All-weather high-visibility aircraft cover

Abstract

The utility model discloses all -weather high visual aircraft protection cover, relates to the aircraft cover technical field, including cover, the inside of cover and the aircraft fuselage abut, the outside of cover even fixed mounting has a plurality of mounting seat, the inside even magnetism joint of mounting seat has the receiving seat, the rotary plate of receiving seat all limit rotation installation has, the front side of rotary plate all has set up the slot, the inside limit sliding installation of slot has the reflector plate, the bottom fixed mounting of rotary plate has the storage battery, the both sides of slot all fixed mounting have LED light bar, and the storage battery provides the power supply for LED light bar. The operator can manually adjust rotary plate to the angle required and utilize the damping and keep stable, and the reflector plate can be inserted into the slot and by LED auxiliary luminescence. Ensure that the aircraft contour is always clear and identifiable under the all -weather conditions of night, rain and fog, improve the identification ability of ground personnel and helicopter pilots, effectively avoid the collision risk, guarantee the safety of the parking and take -off area.

Description

Technical Field

[0001] This utility model relates to the field of aircraft cover technology, and in particular to all-weather high-visibility aircraft protective cover. Background Technology

[0002] Aircraft protective tarpaulin is a specialized protective material applied to the surface of an aircraft, primarily used to protect it from external environmental damage during parking or transport. It effectively prevents corrosion and physical damage to critical components such as the fuselage, engine, and pitot tube from ultraviolet rays, rain, snow, dust, and bird droppings, maintaining their good condition, extending their service life, and ensuring flight safety.

[0003] Currently widely used aircraft protective tarpaulins have a deficiency: they generally lack effective reflective or high-visibility functions. This results in extremely poor visibility in low-visibility environments, such as heavy fog, heavy rain, or nighttime conditions. This low visibility not only makes it difficult for ground support vehicles to identify and avoid collisions on taxiways or aprons, posing a risk to aircraft surface safety; more seriously, in helicopter landing areas, if aircraft parked on the ground are covered by such tarpaulins, their blurred outlines will blend into the background environment, easily interfering with helicopter pilots' judgment of ground obstacles, potentially leading to misjudgments of flight path or altitude, and posing a potential threat to flight safety.

[0004] To address the aforementioned issues, this utility model proposes an all-weather, high-visibility aircraft protective cover. Utility Model Content

[0005] To address the problems existing in the background technology, this utility model proposes an all-weather high-visibility aircraft protective cover.

[0006] To achieve the above objectives, this utility model provides the following technical solution: an all-weather high-visibility aircraft protective cover, comprising a cover, the inner side of which abuts against the aircraft fuselage, and multiple mounting seats evenly fixedly installed on the outer side of the cover. Each mounting seat has a magnetically engaged receiving seat, and each receiving seat has a rotating plate rotatably mounted on it. Each rotating plate has a slot on its front side, and a reflector is slidably mounted inside the slot. A storage battery is fixedly installed at the bottom of the rotating plate, and LED light strips are fixedly installed on both sides of the slot. The storage battery provides power to the LED light strips.

[0007] The present invention is further configured such that a rotating groove is provided on the side of the receiving seat away from the mounting seat, a rotating block is rotatably installed inside the rotating groove, the side of the rotating block away from the rotating groove is fixedly connected to the rotating plate, and a damping shaft is rotatably installed on the upper limit of the receiving seat, and the damping shaft is fixedly connected to the rotating block.

[0008] The present invention is further configured such that straps are symmetrically fixedly installed on both bottom ends of the cover, and buckles are fixedly installed on the ends of the straps away from the cover, so that the cover can be detachably tied to the fuselage of the aircraft by means of the straps and buckles.

[0009] The present invention is further configured such that the upper end of the covering fabric is provided with a double zipper, so as to make room for the helicopter rotor shaft.

[0010] The present invention is further configured such that a magnetic block is fixedly installed inside the mounting base and on the opposite surface of the receiving base.

[0011] Compared with the prior art, the beneficial effects of this utility model are:

[0012] This all-weather high-visibility aircraft protective tarpaulin consists of a mounting base, magnetic support, damping pivot, rotatable plate, reflector, and battery. After installation, the tarpaulin is secured with straps. Operators can manually adjust the rotatable plate to the desired angle and utilize damping for stability. The reflector can be inserted into a slot and is illuminated by LEDs. This ensures that the aircraft's outline remains clearly visible in all weather conditions, including nighttime, rain, and fog, enhancing the identification capabilities of ground personnel and helicopter pilots, effectively mitigating collision risks, and ensuring the safety of parking and landing areas. Attached Figure Description

[0013] The present invention will be further described below with reference to the accompanying drawings and embodiments:

[0014] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0015] Figure 2 This is a partial structural diagram of the present invention;

[0016] Figure 3 This is a partial cross-sectional view of the present invention.

[0017] Reference numerals: 1. Covering fabric; 2. Mounting base; 3. Receiving base; 4. Rotating plate; 5. Slot; 6. Reflector; 7. Storage battery; 8. LED light strip; 9. Rotating groove; 10. Rotating block; 11. Damping shaft; 12. Strap; 13. Buckle; 14. Double zipper; 15. Magnetic block. Detailed Implementation

[0018] It should be noted that, unless otherwise specified, the embodiments and features described in this application can be combined with each other. The present invention will now be described in detail with reference to the accompanying drawings and embodiments.

