Detachable low-altitude aircraft transparent part

Abstract

The invention belongs to the technical field of low-altitude flight products, and provides a detachable low-altitude aircraft transparent part which comprises a transparent part body, a sealing strip and a fuselage, the sealing strip is located between the transparent part body and the fuselage and used for installation and sealing between the transparent part body and the fuselage, and a detachable connecting structure is arranged between the transparent part body and the fuselage. The transparent part is connected with the machine body through a detachable connecting structure. The structure has the advantages that a sealing ring bolt installation structure is adopted to replace a gluing structure, installation is easy, stress is small, the production time cost is greatly reduced, the production efficiency and the qualified rate of products are improved, the sealing strip structure also improves the fit clearance between the transparent part and the machine body and the appearance effect, and later disassembly and maintenance are also facilitated.

Description

Technical Field

[0001] The invention belongs to the technical field of low-altitude flight products, and in particular relates to a detachable transparent part for low-altitude aircraft. Background Art

[0002] The existing transparent front shield solution for low-altitude aircraft basically adopts a structure with complex process, which is prone to glue shortage and leakage, and is difficult to clean, and the entire process takes a long time. Under harsh environmental tests, there is a risk of debonding, which poses a major safety hazard to the driver and passengers. In addition, the low-altitude aircraft transparent parts formed by the gluing solution are in a fixed state, and later disassembly and maintenance are also relatively troublesome. Therefore, it is necessary to develop a new low-altitude aircraft transparent part. Summary of the Invention

[0003] The technical problem to be solved by the present invention is to provide a detachable low-altitude aircraft transparent part that is simple to install, convenient to disassemble, has low stress, greatly reduces production labor costs, and improves product production efficiency and qualification rate based on the current status of the existing technology.

[0004] The technical solution adopted by the present invention to solve the above-mentioned technical problems is: a detachable low-altitude aircraft transparent part, characterized in that it includes a transparent part, a sealing strip and a fuselage, the sealing strip is located between the transparent part and the fuselage and is used for installation and sealing between the transparent part and the fuselage, and a detachable connecting structure is provided between the transparent part and the fuselage, and the transparent part is connected and installed to the fuselage through the detachable connecting structure.

[0005] In the above-mentioned detachable low-altitude aircraft transparent part, the detachable connection structure between the transparent part and the fuselage is a bolt connection or a screw connection.

[0006] As one of the methods, in the above-mentioned detachable low-altitude aircraft transparent part, the transparent part includes a main body, the main body is made of PC material, a copper sleeve is embedded in the main body, the middle of the copper sleeve is a fixing hole, the fixing hole passes through the main body, the sealing strip and the fuselage at the same time, the detachable connecting structure is a bolt and a nut, the bolt passes through the fixing hole and one end is connected and fixed to the nut.

[0007] In the aforementioned detachable low-altitude aircraft transparent component, the transparent component is formed by two-color injection molding, wherein the first color is PC and the second color is PUR. The PUR dielectric body is formed by two-color injection molding on the outer surface of the main body. The PUR dielectric body can improve the toughness and heat resistance of the transparent component.

[0008] As a second method, in the above-mentioned detachable low-altitude aircraft transparent part, the transparent part is formed by three-color injection molding, and the transparent part includes a main body, the first color of the transparent part is PC, the second color is PUR, and the third color is PC / ABS. A PUR medium body formed by the second color is injection-molded on the outer surface of the main body, wherein the PC / ABS has a through hole, and the detachable connecting structure is a bolt and a nut, and the bolt passes through the through hole and one end is connected and fixed to the nut.

[0009] As a third method, in the above-mentioned detachable low-altitude aircraft transparent part, the transparent part is formed by three-color injection molding, and the transparent part includes a main body, wherein the first color of the transparent part is PC, the second color is PUR, and the third color is PC / ABS, wherein the outer side of the main body is a PUR medium body formed by in-film reaction; a PC / ABS insert block is injection-molded on the back of the main body, and the detachable connecting structure is a screw and a nut, and a blind hole is provided on the insert block, the nut is located at the blind hole, and the screw is passed through the blind hole and fixed to the nut.

[0010] As a fourth method, in the above-mentioned detachable low-altitude aircraft transparent part, the transparent part is formed by two-color injection molding, and the transparent part includes a main body, wherein the first color of the transparent part is PC, and the second color is PUR, wherein the outer side of the main body is formed by in-film reaction molding of a PUR medium body, and the detachable connecting structure is a bolt and a nut, and the first color is PC embedded with a bolt, and the nut is fixed to the bolt.

