CN213862704U - External camera device of aircraft - Google Patents

Abstract

The utility model provides an external camera device of aircraft, includes the aircraft main part, aircraft main part top is equipped with camera device, camera device is connected with the supporting seat, supporting seat bottom fixed connection is in clamp plate one, clamp plate one bottom is equipped with presss from both sides tight layer one, press from both sides tight layer one surface contact aircraft main part, clamp plate one surface both sides are installed joint spare, joint spare is connected with the tie up area, clamp plate one is connected in clamp plate two through tying up the area, two surface connection of clamp plate have and press from both sides tight layer two, press from both sides two surface contact aircraft main parts on the tight layer.

Description

External camera device of aircraft

Technical Field

The utility model relates to an aircraft equipment field, in particular to external camera device of aircraft.

Background

Unmanned aerial vehicle aircraft has received liking of many people as the remote control flying device that has risen in recent years, and unmanned aerial vehicle aircraft is a mode of shooing through the unmanned aerial vehicle aircraft, when using the unmanned aerial vehicle aircraft to shoot, and some unmanned aerial vehicle aircraft of low price do not have special camera device, need install special camera device on the unmanned aerial vehicle aircraft. However, the existing external camera device of the aircraft has a complex structure, is difficult to install and is inconvenient to disassemble.

SUMMERY OF THE UTILITY MODEL

The utility model mainly aims at providing an external camera device of an aircraft to overcome the defects in the prior art;

in order to solve the technical problem, the utility model provides a following technical scheme:

an external camera device of an aircraft comprises an aircraft body 6, wherein a camera device 1 is arranged above the aircraft body 6, the camera device 1 is connected with a supporting seat 7, the bottom of the supporting seat 7 is fixedly connected with a first clamping plate 2, a first clamping layer 5 is arranged at the bottom of the first clamping plate 2, the lower surface of the first clamping layer 5 contacts with the aircraft body 6, clamping pieces 9 are arranged on two sides of the lower surface of the first clamping plate 2, the clamping pieces 9 are connected with a binding belt 8, the first clamping plate 2 is connected with a second clamping plate 3 through the binding belt 8, the upper surface of the second clamping plate 3 is connected with a second clamping layer 4, and the upper surface of the second clamping layer 4 contacts with the aircraft body 6;

optionally, two binding bands 8 are arranged, and the first clamping plate and the second clamping plate are connected through the binding bands to clamp the aircraft main body to fix the camera device;

optionally, the lower surfaces of the first clamping layer 5 and the second clamping layer 4 are arc surfaces, so that the aircraft clamping device is suitable for aircrafts in various shapes, and the contact area is increased;

optionally, the second clamping layer 4 and the first clamping layer 5 are made of soft elastic materials, so that the aircraft body can be effectively clamped and protected, and abrasion is avoided;

optionally, the camera device 1 is movably connected to the support base 7;

has the advantages that: the utility model discloses a fix camera device at clamp plate an upper surface, then come to press from both sides tightly the aircraft main part through clamp plate one and clamp plate two and take to connect fixedly through tying up, convenient operation, the installation is easy and the installation is stable, the clamp layer one and the clamp layer two of soft elasticity material can effectively protect the aircraft main part and press from both sides tightly, avoid producing wearing and tearing still can carry out certain guard action when unmanned aerial vehicle bumps the condition.

Drawings

FIG. 1 is a schematic structural view of the present invention;

the device comprises a camera device 1, a clamping plate I2, a clamping plate II 3, a clamping layer II 4, a clamping layer I5, an aircraft body 6, a supporting seat 7, a binding belt 8 and a clamping piece 9.

Detailed Description

The technical solution of the present invention will be described clearly and completely with reference to the accompanying drawings, and obviously, the described embodiments are some, but not all embodiments of the present invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases by those skilled in the art.

As shown in fig. 1, the device comprises an aircraft body 6, a camera device 1 is arranged above the aircraft body 6, the camera device 1 is connected with a supporting seat 7, the bottom of the supporting seat 7 is fixedly connected with a first clamping plate 2, a first clamping layer 5 is arranged at the bottom of the first clamping plate 2, the lower surface of the first clamping layer 5 contacts with the aircraft body 6, clamping pieces 9 are arranged on two sides of the lower surface of the first clamping plate 2, the clamping pieces 9 are connected with a binding belt 8, the first clamping plate 2 is connected with a second clamping plate 3 through the binding belt 8, the upper surface of the second clamping plate 3 is connected with a second clamping layer 4, and the upper surface of the second clamping layer 4 contacts with the aircraft body 6; the number of the binding bands 8 is two, and the first clamping plate and the second clamping plate are connected through the binding bands to clamp the aircraft main body to fix the camera device; the lower surfaces of the first clamping layer 5 and the second clamping layer 4 are arc surfaces, so that the aircraft clamping device is suitable for aircrafts in various shapes, and the contact area is increased; the second clamping layer 4 and the first clamping layer 5 are made of soft elastic materials, so that the aircraft main body can be effectively clamped and protected, and abrasion is avoided; the camera device 1 is movably connected to the supporting seat 7.

The working principle is as follows: when the device is used, the clamping pieces 9 arranged at the two ends of the first clamping plate 2 and the second clamping plate are connected through the binding belt 8 to clamp and fix the aircraft body 6, the first clamping layer 5 connected to the bottom of the first clamping plate 2 clamps the upper surface of the aircraft body 6, the second clamping layer 4 connected to the top of the second clamping plate 3 clamps the lower surface of the aircraft body 6, and the camera device can be fixed on the aircraft body 6 through the first clamping plate 2 and the second clamping plate 3 to perform flight shooting operation.

Claims (5)

1. The utility model provides an external camera device of aircraft, includes aircraft main part (6), its characterized in that: aircraft main part (6) top is equipped with camera device (1), camera device (1) is connected with supporting seat (7), supporting seat (7) bottom fixed connection is in clamp plate (2), clamp plate (2) bottom is equipped with and presss from both sides tight layer (5), press from both sides tight layer (5) lower surface contact aircraft main part (6), joint spare (9) are installed to clamp plate (2) lower surface both sides, joint spare (9) are connected with tie-up band (8), clamp plate (2) are connected in clamp plate two (3) through tie-up band (8), surface connection has clamp layer two (4) on clamp plate two (3), press from both sides tight layer two (4) upper surface contact aircraft main part (6).

2. The aircraft external camera device according to claim 1, wherein: the number of the binding bands (8) is two.

3. The aircraft external camera device according to claim 1, wherein: the lower surfaces of the first clamping layer (5) and the second clamping layer (4) are arc surfaces.

4. The aircraft external camera device according to claim 1, wherein: and the second clamping layer (4) and the first clamping layer (5) are both made of soft elastic materials.

5. The aircraft external camera device according to claim 1, wherein: the camera device (1) is movably connected to the supporting seat (7).

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