Integrated fixed-wing aircraft covering cloth with quick release function

Abstract

The utility model belongs to the technical field of aircraft covering cloth, and particularly relates to an integrated fixed-wing aircraft covering cloth with a quick release function, which is characterized in that the covering cloth is of an integrated bilateral symmetry structure, a radome is arranged on the corresponding tail side, the covering cloth covers the top of a fixed-wing aircraft from the head to the tail, and the left side and the right side of the covering cloth cover the belly downwards to be spliced and connected at the belly; the covering cloth located on the fixed wing is covered by the fixed wing downwards from front to back and is spliced and connected below the fixed wing, and a lower splicing seam of the fixed wing extends downwards to the splicing position of the belly; air hole buckles are arranged at the splicing positions and connected through elastic hook rings. Compared with the prior art, the covering cloth has the advantages that the covering cloth is of an integrated structure, can be well attached to the appearance of a fixed-wing aircraft and cover an aircraft body, wings, an antenna and other exposed devices, has more sewing interfaces, is more attached, and is simple in structure and light in weight; the covering cloth can be curled and arranged after being unfolded, storage is convenient, practicability is high, and application and popularization are facilitated.

Description

Technical Field

[0001] This utility model belongs to the field of aircraft fabric technology, and particularly relates to an integrated fixed-wing aircraft fabric with quick-release function. Background Technology

[0002] Aircraft tarpaulins are ground protection devices that provide protective functions. While an aircraft is parked on the ground, ground crew need to cover its surface with an aircraft tarpaulin to reduce damage to the aircraft or equipment from ultraviolet rays, rain, snow, and dust. When installing the tarpaulin, it is required to effectively cover the main parts of the aircraft and secure it firmly, while also considering ease of operation for ground crew.

[0003] Chinese utility model patent application number 202021365395.2 discloses a fixed-wing aircraft cover structure, including a nose cover, a fuselage cover, and a tail cover. The nose cover and fuselage cover form overlapping portions at their connections, and the fuselage cover and tail cover also form overlapping portions. The overlapping portions have a fastening structure that prevents lateral sliding between the two covers and ensures they remain overlapping and connected. While the above-mentioned aircraft cover structures meet usage requirements, the use of a split structure to ensure the cover fits snugly against the aircraft surface results in drawbacks such as high weight, complex structure, and cumbersome operation. Furthermore, the aforementioned covers do not consider covering exposed equipment such as antennas on the aircraft surface, thus failing to provide satisfactory protection. Utility Model Content

[0004] The purpose of this invention is to provide an integrated fixed-wing aircraft cover with quick-release function, overcoming the shortcomings of the existing technology. The cover adopts an integrated structure, which simplifies the structure. All connection and fixing positions are located at the lower part of the aircraft, which meets the functions of quick installation, disassembly and storage of the cover, and is suitable for the daily use of fixed-wing aircraft for covering and protection.

[0005] To achieve the above objectives, this utility model employs the following technical solution:

[0006] A one-piece fixed-wing aircraft cover with quick-release function. The cover is a one-piece symmetrical structure with an antenna radome on the tail side. After the cover covers the top of the fixed-wing aircraft from head to tail, the left and right sides wrap downwards and are spliced ​​together at the belly of the aircraft. The cover on the fixed wing wraps downwards from the front and rear of the fixed wing and is spliced ​​together below the fixed wing. The splicing seam under the fixed wing extends downwards to the splicing point at the belly of the aircraft. All splicing points are provided with eyelets and are connected by elastic hooks.

[0007] Furthermore, the elastic hook is a universal connector consisting of two quick-release hooks connected by an elastic strap.

[0008] Furthermore, the covering fabric is made by sewing together multiple pieces of fabric cut from a template, with the seams having a double-quilted structure.

[0009] Furthermore, the covering is made of a single layer of silver-coated waterproof polyester fabric.

[0010] Furthermore, the radome is a prefabricated component, and the base of the radome is connected to the tail side lining by sewing. The internal space of the radome matches the size of the antenna.

[0011] Furthermore, the quick-release hook is an automatic locking rock climbing hook, and the surface of the quick-release hook is covered with a rubber layer.

[0012] Furthermore, the elastic strap is a closed loop.

[0013] Compared with the prior art, the beneficial effects of this utility model are:

[0014] 1) The fabric has an integrated structure, which can fit the shape of the fixed-wing aircraft well and cover the fuselage, wings and exposed equipment such as antennas. It has more sewing interfaces, fits better, and has a simple structure and is lightweight.

[0015] 2) Once the fabric is unfolded, it can be rolled up and organized for easy storage;

[0016] 3) The elastic straps with quick-release function can moderately tighten the fabric, making the fabric fit tightly against the aircraft surface and reducing the risk of skin tearing or damage caused by wind resistance.

[0017] 4) The elastic straps are connected to quick-release hooks at both ends, and the connection and fixing positions are all located at the bottom of the aircraft, which facilitates the installation and removal by ground staff, improves the work efficiency of removing and installing the aircraft cover, and thus ensures the frequency of aircraft field operations. The overall structure is simple, practical and suitable for widespread application. Attached Figure Description

[0018] Figure 1 This is a schematic diagram of the planar unfolded structure of an embodiment of this utility model;

[0019] Figure 2 This is a schematic diagram of the usage state of an embodiment of this utility model;

[0020] Figure 3 yes Figure 2 The side-tilt view shows the location of the connection and fixing point;

[0021] Figure 4 This is a schematic diagram of the fabric splicing and connection state in an embodiment of this utility model.