[0011] In the above-mentioned detachable low-altitude aircraft transparent part, a portion of the sealing strip is arranged at the bottom of the transparent part, a shielding coating is applied on the outermost side of the transparent part, and a sealant is applied to the side gaps.

[0012] Compared with the existing technology, the advantage of the present invention is that it adopts a sealing ring bolt installation structure instead of a gluing structure, which is simple to install and has low stress, greatly reducing production labor costs, and improving product production efficiency and pass rate. The sealing strip structure also improves the fitting clearance and appearance effect between the transparent parts and the fuselage, and is also convenient for later disassembly and maintenance. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 This is a structural diagram of the first embodiment of the detachable low-altitude aircraft transparent component;

[0014] Figure 2 This is a structural diagram of a second embodiment of the detachable low-altitude aircraft transparent component;

[0015] Figure 3 This is a structural diagram of a third embodiment of the detachable low-altitude aircraft transparent component;

[0016] Figure 4 It is a structural schematic diagram of the fourth embodiment of the detachable low-altitude aircraft transparent component. DETAILED DESCRIPTION

[0017] The following are specific embodiments of the present invention and the accompanying drawings to further describe the technical solutions of the present invention, but the present invention is not limited to these embodiments.

[0018] In the figure, transparent part 100; PC 101; PUR 102; PC / ABS 103; sealing strip 200; fuselage 300; main body 400; copper sleeve 500; bolt 600; nut 700; screw 800.

[0019] Example 1

[0020] like Figure 1 As shown, the detachable low-altitude aircraft transparent part includes a transparent part 100, a sealing strip 200 and a fuselage 300. The sealing strip 200 is located between the transparent part 100 and the fuselage 300 and is used for installation and sealing between the transparent part 100 and the fuselage 300. The sealing strip 200 also improves the matching clearance and appearance effect between the transparent part 100 and the fuselage 300. Here, in order to facilitate installation, a detachable connecting structure is provided between the transparent part 100 and the fuselage 300. The transparent part 100 is connected and installed with the fuselage 300 through the detachable connecting structure. The detachable connecting structure is used here instead of the gluing structure, which is simple to install and has low stress, greatly reduces the production time cost, and improves the production efficiency and qualified rate of the product. Specifically, in this embodiment, the detachable connecting structure between the transparent part 100 and the fuselage 300 is a screw Bolt connection. In this embodiment, the transparent part 100 includes a main body 400, which is made of PC material. In order to facilitate installation, a copper sleeve 500 is embedded in the main body 400. The middle of the copper sleeve 500 is a fixing hole. The fixing hole passes through the main body 400, the sealing strip 200 and the fuselage 300 at the same time. The detachable connection structure is a bolt 600 and a nut 700. The bolt 600 passes through the fixing hole and one end is connected and fixed to the nut 700. The transparent part 100 is formed by two-color injection molding, wherein the first color is PC101 and the second color is PUR102. A PUR medium body is formed by two-color injection molding on the outer surface of the main body 400. Here, the PUR medium body can be used to improve the toughness and heat resistance of the transparent part 100. At the same time, the bolt 600 and the nut 700 are connected instead of the gluing structure, which is simple to install and has low stress.

[0021] Example 2

[0022] like Figure 2As shown, most of the structures of this embodiment are the same as those of Example 1, with the main difference being that the transparent member 100 is formed by three-color injection molding, and the transparent member 100 includes a body 400, the first color of the transparent member 100 is PC101, the second color is PUR102, and the third color is PC / ABS103, and a PUR medium body formed by the second color is injection-molded on the outer surface of the body 400, wherein the PC / ABS103 has a through hole, and the detachable connection structure is a bolt 600 and a nut 700, wherein the bolt 600 passes through the through hole and one end is connected and fixed to the nut 700, and the installation is achieved through the through hole on the PC / ABS103, which can reduce the stress of the body 400 and the risk of silver streaks; finally, putty is scraped and painted at the bolt 600 to meet the appearance requirements.

