Long-service-life sun-proof covering cloth for military aircrafts

Abstract

The utility model discloses a long-service-life sun-proof covering cloth for a military plane, which relates to the technical field of plane covering cloth and comprises a sun-proof covering cloth with a protective lining at the bottom. The structure reinforcing line is fixedly connected between the sunscreen covering cloth and the protective lining; the multiple sets of supporting mechanisms are arranged, and the multiple sets of supporting mechanisms are all arranged on the protection lining and are evenly distributed; the number of the positioning suction cups is multiple, and each positioning suction cup is fixedly connected to the corresponding supporting mechanism. According to the long-service-life sun-resistant covering cloth for the military plane, the overall structure of the covering cloth can be strengthened through the use of the structural reinforcing lines, the covering cloth is not prone to being torn in the use process, the use effect is guaranteed, meanwhile, the use life is prolonged, the covering cloth can be easily and conveniently positioned on the surface of the plane through the use of the positioning suction cups, and the service life is prolonged. And the stability in the using process is guaranteed, accidental falling in the using process is avoided, and the working efficiency is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of aircraft covers, in particular to a high-life sun-proof cover for military aircraft. Background Art

[0002] The sun-proof cover for military aircraft, also known as the dark cabin cover, is mainly used in the training and teaching of pilots. The main function of this cover is to create an environment for flight trainees to fly only relying on flight instruments by blocking the windshield of the aircraft. In this environment, flight trainees can exercise and improve their instrument flight skills, which are important capabilities necessary for pilots when flying in complex weather, at night, and over the sea.

[0003] Generally speaking, the sun-proof cover for military aircraft plays a key role in the training of pilots, helping pilots improve their instrument flight skills to adapt to various complex flight environments.

[0004] The authorized announcement number "CN220721381U" records "an aircraft cover with waterproof and sun-proof functions, including a cover and binding straps. The cover has an inner layer and an outer layer. A plurality of support bodies are arranged on the inner layer of the cover. The cover abuts against the fuselage of the aircraft through the support bodies. A plurality of symmetrically arranged binding straps are arranged on both sides of the cover. The cover is detachably tied to the fuselage of the aircraft through the binding straps. Using the aircraft cover of the utility model, it not only has waterproof and sun-proof functions, but also can protect the aircraft skin coating, is convenient to carry and operate, can meet the needs of different levels of personnel, is especially suitable for outfield work support, greatly improves work efficiency, has a simple overall structure, strong practicability, and is suitable for popularization and application".

[0005] The above patent has waterproof and sun-proof functions, can also protect the aircraft skin coating, is convenient to carry and operate, can meet the needs of different levels of personnel, is especially suitable for outfield work support, and greatly improves work efficiency. Its overall structure is simple and has strong practicability, suitable for popularization and application. However, its structural strength is not high, and it is easy to tear during use. At the same time, during use, due to the material of the cover, it is easy to slide off, affecting the use effect. Content of the Utility Model

[0006] The utility model provides a high-life sun-proof cover for military aircraft. By using structural strengthening lines, the overall structure of the cover can be strengthened, so that it will not be easily torn during use, ensuring the use effect and at the same time increasing the service life. By using positioning suckers, the cover can be simply positioned on the surface of the aircraft, ensuring stability during use, avoiding accidental detachment during use, and improving work efficiency.

[0007] To achieve the above object, the utility model is realized by the following technical solutions: A sun protection cover for military aircraft with high service life, comprising:

[0008] A sun protection cover with a protective lining at the bottom;

[0009] A structural reinforcement line, which is fixedly connected between the sun protection cover and the protective lining;

[0010] A support mechanism, which has multiple groups. Multiple groups of the support mechanisms are all arranged on the protective lining and are evenly distributed;

[0011] Positioning suckers, and there are multiple of them. Each positioning sucker is fixedly connected to each group of support mechanisms; and

[0012] A traction mechanism, which has four groups. The four groups of traction mechanisms are respectively arranged at the four corners of the sun protection cover.

[0013] Further, each group of the support mechanisms includes a support column and a buffer spring. The support column is fixedly connected to the bottom of the protective lining, and the buffer spring is fixedly connected inside the support column.

