CN216887187U - Take aircraft casing of sign function - Google Patents

Abstract

The utility model relates to an aircraft shell with an identification function, which comprises a shell body, wherein the shell body is formed by connecting an upper shell and a lower shell, and one or more connecting covers are arranged at the joint of the upper shell and the lower shell on the shell body; the connecting cover is provided with an identification part which is used for carrying out identification display by depending on external light, and the shell is internally provided with a light-emitting component which emits light towards the identification part; assemble epitheca and inferior valve through connecting the lid to through the light-emitting component who sets up in the equipment back casing to connecting the sign portion of covering and sending light, the sign is shown to the sign portion, and this utility model possesses that the structure is succinct, easy dismounting just can have the sign characteristics of preferred.

Description

Take aircraft casing of sign function

Technical Field

The utility model relates to the technical field of space race tracks, in particular to an aircraft shell with a marking function.

Background

The spatial track is a novel entertainment mode which is raised in recent years, and is different from the traditional track in that the track is used for competition, a remote control racing car is not used for competition, but a novel remote aircraft is used for competition;

at present, the shell of the aircraft applied to the space track is complex in structure, inconvenient to assemble and disassemble and does not have the identification function.

SUMMERY OF THE UTILITY MODEL

Aiming at the existing defects, the utility model provides an aircraft shell with an identification function.

The technical scheme adopted by the utility model for solving the technical problems is as follows: an aircraft shell with a marking function comprises a shell body, wherein the shell body is formed by connecting an upper shell and a lower shell, and one or more connecting covers are arranged at the connecting position of the upper shell and the lower shell on the shell body; the connecting cover is provided with an identification part which is used for identifying and displaying by means of external light, and the shell is internally provided with a light-emitting component which faces the identification part and emits light.

Preferably, the connection cover is detachably connected to both the upper case and the lower case.

Preferably, the connecting cover is provided with a plurality of buckles in a circular ring shape, and the upper shell and the lower shell are provided with clamping grooves corresponding to the buckles.

Preferably, the light-emitting assembly comprises a light-emitting lamp and a light-ray shaping piece for changing the shape of light rays emitted by the light-emitting lamp; the inside connection of casing is provided with the installation support of installation light emitting component.

Preferably, the connecting covers are annularly arranged on the shell, and gaps between the connecting covers and adjacent propellers of the aircraft in the shell are arranged in a manner of being opposite to each other one by one.

Preferably, the indicator is formed of a plurality of light-transmitting holes.

Preferably, the identification portion is made of a fluorescent material.

Preferably, a plurality of hollow holes are formed in the upper shell and the lower shell.

Preferably, the cross sections of the upper shell and the lower shell are any one of rectangular, semicircular, trapezoidal and oval.

The utility model has the beneficial effects that: the epitheca and inferior valve are connected through the connecting piece that sets up on epitheca and inferior valve and are constituted, and the connection lid that epitheca and inferior valve junction set up simultaneously to through the light-emitting component who sets up in the casing after the equipment to the sign portion of connecting covering send light, sign portion shows the sign, and the structure is succinct, easy dismounting just can have the sign effect of preferred.

Drawings

FIG. 1 is a schematic structural diagram of an embodiment of the present invention;

FIG. 2 is a schematic structural view of a housing according to an embodiment of the present invention;

FIG. 3 is a schematic view of a connecting cover according to an embodiment of the present invention;

FIG. 4 is a schematic view of a mounting bracket configuration of an embodiment of the present invention;

fig. 5 is a schematic structural diagram of a light emitting device according to an embodiment of the utility model.

Part names and serial numbers in the figure: 1-shell 10-upper shell 11-lower shell 12-connecting cover 13-buckle 14-card slot 15-mounting support 16-hollow hole 2-light-emitting component 20-light-emitting lamp 21-light beam shaping piece.

Detailed Description

To more clearly illustrate the objects, technical solutions and advantages of the embodiments of the present invention, the present invention will be further described in detail with reference to the accompanying drawings and embodiments, and it is obvious that the described embodiments are some, but not all embodiments of the present invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments of the present invention without inventive step, are within the scope of the present invention. In addition, directional terms used in the present invention, such as "upper", "lower", "front", "rear", "left", "right", "inner", "outer", etc., refer to directions only as shown in the attached drawings, and are used for better and clearer explanation and understanding of the present invention, and do not indicate or imply orientation which the present invention must have, and thus, should not be construed as limiting the present invention.

Embodiment of the utility model as shown in fig. 1 to 5, an aircraft shell with a marking function comprises a shell 1, wherein the shell 1 is formed by connecting an upper shell 10 and a lower shell 11, and one or more connecting covers 12 are arranged on the shell 1 at the joint of the upper shell 10 and the lower shell 11; the connecting cover 12 is provided with an identification part which is identified and displayed by means of external light, and the shell 1 is internally provided with a light-emitting component 2 which faces the identification part and emits light.

It should be noted that the upper shell 10 and the lower shell 11 are connected by a ring-shaped connecting piece arranged on the upper shell 10 and the lower shell 11, and a special rotary self-locking structure is provided; the connecting cover 12 not only plays a role of assisting in connecting the upper shell 10 and the lower shell 11, but also plays a role of shielding an LED light source of an aircraft and protecting eyes of an operator; the stability and the strength of the structure are further enhanced, the identification part on the connecting cover 12 emits light through the light-emitting component 2 arranged in the assembled shell 1, and the identification part displays identification to play a role in identifying the direction of the aircraft body; the structure is succinct, easy dismounting just can have the marking effect of preferred.