[0023] Example 3

[0024] The transparent part 100 is formed by three-color injection molding. The transparent part 100 includes a main body 400, wherein the first color of the transparent part 100 is PC101, the second color is PUR102, and the third color is PC / ABS103. The outer side of the main body 400 is formed by in-film reaction molding of a PUR dielectric body; the third color is PC / ABS103 located at the bottom of the first color PC101, and an insert block of PC / ABS103 is injection-molded on the back of the main body 400. The detachable connection structure between the transparent part 100 and the fuselage 300 is a screw 800 and a nut 700. There is a blind hole on the insert block, and the nut 700 is located at the blind hole. The screw 800 is passed through the blind hole and fixed with the nut 700. Here, in this embodiment, the nut 700 is used as an insert block. This solution can avoid stress concentration caused by punching the hole, affecting the service life, and can also reduce the black edge spray painting treatment on the edge of the transparent part 100, while also ensuring the appearance effect.

[0025] Example 4

[0026] In this embodiment, the transparent part 100 is formed by two-color injection molding. The transparent part 100 includes a main body 400, wherein the first color of the transparent part 100 is PC101, and the second color is PUR102. The outer side of the main body 400 is formed by in-film reaction molding of a PUR dielectric body, and the detachable connection structure is a bolt 600 and a nut 700. The first color is PC101 with a bolt 600 embedded thereon, and the nut 700 is fixed to the bolt 600. A portion of the sealing strip 200 is arranged at the bottom of the transparent part 100, and a shielding coating is applied on the outermost side of the transparent part 100, and a sealant is applied to the side gap. This solution adopts a three-layer sealing structure, which has more reliable sealing, and a sealing ring is used at the bottom, which is more convenient for subsequent disassembly and maintenance.

[0027] The specific embodiments described herein are merely examples of the spirit of the present invention. Those skilled in the art may make various modifications to the described specific embodiments or replace them with similar methods without departing from the scope defined by the spirit of the present invention.

Claims

1. A detachable low-altitude aircraft transparent part, characterized in that: It includes a transparent part, a sealing strip and a fuselage. The sealing strip is located between the transparent part and the fuselage and is used for installation and sealing between the transparent part and the fuselage. A detachable connection structure is provided between the transparent part and the fuselage, and the transparent part is connected and installed with the fuselage through the detachable connection structure.

2. The detachable low-altitude aircraft transparent part according to claim 1, characterized in that: The detachable connection structure between the transparent part and the fuselage is a bolt connection or a screw connection.

3. A detachable low-altitude aircraft transparent part according to claim 1 or 2, characterized in that: The transparent part includes a main body, which is made of PC material. A copper sleeve is embedded in the main body. The middle of the copper sleeve is a fixing hole. The fixing hole passes through the main body, the sealing strip and the fuselage at the same time. The detachable connection structure is a bolt and a nut. The bolt passes through the fixing hole and one end is connected and fixed to the nut.

4. The detachable low-altitude aircraft transparent component according to claim 3, characterized in that: The transparent part is formed by double-color injection molding, wherein the first color is PC and the second color is PUR. The outer surface of the main body is double-color injection molded with a PUR dielectric body. The PUR dielectric body can improve the toughness and heat resistance of the transparent part.

5. A detachable low-altitude aircraft transparent component according to claim 1 or 2, characterized in that: The transparent part is formed by three-color injection molding, and the transparent part includes a body. The first color of the transparent part is PC, the second color is PUR, and the third color is PC / ABS. A PUR medium body formed by the second color is injection-molded on the outer surface of the body, wherein the PC / ABS has a through hole, and the detachable connection structure is a bolt and a nut. The bolt passes through the through hole and one end is connected and fixed to the nut.

6. A detachable low-altitude aircraft transparent component according to claim 1 or 2, characterized in that: The transparent part is formed by three-color injection molding, and includes a body, wherein the first color of the transparent part is PC, the second color is PUR, and the third color is PC / ABS. The outer side of the body is formed by an in-film reaction molding PUR dielectric body; an insert block of PC / ABS is injection-molded on the back of the body, and the detachable connection structure is a screw and a nut. There is a blind hole on the insert block, and the nut is located at the blind hole. The screw is passed through the blind hole and fixed to the nut.

7. A detachable low-altitude aircraft transparent component according to claim 1 or 2, characterized in that: The transparent part is formed by two-color injection molding, and the transparent part includes a body, wherein the first color of the transparent part is PC and the second color is PUR, wherein the outer side of the body is formed by in-film reaction molding of a PUR medium body, and the detachable connection structure is a bolt and a nut, wherein the first color is PC with a bolt embedded therein, and the nut is fixed to the bolt.

8. The detachable low-altitude aircraft transparent component according to claim 7, characterized in that: A portion of the sealing strip is arranged at the bottom of the transparent part, a masking coating is applied on the outermost side of the transparent part, and sealant is applied to the side gaps.

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