[0014] Further, each group of the traction mechanisms includes a traction connection buckle and a pull rope. The traction connection buckle is fixedly connected to the sun protection cover, and the pull rope is installed on the traction connection buckle.

[0015] Further, a heat insulation aerogel is installed between the sun protection cover and the protective lining, and the heat insulation aerogel is wrapped around the structural reinforcement line.

[0016] Further, a plurality of force-bearing connection points are fixedly connected to the structural reinforcement line, and each force-bearing connection point is arranged on the top of each support column.

[0017] Further, a waterproof adhesion layer is attached to the top of the sun protection cover.

[0018] The utility model provides a sun protection cover for military aircraft with high service life. It has the following beneficial effects:

[0019] (1). For the sun protection cover for military aircraft with high service life, by using the structural reinforcement line, the overall structure of the cover can be strengthened, so that it will not be easily torn during use, ensuring the use effect and at the same time increasing the service life.

[0020] (2). For the sun protection cover for military aircraft with high service life, by using the positioning suckers, the cover can be simply positioned on the surface of the aircraft, ensuring the stability during use, avoiding accidental detachment during use, and improving the work efficiency. Description of the Drawings

[0021] Figure 1 This is the sectional exploded view of the present utility model;

[0022] Figure 2 This is the partial sectional view of the present utility model;

[0023] Figure 3 This is the three-dimensional view of the present utility model.

[0024] In the figure: 1. Sunscreen cloth; 2. Heat-insulating aerogel; 3. Structure strengthening line; 4. Waterproof adhesion layer; 5. Traction connection buckle; 6. Pulling rope; 7. Positioning sucker; 8. Support column; 9. Buffer spring; 10. Force-bearing connection point; 11. Protection lining. Specific implementation manner

[0025] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described with reference to the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present utility model.

[0026] Please refer to Figures 1-3 , the present utility model provides a technical solution: a high-life sunscreen cloth for military aircraft, including:

[0027] A sunscreen cloth 1 with a protection lining 11 provided at the bottom;

[0028] A structure strengthening line 3, and the structure strengthening line 3 is fixedly connected between the sunscreen cloth 1 and the protection lining 11;

[0029] A support mechanism, which has multiple groups, and multiple groups of support mechanisms are all arranged on the protection lining 11 and are evenly distributed;

[0030] Positioning suckers 7, and there are multiple of them, and each positioning sucker 7 is fixedly connected to each group of support mechanisms; and

[0031] A traction mechanism, which has four groups, and the four groups of traction mechanisms are respectively arranged at the four corners of the sunscreen cloth 1.

[0032] In this implementation: The protective inner lining 11 serves to protect the internal structure and materials, preventing wear and tear. It is made of wear-resistant and tear-resistant materials to ensure that the sunshade cloth 1 can still maintain a good appearance and performance during long-term use. It has a certain anti-slip performance to ensure that the sunshade cloth 1 can fit tightly against the windshield during installation. The sunshade cloth 1 is mainly responsible for blocking the direct irradiation of ultraviolet rays and sunlight. It is made of materials with high sun protection performance and is coated with a special sun protection coating to improve its ability to reflect and absorb sunlight. Its color is usually dark to better absorb heat and reduce light penetration. The structural reinforcement line 3 is inclined inside the structure to improve the overall structural strength, ensure the use effect, and extend the service life. The positioning suction cup 7 can be used for simple positioning on the surface of the aircraft to prevent slipping during use.

[0033] Specifically, each set of support mechanisms includes a support column 8 and a buffer spring 9. The support column 8 is fixedly connected to the bottom of the protective inner lining 11, and the buffer spring 9 is fixedly connected inside the support column 8.

[0034] In this embodiment: The support column 8 is made of rubber and has flexible mobility. The overall buffering is increased through the buffer spring 9 to prevent the protective inner lining 11 from directly contacting the aircraft surface and improve the use effect.

[0035] Specifically, each set of traction mechanisms includes a traction connection buckle 5 and a pull rope 6. The traction connection buckle 5 is fixedly connected to the sunshade cloth 1, and the pull rope 6 is installed on the traction connection buckle 5.

[0036] In this embodiment: The traction connection buckle 5 and the pull rope 6 cooperate to mainly provide the connection and fixation functions with the aircraft windshield or other components, ensuring the stable connection and use of the sunshade cloth.