Further, as shown in fig. 1 to 2, the connection cover 12, the upper case 10 and the lower case 11 are detachably connected, and the utility model includes other detachable connection modes except for the mode that the buckle 13 and the slot 14 match the clamping, and different installation modes are selected according to actual conditions, so that the utility model has wider application scenarios.

In a further improvement, as shown in fig. 2 to 3, in the embodiment of the present invention, a plurality of buckles 13 are distributed on the connecting cover 12 in a circular ring shape, and the upper shell 10 and the lower shell 11 are both provided with a clamping groove 14 corresponding to the buckles 13; buckle 13 and draw-in groove 14 phase-match can make the position of epitheca 10 and inferior valve 11 more firm, also can let this utility model at the dismouting in-process simpler and easier simultaneously.

In a further improvement, as shown in fig. 5, the light assembly 2 includes a light emitting lamp 20 and a light-shaping unit 21 for shaping the light emitted from the light emitting lamp 20, wherein the light emitting lamp 20 can emit light, and the light-shaping unit 21 can change the light emitted from the light emitting lamp 20 into various shapes, such as trapezoid, diamond, triangle, rectangle, etc.; the light shaping element 21 can be formed by existing equipment; the internal connection of casing 1 is provided with the installation light emitting component 2's installing support 16, and installing support 16 also can let casing 1 more firm for light emitting component 2 provides the installation place simultaneously.

In a further improvement, as shown in fig. 4, in the embodiment of the present invention, a plurality of the connection covers 12 are annularly arranged on the housing 1, and the connection covers 2 are arranged opposite to adjacent propellers of the aircraft in the housing 1 in a one-to-one manner with gaps therebetween, and form an angle of 90 degrees with the propellers at the center of the whole sphere, and the four symmetrical positions of the housing closest to the rotating outer ring of the propellers play a better role in preventing foreign matters from entering the interior and improving the safety of personnel.

In a preferred mode, the identification part is directly the whole of the connection cover 12 or a part of the connection cover 12, and the connection cover 12 is made of a transparent or semi-transparent material, and the transparent material is uniform, specific figures and characters are engraved, and the identification part is projected by a rear light source to play a role in highlighting the identification and the transparent effect.

Another alternative embodiment is: the sign portion is formed by a plurality of light transmission holes or light transmission grooves provided in the connection cover 12, and the light emitted from the light emitting element 2 can be emitted from the outside of the housing 1 through the light transmission holes to form a sign by the light emitting shape.

Another alternative embodiment is: the mark part is made of fluorescent material, and when the light emitted by the light emitting component 2 reaches the mark part, the mark part absorbs the light and then emits light; when made of fluorescent material, the identification part may be disposed on the connection cover 12, or may be connected with the connection cover 12 through a connector, but it is preferable that the connection is performed through a connector.

In a further improvement, as shown in fig. 1 to 2, a plurality of hollowed holes 16 are formed in both the upper shell 10 and the lower shell 11, and the hollowed holes 16 not only make the utility model more beautiful, but also make the bearing capacity of the shell 1 more enhanced, just like a spider web.

In a further improvement, as shown in fig. 1 to 2, the cross sections of the upper shell 10 and the lower shell 11 are any one of rectangular, semicircular, trapezoidal and elliptical, so that a user can select the shells 1 with different shapes according to actual use conditions, and the diversity of the utility model is increased.

It will be understood that modifications and variations can be made by persons skilled in the art in light of the above teachings and all such modifications and variations are intended to be included within the scope of the utility model as defined in the appended claims.

Claims (10)

1. The utility model provides a take aircraft casing of sign function which characterized in that: the shell is formed by connecting an upper shell and a lower shell, and one or more connecting covers are arranged at the joint of the upper shell and the lower shell on the shell; the connecting cover is provided with an identification part which is used for identifying and displaying by means of external light, and the shell is internally provided with a light-emitting component which faces the identification part and emits light.

2. The aircraft shell with identification function of claim 1, wherein the connecting cover is detachably connected to both the upper shell and the lower shell.

3. The aircraft shell with the identification function as claimed in claim 2, wherein the connecting cover is provided with a plurality of buckles distributed in a circular ring shape, and the upper shell and the lower shell are provided with clamping grooves corresponding to the buckles.

4. The aircraft shell with identification function of claim 1, wherein the light assembly comprises a light lamp and a light shaping element for changing the shape of the light emitted by the light lamp; the inside connection of casing is provided with the installation support of installation light emitting component.

5. The aircraft shell with the identification function as claimed in claim 1, wherein the connecting covers are annularly arranged on the shell, and gaps between the connecting covers and adjacent propellers of the aircraft in the shell are arranged in a one-to-one opposite mode.

6. The aircraft shell with identification function of any one of claims 1 to 5, wherein the identification portion is made of a transparent or semi-transparent material.

7. The aircraft housing with identification function of any one of claims 1-5, wherein said identification portion is formed by a plurality of light-transmitting holes.

8. The aircraft shell with identification function of any one of claims 1 to 5, wherein the identification portion is made of a fluorescent material.

9. The aircraft shell with identification function of any one of claims 1-5, wherein a plurality of hollowed-out holes are formed on both the upper shell and the lower shell.

10. The aircraft shell with identification function of any one of claims 1-5, wherein the upper shell and the lower shell have any one of a rectangular, semicircular, trapezoidal and oval cross section.

Images