Anti-icing net for aircraft

Abstract

The utility model discloses an anti-icing net for an aircraft, which relates to the technical field of anti-icing nets and specifically comprises an anti-icing net body, silk hairs are fixedly mounted on the upper surface of the anti-icing net body, a round rod is fixedly mounted at the front end of the silk hairs, a metal ring is fixedly mounted at the front end of the round rod, and the metal ring is fixedly mounted on the upper surface of the anti-icing net body. A pulling rod is fixedly installed at the front end of the metal ring, a belt is fixedly installed at the front end of the round rod, a fixing plate is movably installed at one end of the belt, a fixing suction cup is fixedly installed on the lower surface of the fixing plate, a storage barrel is fixedly installed at the rear end of the anti-icing net body, and a net leaking bag is fixedly installed on the outer arc face of the storage barrel. And a first tooth chain is fixedly installed on the side, close to the net leaking bag, of the outer arc surface of the storage barrel, through arrangement of a rotating rod, a transmission gear and a storage shaft, after the anti-icing net is used, the gear can drive the storage shaft to rotate through rotation of the rotating rod, and then the anti-icing net can be stored in the storage barrel more conveniently.

Description

Technical Field

[0001] The utility model relates to the technical field of anti-icing nets, in particular to an anti-icing net that can be used for aircraft. Background Art

[0002] An aircraft is any craft capable of flying within the atmosphere. To become airborne, any aircraft must generate lift greater than its own weight. Based on the principle of lift generation, aircraft can be divided into two categories: lighter-than-air aircraft and heavier-than-air aircraft. The former relies on static buoyancy to achieve lift, while the latter relies on aerodynamic forces to overcome their own weight.

[0003] Currently, the anti-icing nets available on the market for aircraft are difficult to quickly store after actual use, and it is also difficult to clean the ice on the surface of the anti-icing nets when storing them. Utility Model Content

[0004] In view of the shortcomings of the existing technology, the utility model provides an anti-icing net that can be used for aircraft, which solves the problems of being difficult to quickly store the anti-icing net after actual use and difficult to clean the ice on the surface of the anti-icing net when storing.

[0005] To achieve the above objectives, the present invention is implemented through the following technical solutions: an anti-icing net that can be used for aircraft includes an anti-icing net body, the upper surface of the anti-icing net body is fixedly installed with silk wool, the front end of the silk wool is fixedly installed with a round rod, the front end of the round rod is fixedly installed with a metal ring, the front end of the metal ring is fixedly installed with a pull rod, the front end of the round rod is fixedly installed with a belt, one end of the belt is movably installed with a fixed plate, the lower surface of the fixed plate is fixedly installed with a fixed suction cup, the rear end of the anti-icing net body is fixedly installed with a storage tube, the outer arc surface of the storage tube is fixedly installed with a leakage net bag, and the side of the outer arc surface of the storage tube close to the leakage net bag is fixedly installed with a first tooth chain.

[0006] Optionally, a net bag cover is fixedly mounted on one side of the outer arc surface of the storage tube close to the leakage net bag, a second fastener chain is fixedly mounted on the upper surface of the net bag cover, and a zipper head is movably mounted on the upper surface of the second fastener chain.

[0007] Optionally, a groove is provided on one side of the storage tube, and a rotating rod is movably mounted on the inner side wall of the groove.

[0008] Optionally, a rotating rod is fixedly mounted on one side of the rotating rod, and a half gear is fixedly mounted on one end of the rotating rod.

[0009] Optionally, a transmission gear is movably mounted on the outer arc surface of the half gear, and a storage shaft is fixedly mounted on one side of the transmission gear, so that the storage shaft can be rotated by a rotating rod to store the anti-icing net to the surface of the storage shaft.

[0010] Optionally, a positioning rod is movably installed on the inner wall of the storage cylinder, and a friction block is fixedly installed on the outer arc surface of the positioning rod, so that when the storage shaft stores the anti-icing net, the ice on the anti-icing net can be scraped off by the friction block and then leaked out from the net bag.

