CN219082921U - Temporary protective lampshade for aircraft manufacturing - Google Patents

Abstract

The utility model discloses a temporary protective lampshade for aircraft manufacture, which comprises a lampshade body and an adhesive layer, wherein the middle of the lampshade body is sunken, the edge of the lampshade body is a plane, a warning area is arranged around the sunken position on the plane close to the sunken position, the adhesive layer is arranged at the edge of the lampshade body and used for adhering the lampshade to the position where a lamp is located, the temporary protective lampshade is arranged to realize temporary protection in the aircraft manufacture process, the use is convenient, the installation mode of double-sided adhesive can be directly used for adhering and installing, soft silica gel material can play the effect of preventing collision injury, plays a certain role in protecting the lamp and simultaneously plays an insulating role, the lampshade of the soft silica gel material can realize good adhesion, the condition of not tightly adhering is guaranteed, the adhesion is good, the soft silica gel material is light in weight, the pressure of the adhesive layer is smaller, the double-sided adhesive installation can be realized more conveniently, and no punching or any installation structure is required.

Description

Temporary protective lampshade for aircraft manufacturing

Technical Field

The utility model belongs to the technical field of aircraft manufacturing, and particularly relates to a temporary protective lampshade for aircraft manufacturing.

Background

When the aircraft is manufactured, a plurality of scenes for installing the lamp exist, and the subsequent procedures also need to be used for lighting, but when the lamp is installed, other installation such as covering, paint spraying and the like is needed for the aircraft, so that the aircraft is always in a bare state after the lamp is installed, the danger of dust entering and collision and touching by collision exists, the lamp is impacted and has damage and leakage risks, therefore, a lampshade capable of protecting the temporary lamp is needed, the lampshade is required to be stably installed, convenient and fast to detach and free from leaving installation marks, and the possible collision of operators can be protected in the use process, so that the lamp is not damaged and the leakage risks are avoided.

Disclosure of Invention

In order to overcome the defects, the inventor of the utility model continuously reforms and innovates through long-term exploration and repeated experiments and efforts, and provides a temporary protective lampshade for aircraft manufacture, which is provided with the temporary protective lampshade, so that temporary protection in the aircraft manufacturing process is realized, the use is convenient, the installation mode of double-sided adhesive can be directly stuck and installed, the soft silica gel material can play the role of preventing people from being injured, a certain protection is realized for a lamp, meanwhile, the insulation effect is realized, the lampshade of the soft silica gel material can realize good lamination, the condition of unsmooth lamination is ensured, the lamination performance is good, the soft silica gel material is light in weight, the pressure on a sticking layer is small, the double-sided adhesive installation can be realized conveniently, the adopted double-sided adhesive is colloid (such as 3m colloid) without residual adhesive, the extra cleaning burden on the aircraft manufacturing in the use process of the lampshade can be avoided, and any influence on the aircraft body is avoided, and any punching or installation structure is not required.

The technical scheme adopted by the utility model for achieving the purpose is as follows: a temporary protective lampshade for aircraft manufacture is provided. The lamp comprises a cover body and a pasting layer, wherein the middle of the cover body is sunken, the edge of the cover body is a plane, a warning area is arranged around the sunken part on the plane close to the sunken part, and the pasting layer is arranged on the edge of the cover body and used for pasting the cover at the position where the lamp is located.

According to the utility model, the aircraft manufacturing temporary protective lampshade comprises the following further preferred technical scheme: the cover body is made of transparent silica gel.

According to the utility model, the aircraft manufacturing temporary protective lampshade comprises the following further preferred technical scheme: the warning area is composed of a warning paste or a warning coating, the warning paste is a yellow-black or red-black alternative paste paper, and the warning coating is a yellow-black or red-black alternative stripe directly printed on the cover body.

According to the utility model, the aircraft manufacturing temporary protective lampshade comprises the following further preferred technical scheme: the stripes of the warning area are arranged in a regular hexagon, the concave position is positioned in the middle, and a lamp shade model mark is arranged beside the warning area.

According to the utility model, the aircraft manufacturing temporary protective lampshade comprises the following further preferred technical scheme: the adhesive layers are arranged at intervals around the six sides of the warning area, and the adhesive layers are parallel to the warning welt.

