Anti-mite airplane window shade

Abstract

The utility model discloses an anti-mite airplane window shade, which comprises a curtain main body, a dismounting mechanism is arranged on the curtain main body and is used for conveniently dismounting and cleaning the airplane window shade, the dismounting mechanism comprises a curtain strip, a rotating shaft, a sliding track and a bolt block, the curtain strip is arranged on the rotating shaft, and the bolt block is arranged on the rotating shaft. The curtain strips comprise chitin fiber knitted layers and linen fiber layers, the two sides of each linen fiber layer are each provided with one chitin fiber knitted layer, the rotating shafts are rotationally connected to the curtain body, and the chitin fiber knitted layers are arranged on the linen fiber layers, so that the anti-mite effect is achieved; the bolt block is fixed in a sliding mode along the sliding rail in the rotating shaft, the lifting rod is driven to slide downwards by pressing the pressing plate, the curtain strip is placed into the bolt block, the pressing plate is loosened, the sliding column is inserted into the mounting hole in the curtain strip in a sliding mode through the reset spring connected to the lifting rod in a sleeving mode, the effect of rapid assembly and disassembly is achieved, and the curtain strip is convenient to clean and air. And the usability of the equipment is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of textile fabrics, in particular to an anti-mite aircraft blackout curtain. Background Art

[0002] There are various types of blackout curtains on the market. With the advancement of textile technology, the styles of blackout curtains can far meet people's demands for the appearance of blackout curtains.

[0003] Existing anti-mite aircraft blackout curtains, such as an anti-mite blackout curtain disclosed in Chinese patent application CN205457969U, record: comprising a plurality of rectangular curtain strips, the curtain strips are arranged up and down, the longer sides of each curtain strip are parallel to each other, the upper edge of the curtain strip located below is connected to the middle position of the back side of the curtain strip immediately above it by a connecting piece, and the connecting piece is arranged horizontally: a chitin fiber knitted layer is provided on both sides of the curtain strip.

[0004] After the above-mentioned anti-mite blackout curtains have been used for too long, their stickiness will decrease with time and frequency of use, and they need to be replaced frequently. In addition, the mesh of the Velcro is relatively fine, which is easily contaminated with dust and difficult to clean. If it is not cleaned in time, dust will accumulate to a certain extent, which will not only affect the appearance, but also affect the sanitary conditions of the surrounding environment, attract more mites, and bring potential risks to the health of passengers. Utility Model Content

[0005] 1. Technical issues to be solved

[0006] In view of the deficiencies in the prior art, the utility model provides an anti-mite aircraft blackout curtain, which has the advantages of convenient disassembly and the like, and solves the problem of Velcro disassembly.

[0007] (II) Technical solution

[0008] To achieve the above, the utility model not only solves the problem of Velcro disassembly method, but also ensures the purpose of curtain storage, and provides the following technical solutions: an anti-mite aircraft blackout curtain, comprising a curtain main body, a disassembly mechanism is installed on the curtain main body, for convenient disassembly and cleaning of the aircraft blackout curtain, the disassembly mechanism comprises a curtain strip, a rotating shaft, a sliding track and a latch block, the curtain strip is installed on the rotating shaft, the curtain strip comprises a chitosan fiber knitted layer and a flax fiber layer, a chitosan fiber knitted layer is provided on both sides of the flax fiber layer, the rotating shaft is rotatably connected to the curtain main body, the sliding track is opened on the rotating shaft, and the latch block is slidably connected to the sliding track.

[0009] As a preferred solution of the anti-mite aircraft blackout curtain of the utility model, the inner wall of the latch block is slidably connected with a lifting rod, and a return spring is sleeved on the lifting rod.

[0010] As a preferred solution of the anti-mite aircraft blackout curtain of the utility model, a sliding column is fixedly connected to the lifting rod, and the sliding column is inserted into the curtain strip.

[0011] As a preferred solution of the anti-mite aircraft blackout curtain of the utility model, a pressing plate is provided on one side of the latch block, and one end of the lifting rod away from the return spring is fixedly connected to the pressing plate.

[0012] As a preferred solution of the anti-mite aircraft blackout curtain of the utility model, one end of the rotating shaft is fixedly connected to a sliding shaft, the end of the rotating shaft away from the sliding shaft is rotatably connected to a rotating block, and the rotating block is hinged to a fixed block.