[0019] It should be noted that, unless otherwise specified, all technical and scientific terms used in this application have the same meaning as commonly understood by one of ordinary skill in the art to which this application pertains.

[0020] In this utility model, unless otherwise stated, the orientations used, such as "up" and "down", usually refer to the direction shown in the accompanying drawings, or to the vertical, perpendicular, or gravitational direction; similarly, for ease of understanding and description, "left" and "right" usually refer to the left and right shown in the accompanying drawings; "inner" and "outer" refer to the inner and outer contours of each component itself, but the above directional terms are not used to limit this utility model.

[0021] Please see Figure 1-3 This utility model provides a technical solution: an all-weather high-visibility aircraft protective cover, including a cover 1, the inner side of the cover 1 abuts against the aircraft fuselage, and multiple mounting seats 2 are evenly fixedly installed on the outer side of the cover 1. Each mounting seat 2 is magnetically snapped with a receiving seat 3. Specifically, a magnetic block 15 is fixedly installed on the inner side of the mounting seat 2 and the opposite surface of the receiving seat 3.

[0022] By adopting the above solution, the quick assembly and disassembly of the mounting base and the receiving base facilitates maintenance and replacement.

[0023] Each receiving seat 3 is equipped with a rotating plate 4 for limiting rotation. Specifically, a rotating groove 9 is provided on the side of the receiving seat 3 away from the mounting seat 2. A rotating block 10 is rotatably installed inside the rotating groove 9. The side of the rotating block 10 away from the rotating groove 9 is fixedly connected to the rotating plate 4. A damping shaft 11 is rotatably installed on the upper limit of the receiving seat 3. The damping shaft 11 is fixedly connected to the rotating block 10.

[0024] By adopting the above solution, the rotating plate can be adjusted at multiple angles and can be stably hovered at any position, thus ensuring the best viewing angle of the reflector.

[0025] Each rotating plate 4 has a slot 5 on its front side. A reflector 6 is slidably mounted inside the slot 5. A storage battery 7 is fixedly mounted at the bottom of the rotating plate 4. LED light strips 8 are fixedly mounted on both sides of the slot 5. The storage battery 7 provides power to the LED light strips 8. This provides active lighting to enhance visibility at night or in inclement weather.

[0026] In this embodiment of the utility model: straps 12 are symmetrically fixedly installed on the bottom ends of both sides of the cover 1, and buckles 13 are fixedly installed on the end of the straps 12 away from the cover 1. The cover 1 can be detachably tied to the fuselage of the aircraft by the straps 12 and the buckles 13.

[0027] In this embodiment of the utility model: the upper end of the cover 1 is provided with a double zipper 14 so as to make room for the helicopter rotor shaft.

[0028] Working principle:

[0029] When the cover 1 covers the body, the evenly distributed mounting bases 2 on its outer side magnetically engage with the receiving base 3 via built-in magnetic blocks 15, ensuring that each functional unit can be quickly installed or removed, providing a basis for subsequent maintenance and replacement. The receiving base 3, through the cooperation of the rotating groove 9, rotating block 10, and damping shaft 11, achieves the limited rotational installation of the rotating plate 4; the damping shaft 11 provides stable rotational resistance, allowing the operator to manually and precisely adjust the rotating plate 4 to the required angle and stably hover it at any position, thus ensuring that the reflective unit fixed on the rotating plate 4 can adapt to different viewing angles and ambient light, always achieving the best reflective effect.

[0030] The reflective function is achieved in two ways: active illumination with a light source and passive reflection without a light source. A reflector 6 is slidably mounted in the slot 5 on the front side of the rotating plate 4. This plug-and-play design allows the reflector 6 to be easily removed and replaced when worn or requiring an upgrade. Meanwhile, the LED light strips 8 fixedly mounted on both sides of the slot 5 are powered by the battery 7 at the bottom of the rotating plate 4. In low-visibility conditions such as nighttime or rain / fog, the LED light strips 8 can actively emit light, greatly enhancing the overall visibility of the covering 1.

[0031] The cover 1 is secured to the fuselage by symmetrical straps 12 and buckles 13 at both bottom sides, ensuring a firm hold even in windy conditions, while also facilitating easy assembly and disassembly. For helicopter models, the double zipper 14 structure on the upper surface of the cover 1 effectively provides space for the rotor shaft, ensuring that the cover 1 provides comprehensive protection without affecting critical helicopter components.

[0032] In summary, this design achieves the core functions of high reflectivity, multi-angle adjustment, convenient disassembly, easy maintenance, and clear identification through a series of actions such as magnetic connection, damped rotation, slot replacement, battery power, strap fixation, and zipper avoidance. All of its action designs are aimed at improving safety and operational efficiency.

[0033] The embodiments of the present utility model have been described in detail above with reference to the accompanying drawings. However, the present utility model is not limited to the above embodiments. Within the scope of knowledge possessed by those skilled in the art, various changes can be made without departing from the spirit of the present utility model.

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