According to the utility model, the aircraft manufacturing temporary protective lampshade comprises the following further preferred technical scheme: the pasting layer adopts a double faced adhesive tape form, one face contacted with the cover body is directly pasted on the cover body, and the face contacted with the plane wall surface is covered with the isolation paper.

According to the utility model, the aircraft manufacturing temporary protective lampshade comprises the following further preferred technical scheme: the concave is concave towards the lower surface, the shape of the concave is hemispherical or semi-ellipsoidal, and the lowest part of the concave is a plane structure.

According to the utility model, the aircraft manufacturing temporary protective lampshade comprises the following further preferred technical scheme: the warning area is located the lower surface of the cover body, and the adhesion layer is located the upper surface of the cover body.

According to the utility model, the aircraft manufacturing temporary protective lampshade comprises the following further preferred technical scheme: the cover body is circular, and the recess is located the central point.

Compared with the prior art, the technical scheme of the utility model has the following advantages/beneficial effects:

1. the temporary protective lampshade is arranged, temporary protection in the aircraft manufacturing process is achieved, the use is convenient, the installation mode of double-sided adhesive tape can be directly pasted and installed, the soft silica gel material can play a role in preventing people from being injured, certain protection is achieved on the lamp, and meanwhile the insulation effect is achieved.

2. The lamp shade of soft silica gel material can realize good laminating, guarantees not taking place the inseparable condition of laminating, and laminating nature is good, and soft silica gel material light in weight is less to the pressure of pasting the layer, can be comparatively convenient realization double faced adhesive tape installation, and the double faced adhesive tape that adopts is the colloid (like 3m glues) that do not stay the residual glue, can avoid the lamp shade in-process to cause extra clean burden to aircraft manufacturing, can not cause any influence to the aircraft organism, need not to punch or set up any mounting structure.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings that are needed in the embodiments will be briefly described below, it being understood that the following drawings only illustrate some examples of the present utility model and therefore should not be considered as limiting the scope, and other related drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.

Fig. 1 is a schematic perspective view of a temporary protective lampshade for an aircraft.

Fig. 2 is a schematic view of the bottom structure of a temporary protective lampshade for an aircraft.

The marks in the figure are respectively: 1. cover 101, concave 102, plane 2, adhesive layer 3 and warning area.

Detailed Description

To make the objects, technical solutions and advantages of the present utility model more apparent, the technical solutions in the embodiments of the present utility model will be clearly and completely described below, and it is apparent that the described embodiments are some embodiments of the present utility model, but not all embodiments. All other embodiments, based on the embodiments of the utility model, which are apparent to those of ordinary skill in the art without inventive faculty, are intended to be within the scope of the utility model. Accordingly, the detailed description of the embodiments of the utility model provided below is not intended to limit the scope of the utility model as claimed, but is merely representative of selected embodiments of the utility model.

It should be noted that: like reference numerals and letters denote like items in the following figures, and thus, once an item is defined in one figure, it may not be further defined and explained in the following figures.

Examples:

as shown in fig. 1-2, an aircraft manufacturing temporary protective lampshade comprises a lampshade body 1 and an adhesive layer 2, wherein a concave 101 is formed in the middle of the lampshade body 1, the edge of the lampshade body is a plane 102, a warning area 3 is arranged around the concave 101 on the plane 102 close to the position of the concave 101, and the adhesive layer 2 is arranged on the edge of the lampshade body 1 and used for adhering the lampshade to the position of a lamp.

The cover body 1 is made of transparent silica gel materials, so that the cover body can be tightly attached to the surface to be attached, light transmission can be realized, meanwhile, the soft silica gel materials can buffer accidental impact, damage to a lamp is avoided, damage to personnel is avoided, the silica gel is an insulating material, and when the impact force is too large, the lamp is damaged, and electric shock accidents cannot occur. The soft silica gel can not damage the surface of the airplane.

The warning area 3 is formed by a warning paste or a warning coating, the warning paste is yellow-black or red-black alternate paste paper, the warning coating is yellow-black or red-black alternate stripes directly printed on the cover body 1, and the warning area 3 mainly plays a warning role, so long as the warning can be clearly prompted. A lamp shade model mark is arranged beside the warning area 3, so that the correct model can be conveniently selected when the lamp shade is installed.

The warning areas 3 are arranged in a regular hexagon, the positions of the concave areas 101 are located in the middle, warning patches are required to be conspicuous and regular enough, direct attention is convenient to be paid, dangerous areas are marked, and therefore the warning patches are arranged around the positions of the concave areas 101.