[0011] The utility model provides an anti-icing net that can be used for aircraft, which has the following beneficial effects:

[0012] 1. Through the arrangement of the rotating rod, half gear, transmission gear and storage shaft, the anti-icing net can be stored in the storage tube more conveniently after use by rotating the rotating rod, which causes the gear to drive the storage shaft to rotate. The storage method is simple and quick.

[0013] 2. The arrangement of the net bag, positioning rod, and friction block allows the friction block on the positioning rod to wipe away ice from the surface of the anti-icing net as it is retracted into the storage cylinder, thereby ensuring that the anti-icing net remains dry after storage and improving its moisture-proofing effect. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for the embodiments or the description of the prior art. Obviously, the drawings described below are only exemplary, and those skilled in the art can also derive other implementation drawings based on the provided drawings without inventive effort.

[0015] Figure 1 This is a schematic diagram of the structure of the utility model;

[0016] Figure 2 It is a schematic diagram of the local structure of the utility model;

[0017] Figure 3 This is a schematic diagram of the back structure of the utility model;

[0018] Figure 4 It is a schematic diagram of the local structure of the utility model.

[0019] In the figure: 1. Anti-icing net body; 2. Silk wool; 3. Round rod; 4. Metal ring; 5. Pull rod; 6. Belt; 7. Fixed plate; 8. Fixed suction cup; 9. Storage tube; 10. Net bag; 11. First chain; 12. Net bag cover; 13. Second chain; 14. Zipper head; 15. Groove; 16. Turn rod; 17. Turn rod; 18. Half gear; 19. Transmission gear; 20. Storage shaft; 21. Positioning rod; 22. Friction block. DETAILED DESCRIPTION

[0020] The structures, proportions, sizes, etc. illustrated in this specification are intended solely to complement the contents disclosed herein and to facilitate understanding and reading by persons familiar with the art. They are not intended to limit the conditions under which the present invention may be implemented and therefore have no substantive technical significance. Any structural modifications, changes in proportions, or adjustments in size, without affecting the efficacy and objectives of the present invention, shall remain within the scope of the technical contents disclosed herein.

[0021] See also Figures 1 to 4 The utility model provides a technical solution: an anti-icing net that can be used for aircraft, comprising an anti-icing net body 1, a silk wool 2 is fixedly installed on the upper surface of the anti-icing net body 1, a round rod 3 is fixedly installed on the front end of the silk wool 2, a metal ring 4 is fixedly installed on the front end of the round rod 3, a pulling rod 5 is fixedly installed on the front end of the metal ring 4, a belt 6 is fixedly installed on the front end of the round rod 3, a fixing plate 7 is movably installed on one end of the belt 6, a fixed suction cup 8 is fixedly installed on the lower surface of the fixing plate 7, a storage tube 9 is fixedly installed on the rear end of the anti-icing net body 1, a leakage net bag 10 is fixedly installed on the outer arc surface of the storage tube 9, and a first tooth chain 11 is fixedly installed on the side of the outer arc surface of the storage tube 9 close to the leakage net bag 10.

[0022] By setting the rotating rod 16, the half gear 18, the transmission gear 19 and the storage shaft 20, the anti-icing net can be more conveniently stored in the storage tube 9 after use by rotating the rotating rod 16 so that the gear can drive the storage shaft 20 to rotate. The storage method is simple and quick.

[0023] A net bag cover 12 is fixedly installed on the side of the outer arc surface of the storage tube 9 close to the leakage net bag 10, and a second tooth chain 13 is fixedly installed on the upper surface of the net bag cover 12. A zipper head 14 is movably installed on the upper surface of the second tooth chain 13. A groove 15 is provided on one side of the storage tube 9, and a rotating rod 16 is movably installed on the inner side wall of the groove 15. A rotating rod 17 is fixedly installed on one side of the rotating rod 16, and a half gear 18 is fixedly installed on one end of the rotating rod 17. A transmission gear 19 is movably installed on the outer arc surface of the half gear 18, and a storage shaft 20 is fixedly installed on one side of the transmission gear 19. A positioning rod 21 is movably installed on the inner side wall of the storage tube 9, and a friction block 22 is fixedly installed on the outer arc surface of the positioning rod 21.