[0037] Specifically, a heat-insulating aerogel 2 is installed between the sunshade cloth 1 and the protective inner lining 11, and the heat-insulating aerogel 2 is wrapped around the structural reinforcement line 3.

[0038] In this embodiment: The heat-insulating aerogel 2 mainly plays a role in heat insulation, reducing the heat transfer to the interior of the cabin. By reducing heat transfer, it helps to maintain the temperature stability inside the cabin and improve the comfort of the pilot.

[0039] Specifically, a plurality of force-bearing connection points 10 are fixedly connected to the structural reinforcement line 3, and each force-bearing connection point 10 is located at the top of each support column 8.

[0040] In this embodiment: While increasing the connection between the structural reinforcement lines 3, the force-bearing connection points 10 integrate the support columns 8 with the structure for use.

[0041] Specifically, a waterproof attachment layer 4 is attached to the top of the sunshade cloth 1.

[0042] In this embodiment, the waterproof adhesion layer 4 improves the waterproof property of the sunscreen tarp 1, enhancing its ability to adapt to different environmental and climatic conditions.

[0043] During use, after adjusting the position, the tarp is placed on the aircraft through the positioning suction cups 7 to maintain stability. After completion, through the cooperation of the traction connection buckle 5 and the pull rope 6, the tarp is connected to the aircraft windshield or other components to ensure stable connection and use of the tarp. During the use process, the waterproof adhesion layer 4 improves the waterproof property of the sunscreen tarp 1, and the internal heat-insulating aerogel 2 reduces the heat transfer to the interior of the cabin, maintaining the temperature stability inside the cabin.

[0044] The control method of the present utility model is controlled by manually starting and closing the switch. The wiring diagram of the power element and the power supply are common knowledge in the art, and the present utility model is mainly used to protect mechanical devices. Therefore, the control method and wiring arrangement of the present utility model will not be explained in detail.

[0045] The above is only the preferred specific embodiment of the present utility model, but the protection scope of the present utility model is not limited thereto. Any person skilled in the art within the technical scope disclosed by the present utility model, according to the technical solution of the present utility model and its inventive concept, making equivalent replacements or changes, should be covered by the protection scope of the present utility model.

Claims

1. A long-life sunscreen cover for military aircraft, characterized in that: include: A sunscreen cover (1) with a protective lining (11) at the bottom; A structural reinforcement line (3), wherein the structural reinforcement line (3) is fixedly connected between the sunscreen cover (1) and the protective lining (11); A supporting mechanism, which is provided in multiple groups, wherein the multiple groups of supporting mechanisms are all provided on the protective lining (11), and the multiple groups of supporting mechanisms are evenly distributed; A plurality of positioning suction cups (7) are provided, each of the positioning suction cups (7) being fixedly connected to each set of supporting mechanisms; and The traction mechanism is provided with four groups, and the four groups of traction mechanisms are respectively arranged at the four corners of the sun-proof cover (1).

2. The long-life sunscreen cloth for military aircraft according to claim 1 is characterized in that: Each group of the support mechanisms comprises a support column (8) and a buffer spring (9); the support column (8) is fixedly connected to the bottom of the protective lining (11); and the buffer spring (9) is fixedly connected inside the support column (8).

3. A long-life sunscreen cloth for military aircraft according to claim 2, characterized in that: Each group of the traction mechanisms comprises a traction connection buckle (5) and a pull rope (6); the traction connection buckle (5) is fixedly connected to the sunscreen cover (1), and the pull rope (6) is installed on the traction connection buckle (5).

4. The long-life sunscreen cloth for military aircraft according to claim 3 is characterized in that: A thermal insulation aerogel (2) is installed between the sun protection cover (1) and the protective lining (11), and the thermal insulation aerogel (2) is wrapped on the structural reinforcement line (3).

5. The long-life sunscreen cloth for military aircraft according to claim 4, characterized in that: A plurality of force-bearing connection points (10) are fixedly connected to the structural reinforcement line (3), and each of the force-bearing connection points (10) is arranged at the top of each support column (8).

6. The long-life sunscreen cloth for military aircraft according to claim 5, characterized in that: A waterproof adhesion layer (4) is attached to the top of the sunscreen cloth (1).

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