The adhesive layers 2 are arranged around the six sides of the warning area 3 at intervals, and the adhesive layers 2 are parallel to the sides of the warning area 3, so that the adhesive positions cannot influence the warning area 3.

The adhesive layer 2 is in a double-sided adhesive form, one surface in contact with the cover body 1 is directly adhered to the cover body 1, the surface in contact with the aircraft wall surface is covered with release paper, and when the adhesive layer 2 is used, the release paper is torn off to be adhered, so that no adhesive mark is left after the release, materials such as 3m adhesive are needed, and when necessary, the adhesive layer 2 can be adhered again and is firm after the adhesive layer is temporarily peeled off and is installed.

The adhesive layer 2 is evenly arranged around the edge of the cover body 1, the adhesive layer 2 is located on the upper surface of the cover body 1, the adhesive layer 2 is evenly arranged to ensure firm adhesion, no wrinkles are generated, no dropping occurs under the action of external force, and stable protection is ensured.

The concave 101 is concave 101 towards the lower surface, the shape of the concave 101 is hemispherical or semi-ellipsoidal, the shape of the concave 101 can be specifically set according to requirements, the hemispherical or semi-ellipsoidal is convenient and fast to process, the concave 101 is attractive, and the image of a lampshade can be formed.

The warning area 3 is located the lower surface of the cover body 1, the adhesive layer 2 is located the upper surface of the cover body 1, the warning area 3 is located the lower surface more obviously, and the blurring can not be avoided.

The cover body 1 is circular, the concave 101 is positioned at the central position, the circular shape of the cover body 1 can form complete coverage on the installation positions of lamps with various shapes, the direction requirement does not exist, the installation is convenient, and the shape of the cover body 1 can be changed according to specific requirements.

In the description of the present utility model, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings are merely for convenience in describing the present utility model and simplifying the description, and do not indicate or imply that the apparatus or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present utility model.

In the present utility model, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. The specific meaning of the above terms in the present utility model can be understood by those of ordinary skill in the art according to the specific circumstances.

The foregoing is merely a preferred embodiment of the present utility model, and it should be noted that the above-mentioned preferred embodiment should not be construed as limiting the utility model, and the scope of the utility model should be defined by the appended claims. It will be apparent to those skilled in the art that various modifications and adaptations can be made without departing from the spirit and scope of the utility model, and such modifications and adaptations are intended to be comprehended within the scope of the utility model.

Claims (9)

1. The temporary protective lampshade is characterized by comprising a lampshade body and a pasting layer, wherein the middle of the lampshade body is sunken, the edge of the lampshade body is a plane, a warning area is arranged around the sunken part on the plane close to the sunken part, and the pasting layer is arranged on the edge of the lampshade body and used for pasting the lampshade at the position where a lamp is located.

2. The aircraft-made temporary protective cover according to claim 1, wherein the cover is made of light-transmitting silicone material.

3. The temporary protective cover for an aircraft according to claim 1, wherein the warning area is formed by a warning patch or a warning coating, the warning patch is a yellow-black or red-black-alternate paste patch, and the warning coating is a yellow-black or red-black alternate stripe directly printed on the cover body.

4. An aircraft manufacturing temporary protective cover according to claim 3, wherein the stripes of the warning area are arranged in a regular hexagon, the concave position is located in the middle, and a cover model mark is arranged beside the warning area.

5. The aircraft-made temporary protective cover of claim 4, wherein the adhesive layers are spaced around the periphery of the alert area and are parallel to the alert welt.

6. The temporary protective cover for aircraft according to claim 1, wherein the adhesive layer is in the form of double-sided tape, and the surface of the adhesive layer contacting the cover is directly adhered to the cover, and the surface contacting the wall of the aircraft is covered with a piece of release paper.

7. An aircraft manufacturing temporary protective lampshades according to claim 1, wherein the recess is concave towards the lower surface, the recess being hemispherical or semi-ellipsoidal in shape and the lowest part of the recess being planar.

8. The aircraft-made temporary protective cover according to claim 1, wherein the warning area is located on a lower surface of the cover body, and the adhesive layer is located on an upper surface of the cover body.

9. The aircraft manufacturing temporary protective cover according to claim 1, wherein the cover is circular and the recess is centrally located.

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