Visual anti-vibration wind shield

Abstract

The utility model relates to a visual anti-vibration wind shield which comprises a shield body attaching frame, an arc-shaped shield body embedded in the shield body attaching frame, lateral supporting assemblies arranged on the two sides of the shield body attaching frame and a C-shaped connecting assembly arranged on the top of the shield body attaching frame. The C-shaped connecting assembly is connected with the machine body; the arc-shaped cover body is made of organic glass and is in a hyperbolic shape, so that wind resistance in flight is reduced; the wind shield is made of organic glass, is good in light transmission and has a good forward view field; the force transmission frame reduces air resistance and prevents the arc-shaped cover body from generating cracks; the side wind shield is used for being connected with the outer surface of the airplane belly skin and reducing stress concentration at the arc angle of the tip end, and the attaching frame, the lateral supporting assembly and the C-shaped connecting assembly reduce vibration of the wind shield and prevent damage caused by shaking of the wind shield.

Description

Technical Field

[0001] The utility model relates to a visible anti-vibration windshield, belonging to the technical field of aviation. Background Art

[0002] At present, the optical equipment on board small multi-purpose aircraft is mostly hung on the belly of the aircraft. When the aircraft is flying, impurities carried in the airflow will cause the lens to wear and tear. The windshield made of fiber composite materials is mostly opaque, which will reduce the field of view of the optical equipment. The general aviation organic glass adopts a flat structure and is easily cracked due to the stress concentration caused by the vibration during flight. It cannot protect the optical equipment on board, and has an adverse effect on flight safety. Utility Model Content

[0003] The technical problem to be solved by the utility model is to provide a visible anti-vibration wind shield which can reduce air resistance, vibration and prevent damage caused by shaking.

[0004] The utility model adopts the following technical solutions:

[0005] The utility model comprises a cover body fitting frame, an arc-shaped cover body embedded in the cover body fitting frame, lateral support components arranged on both sides of the cover body fitting frame and a C-shaped connecting component arranged on the top of the cover body fitting frame; the C-shaped connecting component is connected to the fuselage.

[0006] The arc-shaped cover body of the utility model is a hyperbolic shape, and its curvature is 0.008-0.01.

[0007] The utility model comprises a lateral support component which is arranged on both sides of the cover body fitting frame and the inner side of the bottom edge and is used to prevent the arc-shaped cover body tip from deforming.

[0008] The utility model C-shaped connecting assembly comprises an inner frame arranged on the inner side of the top of the cover body fitting frame and an outer frame arranged on the outer side of the top of the cover body fitting frame, and both the inner frame and the outer frame are connected to the fuselage.

[0009] The utility model is provided with triangular side wind shielding plates at the outer sides of the force transmission frames on both sides, and the top ends of the side wind shielding plates are folded outwards.

[0010] The arc-shaped cover body of the utility model is made of organic glass.

[0011] The positive effects of the utility model are as follows: the arc-shaped cover body of the utility model is made of plexiglass and has a hyperbolic shape, and its curvature is 0.008-0.01, which reduces wind resistance during flight; the windshield is made of plexiglass, has good light transmittance, and has a good forward field of vision; the force transmission frame reduces air resistance and prevents cracks from occurring in the arc-shaped cover body; the side windshield plate is used to connect the outer surface of the aircraft's belly skin, reducing stress concentration at the tip of the arc corner, and the fitting frame, lateral support assembly and C-shaped connection assembly reduce the vibration of the windshield and prevent the windshield from shaking and causing damage.

[0012] The utility model is convenient for maintenance and effectively protects the airborne optical equipment and instruments. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Attached Figure 1 It is a schematic diagram of the structure of the utility model;

[0014] Attached Figure 2 This is a schematic diagram of the cover body fitting frame structure of the utility model;

[0015] Attached Figure 3 This is a schematic diagram of the installation structure of the side wind shield of the utility model. DETAILED DESCRIPTION

[0016] As attached Figure 1 As shown, the utility model comprises a cover body fitting frame 1, an arc-shaped cover body 2 embedded in the cover body fitting frame 1, lateral support components arranged on both sides of the cover body fitting frame 1, and a C-shaped connecting component arranged on the top of the cover body fitting frame 1; the C-shaped connecting component is connected to the fuselage. The arc-shaped cover body 2 is made of organic glass and has a hyperbolic shape with a curvature of 0.008 to 0.01, which reduces wind resistance during flight.

[0017] As attached Figure 1-3 As shown, the lateral support assembly of the utility model includes a force transmission frame 3 arranged on both sides of the cover body fitting frame 1 and the inner side of the bottom edge for preventing the slight end of the arc-shaped cover body 2 from deforming. The force transmission frame 3 can effectively reduce air resistance and prevent the arc-shaped cover body 2 from cracking.

[0018] As attached Figure 1 , 3 As shown, the C-shaped connection assembly of the utility model includes an inner frame 4 arranged on the inner side of the top of the cover body fitting frame 1 and an outer frame 5 arranged on the outer side of the top of the cover body fitting frame 1, and the inner frame 4 and the outer frame 5 are both connected to the fuselage.

[0019] The utility model provides triangular side windshield plates 6 on the outer sides of the force transmission frames 3 on both sides, and the top ends of the side windshield plates 6 are folded outwards; the side windshield plates 6 are used to connect the tip end with the belly ground of the aircraft to reduce stress concentration at the arc angle of the tip end.

[0020] The utility model has an arc-shaped cover body 2 made of organic glass and having a hyperbolic shape, with a curvature of 0.008 to 0.01, which reduces wind resistance during flight; the windshield is made of organic glass, has good light transmittance, and has a good forward field of vision; the force transmission frame 3 reduces air resistance and prevents cracks from forming on the arc-shaped cover body; the side windshield plate 6 is used to connect the outer surface of the belly skin of the aircraft to reduce stress concentration at the arc angle at the tip; the fitting frame 1, the lateral support assembly and the C-shaped connection assembly reduce the vibration of the windshield and prevent the windshield from shaking and causing damage.

[0021] The utility model is convenient for maintenance and effectively protects the airborne optical equipment and instruments.

Claims

1. A visual anti-vibration windshield, characterized in that: It comprises a cover body fitting frame (1), an arc-shaped cover body (2) embedded in the cover body fitting frame (1), lateral support components arranged on both sides of the cover body fitting frame (1), and a C-shaped connection component arranged on the top of the cover body fitting frame (1); The C-shaped connecting component is connected to the fuselage.

2. A visual anti-vibration windshield according to claim 1, characterized in that: The arc-shaped cover body (2) is a hyperbolic shape, and its curvature is 0.008-0.

01.

3. The visual anti-vibration windshield according to claim 1, characterized in that: The lateral support assembly comprises a force transmission frame (3) arranged on both sides of the cover body fitting frame (1) and the inner side of the bottom edge and used to prevent the slight end of the arc-shaped cover body (2) from deforming.

4. The visual anti-vibration windshield according to claim 3, characterized in that: The C-shaped connection assembly comprises an inner frame (4) arranged on the inner side of the top of the cover body fitting frame (1) and an outer frame (5) arranged on the outer side of the top of the cover body fitting frame (1); both the inner frame (4) and the outer frame (5) are connected to the fuselage.

5. The visual anti-vibration windshield according to claim 4, characterized in that: Triangular side wind shields (6) are arranged on the outer sides of the force transmission frames (3) on both sides, and the top ends of the side wind shields (6) are folded outwards.

6. The visual anti-vibration windshield according to claim 5, characterized in that: The arc-shaped cover body (2) is made of organic glass.

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