[0022] In the picture: 1-covering cloth, 2-elastic hook and loop, 3-eyelet buckle, 4-elastic strap, 5-quick release hook and loop, 6-antenna cover, 7-aircraft, 8-fixed wing. Detailed Implementation

[0023] The technical solution of this utility model will be clearly and completely described below with reference to specific embodiments. Obviously, the described embodiments are some embodiments of this utility model, but not all embodiments.

[0024] To more clearly illustrate the specific embodiments of this utility model or the technical solutions in the prior art, the specific embodiments used in the description of the specific embodiments or the prior art will be briefly introduced below. Obviously, the specific embodiments described below are some embodiments of this utility model. For those skilled in the art, other specific embodiments can be obtained based on these specific embodiments without creative effort.

[0025] The components of the present invention described and shown in the specific embodiments herein can be arranged and designed in numerous different configurations. Therefore, the following detailed description of the embodiments of the present invention provided in the specific embodiments is not intended to limit the scope of the claimed invention, but only to illustrate selected embodiments of the invention.

[0026] See Figures 1-4 This utility model discloses a schematic diagram of an embodiment of an integrated fixed-wing aircraft cover with quick-release function. The cover 1 is an integrated left-right symmetrical structure. An antenna cover 6 is provided on the tail side. The cover 1 covers the top of the fixed-wing aircraft 7 from head to tail, and the left and right sides wrap downwards and are spliced ​​together at the belly of the aircraft. The cover 1 on the fixed wing 8 wraps downwards from the front and back of the fixed wing 8 and is spliced ​​together below the fixed wing 8. The splicing seam of the fixed wing 8 extends downwards to the splicing point of the belly. Each splicing point is provided with an eyelet buckle 3 and is connected by an elastic hook 2.

[0027] The elastic hook 2 is a universal connector consisting of two quick-release hooks 5 connected by an elastic strap 4. The elastic strap 4 is a closed loop, and the two-layer structure provides more stable elasticity than a single-layer structure. The quick-release hook 5 is an automatic locking climbing hook, allowing for quick installation and removal. The surface of the quick-release hook 5 is covered with a rubber layer to prevent the metal quick-release hook 5 from scratching the paint film on the aircraft surface.

[0028] Fabric cover 1 is made of a single layer of silver-coated waterproof polyester fabric, which has strong UV protection and high tensile strength. Fabric cover 1 is made by sewing together multiple pieces of fabric cut from a pattern, with double-stitched seams. Antenna radome 6 is a prefabricated component. The base of antenna radome 6 is connected to fabric cover 1 on the tail side of the machine by sewing, and the internal space of antenna radome 6 matches the size of the antenna.

[0029] In use, the tarpaulin 1 is unfolded and placed on the surface of the aircraft. Then, the elastic straps 2 are connected to the eyelet buckles 3, and the tarpaulin is securely fixed at the lower part of the fuselage, the side of the fuselage, and the lower part of the fixed wing using several elastic hooks 2. The connection and fixing positions are all located at the lower part of the aircraft, which facilitates the operation of airport service personnel and meets the functions of quick installation, disassembly, and storage of the tarpaulin. It is suitable for the daily use of fixed-wing aircraft for covering and protection requirements.

[0030] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A one-piece fixed-wing aircraft cover with quick-release function, characterized in that, The cover is a one-piece symmetrical structure with an antenna cover on the tail side. The cover covers the top of the fixed-wing aircraft from head to tail, and then the left and right sides wrap downwards and are spliced ​​together at the belly of the aircraft. The cover on the fixed wing wraps downwards from the front and rear of the fixed wing and is spliced ​​together below the fixed wing. The splicing seam under the fixed wing extends downwards to the splicing point on the belly of the aircraft. All splicing points are equipped with eyelets and are connected by elastic hooks.

2. The integrated fixed-wing aircraft cover with quick-release function according to claim 1, characterized in that, The elastic hook and loop is a universal connector consisting of two quick-release hooks connected by an elastic strap.

3. The integrated fixed-wing aircraft cover with quick-release function according to claim 1, characterized in that, The covering fabric is made by sewing together multiple pieces of fabric cut from a template, with the seams having a double-quilted structure.

4. The integrated fixed-wing aircraft cover with quick-release function according to claim 3, characterized in that, The covering fabric is made of a single layer of silver-coated waterproof polyester fabric.

5. The integrated fixed-wing aircraft cover with quick-release function according to claim 1, characterized in that, The radome is a prefabricated component. The base of the radome is connected to the tail side lining by sewing. The internal space of the radome matches the size of the antenna.

6. The integrated fixed-wing aircraft cover with quick-release function according to claim 2, characterized in that, The quick-release hook is an automatic locking rock climbing hook, and the surface of the quick-release hook is covered with a rubber layer.

7. The integrated fixed-wing aircraft cover with quick-release function according to claim 2, characterized in that, The elastic strap is a closed loop.

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