[0013] As a preferred solution of the anti-mite aircraft blackout curtain of the utility model, the fixing block is fixedly connected to a storage box, and the inner wall of the storage box is slidably connected to a sliding door.

[0014] Compared with the known prior art, the technical solution provided by the utility model has the following beneficial effects:

[0015] 1. The chitin fiber knitted layer on the flax fiber layer has an anti-mite effect. The latch block slides and is fixed along the sliding track in the rotating shaft. The lifting rod is driven down by pressing the pressing plate, and the curtain strip is placed into the latch block. The pressing plate is released, and the sliding column is slid into the mounting hole on the curtain strip through the reset spring sleeved on the lifting rod, which plays a role in quick loading and unloading, facilitates the cleaning and drying of the curtain strips, and increases the usability of the equipment.

[0016] 2. Push the sliding door to open it, pull the rotating shaft to make the sliding shaft slide out along the sliding track on one side of the storage box, and hinge the rotating block to the fixed block, which is convenient for inspection and maintenance. The setting of the sliding door can protect the curtain strips and prevent them from being damaged or dust accumulated. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] In order to more clearly illustrate the embodiments of the utility model or the technical solutions in the prior art, the drawings required for use in the embodiments or the prior art descriptions are briefly introduced below. Obviously, the drawings described below are only some embodiments of the utility model, and for ordinary technicians in this field, other drawings can be obtained based on these drawings without creative work.

[0018] Figure 1 It is a three-dimensional overall structural schematic diagram of the utility model;

[0019] Figure 2 This is a structural schematic diagram of the curtain strip of the utility model;

[0020] Figure 3 This is a schematic diagram of the structure of the planed surface of the curtain strip of the utility model;

[0021] Figure 4 This is a schematic diagram of the structure of the enlarged portion of the curtain strip A of the utility model;

[0022] Figure 5 It is a structural schematic diagram of a storage box of the present utility model.

[0023] In the figure: 100, curtain body; 200, disassembly mechanism; 201, curtain strip; 011, chitin fiber knitted layer; 012, flax fiber layer; 202, rotating shaft; 203, sliding track; 204, latch block; 205, lifting rod; 206, return spring; 207, sliding column; 208, pressing plate; 209, sliding shaft; 210, rotating block; 211, fixed block; 212, storage box; 213, sliding door. DETAILED DESCRIPTION

[0024] In order to make the purpose, technical solution and advantages of the embodiment of the utility model clearer, the technical solution in the embodiment of the utility model will be clearly and completely described below in conjunction with the drawings in the embodiment of the utility model. Obviously, the described embodiment is a part of the embodiment of the utility model, not all of the embodiments. Based on the embodiment of the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0025] The utility model is further described below in conjunction with embodiments.

[0026] Example 1

[0027] Reference Figure 1-4 , which is the first embodiment of the utility model, provides an anti-mite aircraft blackout curtain, the anti-mite aircraft blackout curtain comprising a curtain body 100, a disassembly mechanism 200 is installed on the curtain body 100, for facilitating the disassembly and cleaning of the aircraft blackout curtain;

[0028] The disassembly mechanism 200 includes a curtain strip 201, a rotating shaft 202, a sliding track 203 and a latch block 204. The curtain strip 201 is installed on the rotating shaft 202. The curtain strip 201 includes a chitosan fiber knitted layer 011 and a flax fiber layer 012. A layer of chitosan fiber knitted layer 011 is provided on both sides of the flax fiber layer 012. The rotating shaft 202 is rotatably connected to the curtain body 100. The sliding track 203 is provided on the rotating shaft 202. The latch block 204 is slidably connected to the sliding track 203 through the chitosan fiber knitted layer 011 provided on the flax fiber layer 012, which plays an anti-mite role. The latch block 204 is slidably fixed along the sliding track 203 in the rotating shaft 202.

[0029] The inner wall of the latch block 204 is slidably connected with a lifting rod 205, and a reset spring 206 is sleeved on the lifting rod 205. The reset spring 206 drives the lifting rod 205 to reset.

[0030] A sliding column 207 is fixedly connected to the lifting rod 205, and the sliding column 207 is inserted into the curtain strip 201. The setting of the sliding column 207 plays a fixing role. The sliding column 207 is slidably inserted into the mounting hole on the curtain strip 201 to fix it.