[0024] By setting the leakage net bag 10, the positioning rod 21 and the friction block 22, the ice on the surface of the anti-icing net can be wiped off by the friction block 22 on the positioning rod 21 during the process of collecting the anti-icing net into the storage cylinder 9, thereby ensuring that the anti-icing net is dry after storage and improving the moisture-proof effect.

[0025] In the present invention, the working steps of the device are as follows:

[0026] When in use, the staff pulls the rod 5 to pull the anti-icing net body 1 out of the storage tube 9. By setting the anti-icing net body 1, the aircraft can be covered. Then, the fixed suction cups 8 on the two belts 6 at the front end of the round rod 3 can fix the anti-icing net body 1, so that the anti-icing net body 1 will not be blown off by the wind, and the silk hairs 2 on the surface of the anti-icing net body 1 can play a role in blocking snow and ice, preventing snow and ice from directly covering the surface of the aircraft. By pulling out the anti-icing net body 1, the snow and ice can be quickly shaken out. Later, when the anti-icing net body 1 needs to be stored, it can be stored by The rotation of the rotating rod 16 on one side of the storage tube 9 and the rotation of the half gear 18 can drive the storage shaft 20 to rotate to complete the storage of the anti-icing net body 1. At the same time, when the anti-icing net body 1 is stored in the storage tube 9, the positioning rod 21 on the inner wall of the storage tube 9 will wipe the ice on the surface of the anti-icing net body 1, and then the wiped ice will fall out of the net bag 10, thereby ensuring that the anti-icing net is dry after storage. Then, after the anti-icing net is completely stored, the zipper on the outer arc surface of the storage tube 9 is pulled up to prevent dust from entering the storage tube 9, thereby ensuring the sealing of the storage tube 9.

[0027] Although the 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 variations may be made to these embodiments without departing from the principles and spirit of the present invention, and the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An anti-icing net for aircraft, comprising an anti-icing net body (1), characterized in that: The upper surface of the anti-icing net body (1) is fixedly mounted with a silk wool (2), the front end of the silk wool (2) is fixedly mounted with a round rod (3), the front end of the round rod (3) is fixedly mounted with a metal ring (4), the front end of the metal ring (4) is fixedly mounted with a pull rod (5), the front end of the round rod (3) is fixedly mounted with a belt (6), one end of the belt (6) is movably mounted with a fixed plate (7), the lower surface of the fixed plate (7) is fixedly mounted with a fixed suction cup (8), the rear end of the anti-icing net body (1) is fixedly mounted with a storage tube (9), the outer arc surface of the storage tube (9) is fixedly mounted with a leakage net bag (10), and the side of the outer arc surface of the storage tube (9) close to the leakage net bag (10) is fixedly mounted with a first tooth chain (11).

2. The anti-icing net for aircraft according to claim 1, characterized in that: A net bag cover (12) is fixedly mounted on one side of the outer arc surface of the storage tube (9) close to the leakage net bag (10), a second tooth chain (13) is fixedly mounted on the upper surface of the net bag cover (12), and a zipper head (14) is movably mounted on the upper surface of the second tooth chain (13).

3. The anti-icing net for aircraft according to claim 1, characterized in that: A groove (15) is provided on one side of the storage cylinder (9), and a rotating rod (16) is movably mounted on the inner side wall of the groove (15).

4. The anti-icing net for aircraft according to claim 3, characterized in that: A rotating rod (17) is fixedly mounted on one side of the rotating rod (16), and a half gear (18) is fixedly mounted on one end of the rotating rod (17).

5. The anti-icing net for aircraft according to claim 4, characterized in that: A transmission gear (19) is movably mounted on the outer arc surface of the half gear (18), and a storage shaft (20) is fixedly mounted on one side of the transmission gear (19).

6. The anti-icing net for aircraft according to claim 1, characterized in that: A positioning rod (21) is movably mounted on the inner side wall of the storage cylinder (9), and a friction block (22) is fixedly mounted on the outer arc surface of the positioning rod (21).

Images