolt connection plates (8) are provided and are installed in parallel at the bottom of the two front plates (2) to fix the entire special support pillow to the external equipment trolley.

2. The special support pillow for aircraft external equipment according to claim 1, characterized in that, A polyurethane pad (3) is installed at the position where the upper plate (5) contacts the external equipment it supports.

3. A special support pillow for aircraft external equipment according to claim 1, characterized in that, A reinforcing plate (7) is fixedly installed between the two front plates (2) as needed to increase the support strength.

4. A special support pillow for aircraft external equipment according to claim 1, characterized in that, The two front plates (2) are provided with pin holes on both sides of the upper part for inserting stainless steel pins (4) to install straps to fasten the external equipment.

5. A special support pillow for aircraft external equipment according to any one of claims 1-4, characterized in that, The special support pillow is made of 7-series aerospace aluminum welded together.

6. A special support pillow for aircraft external equipment according to any one of claims 1-4, characterized in that, At least two of the special support pillows are used simultaneously, and the special support pillows are arranged in parallel.

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