[0031] A pressing plate 208 is provided on one side of the latch block 204 , and one end of the lifting rod 205 away from the return spring 206 is fixedly connected to the pressing plate 208 . By pressing the pressing plate 208 , the lifting rod 205 is driven to slide down, so that the sliding column 207 lowers the curtain strip 201 .

[0032] During use, the chitin fiber knitted layer 011 provided on the flax fiber layer 012 plays an anti-mite role, the latch block 204 slides and is fixed along the sliding track 203 in the rotating shaft 202, and the lifting rod 205 is driven to slide down by pressing the pressing plate 208, and the curtain strip 201 is placed in the latch block 204, and the pressing plate 208 is released. The sliding column 207 is slid and inserted into the installation hole on the curtain strip 201 through the return spring 206 sleeved on the lifting rod 205, which plays a role in quick loading and unloading, facilitates the cleaning and drying of the curtain strip 201, and increases the usability of the equipment.

[0033] Example 2

[0034] Reference Figure 1-5 , which is the second embodiment of the utility model, provides an anti-mite aircraft blackout curtain, which includes one end of a rotating shaft 202 fixedly connected to a sliding shaft 209, an end of the rotating shaft 202 away from the sliding shaft 209 rotatably connected to a rotating block 210, the rotating block 210 is hinged to a fixed block 211, and the rotating block 210 rotates along the fixed block 211 to make the sliding shaft 209 slide out, driving the rotating shaft 202 to move out.

[0035] The fixed block 211 is fixedly connected with a storage box 212, and the inner wall of the storage box 212 is slidably connected with a sliding door 213. The setting of the sliding door 213 plays a role in protecting and storing the curtain strips 201.

[0036] During use, the sliding door 213 is pushed to open it, and the sliding shaft 209 is pulled out along the sliding track on one side of the storage box 212 by pulling the rotating shaft 202. The rotating block 210 is hinged to the fixed block 211, which facilitates inspection and maintenance. The setting of the sliding door 213 plays a role in protecting the stored curtain strips 201 and preventing the curtain strips 201 from being damaged.

[0037] The remaining structure is the same as that of Example 1.

[0038] The above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit it. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that the technical solutions described in the aforementioned embodiments may still be modified, or some of the technical features may be replaced by equivalents. Such modifications or replacements will not cause the essence of the corresponding technical solutions to deviate from the protection scope of the technical solutions of the embodiments of the present invention.

Claims

1. An anti-mite aircraft blackout curtain, comprising a curtain body (100), characterized in that: A disassembly mechanism (200) is installed on the curtain body (100) for facilitating disassembly and cleaning of the aircraft blackout curtain; The disassembly mechanism (200) comprises a curtain strip (201), a rotating shaft (202), a sliding track (203) and a latch block (204); the curtain strip (201) is mounted on the rotating shaft (202); the curtain strip (201) comprises a chitosan fiber knitting layer (011) and a flax fiber layer (012); both sides of the flax fiber layer (012) are provided with a layer of chitosan fiber knitting layer (011); the rotating shaft (202) is rotatably connected to the curtain body (100); the sliding track (203) is provided on the rotating shaft (202); and the latch block (204) is slidably connected to the sliding track (203).

2. The anti-mite aircraft blackout curtain according to claim 1, characterized in that: The inner wall of the latch block (204) is slidably connected with a lifting rod (205), and a return spring (206) is sleeved on the lifting rod (205).

3. The anti-mite aircraft blackout curtain according to claim 2, characterized in that: A sliding column (207) is fixedly connected to the lifting rod (205), and the sliding column (207) is plugged into the curtain strip (201).

4. The anti-mite aircraft blackout curtain according to claim 2, characterized in that: A pressing plate (208) is provided on one side of the latch block (204), and one end of the lifting rod (205) away from the return spring (206) is fixedly connected to the pressing plate (208).

5. The anti-mite aircraft blackout curtain according to claim 1, characterized in that: One end of the rotating shaft (202) is fixedly connected to a sliding shaft (209), and one end of the rotating shaft (202) away from the sliding shaft (209) is rotatably connected to a rotating block (210), and the rotating block (210) is hinged to a fixed block (211).

6. The anti-mite aircraft blackout curtain according to claim 5, characterized in that: The fixed block (211) is fixedly connected to a storage box (212), and the inner wall of the storage box (212) is slidably connected to a sliding door (213).

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