CN217907283U - Suspension rail for cabin barrier curtain of airplane - Google Patents

Suspension rail for cabin barrier curtain of airplane Download PDF

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Publication number
CN217907283U
CN217907283U CN202023329227.0U CN202023329227U CN217907283U CN 217907283 U CN217907283 U CN 217907283U CN 202023329227 U CN202023329227 U CN 202023329227U CN 217907283 U CN217907283 U CN 217907283U
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CN
China
Prior art keywords
mounting groove
aircraft cabin
sliding plate
slide
horizontal pole
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN202023329227.0U
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Chinese (zh)
Inventor
杨凯龙
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Shaanxi Chenkaishun Decoration Engineering Co ltd
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Shaanxi Chenkaishun Decoration Engineering Co ltd
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Filing date
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Priority to CN202023329227.0U priority Critical patent/CN217907283U/en
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Publication of CN217907283U publication Critical patent/CN217907283U/en
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

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  • Curtains And Furnishings For Windows Or Doors (AREA)

Abstract

The utility model discloses an aircraft cabin separates check curtain and hangs track for clip separates the check curtain, including the mounting groove, the mounting groove is seted up on the link plate in aircraft cabin, is provided with slide and dog on the mounting groove respectively, and the dog is connected with the mounting groove tight pulley, and the dog is used for stopping the slide and slides to the end of mounting groove. The bottom surface of slide is connected with the connecting rod, and the lower extreme of connecting rod is connected with the horizontal pole, and the upper surface of horizontal pole is provided with a plurality of first lacing film and a plurality of second lacing film respectively, and first lacing film and second lacing film symmetry lie in the surface of horizontal pole. Hang a plurality of forked tail through a plurality of first doctor-bars and second doctor-bar on the horizontal pole and press from both sides, saved the trouble of installing a plurality of sliders on the mounting groove, be provided with the dog equally at the right-hand member of mounting groove, can prevent that the horizontal pole from following orbital right-hand member slippage, be provided with the baffle at the leftmost end of mounting groove simultaneously, can be fine prevent that the slide from the leftmost end slippage of mounting groove, have simple structure, convenient characteristics of using well, the practicality is strong.

Description

Hanging rail for cabin barrier curtain of airplane
Technical Field
The utility model relates to an inside supplementary technical field that sets up of civil aviation aircraft cabin especially relates to an aircraft cabin separates and keeps off curtain and hang track.
Background
Economy class (economy class) is a class with a lower seat class when traveling, etc. Although the seat is not comfortable and has limited space, the seat is popular with many passengers because of the lower price. The economy class has advantages in safety. The economy class is a cheaper class space. The seats of the economic cabin of the airplane are arranged near the middle to the tail of the passenger cabin, occupy three quarters of the space of the airplane body or more, and are arranged compactly.
The individual activity space of economy class is narrow and small, and the passenger does not have oneself private space hardly, but needs have private space when partial passenger takes the aircraft, needs to regard oneself as present narrow and small space to keep apart, and this just needs to have the equipment that separates the little space specially, and the baffle device that is used for forming private space has appeared in prior art, has solved above-mentioned technical problem.
However, the general problem of the blocking device is that the structure is complex, the number of sliding blocks for clamping the blocking curtain is too many, the arrangement and the storage of the blocking curtain after the voyage are not convenient for a crew, and the blocking curtain is not convenient to clamp or take down.
SUMMERY OF THE UTILITY MODEL
To the technical problem, the utility model provides an aircraft cabin separates check curtain and hangs track sends out the centre gripping that realizes separating the check curtain through a permanent.
In order to achieve the purpose, the utility model is realized by the following technical scheme:
the utility model provides an aircraft cabin separates check curtain hanging track for clip separates the check curtain, includes the mounting groove, and on the link plate in the aircraft cabin was seted up to the mounting groove, be provided with slide and dog on the mounting groove respectively, slide and mounting groove sliding connection, the slide reciprocated sliding in the mounting groove. The dog is connected with the mounting groove tight pulley, and the dog is used for blockking the slide and slides to the end of mounting groove.
The bottom surface of slide is connected with the connecting rod, and the lower extreme of connecting rod is connected with the horizontal pole, and the upper surface of horizontal pole is provided with a plurality of first lacing films and a plurality of second lacing film respectively, and first lacing film and second lacing film symmetry lie in the surface of horizontal pole. The first hanging piece and the surface of the cross rod form an included angle of 135 degrees, and the second hanging piece and the surface of the cross rod form an included angle of 135 degrees.
The cross rod is connected with a dovetail clamp, one end of the dovetail clamp is sleeved on the first hanging piece, and the other end of the dovetail clamp is sleeved on the second hanging piece.
Compared with the prior art, the utility model has the advantages of it is following: hang a plurality of forked tail clamps through a plurality of first doctor-bars and second doctor-bar on the horizontal pole, it separates the check curtain to clip by the forked tail clamp again, the trouble of installing a plurality of sliders on the mounting groove has been saved, be provided with the dog equally at the right-hand member of mounting groove, can prevent that the horizontal pole from orbital right-hand member slippage, be provided with the baffle at the left end of mounting groove simultaneously, can be fine prevent that the slide from the left end slippage of mounting groove, and the slide is simple structure, convenient good characteristics, therefore, the clothes hanger is strong in practicability.
More preferably: the cross section of the sliding plate is square.
By adopting the technical scheme, the sliding plate can be completely matched with the rail, and the purpose of free sliding without falling off is achieved.
More preferably: the cross section of the sliding plate is circular.
By adopting the technical scheme, the circular sliding plate can be completely matched with the track, and the purpose of free sliding without falling is achieved.
More preferably: the mounting groove is T-shaped.
By adopting the technical scheme, the sliding plate can be completely matched with the mounting groove.
The method is further optimized as follows: the left end of mounting groove is provided with the baffle, and the baffle is used for blockking the slide landing from the mounting groove.
By adopting the technical scheme, when the sliding plate moves to the leftmost end of the mounting groove, the baffle can block the sliding plate from continuously moving, and the sliding plate is prevented from slipping from the mounting groove.
Drawings
Fig. 1 is a schematic structural diagram of the present embodiment.
Reference numerals: 1-hanging a plate; 2-mounting grooves; 3, a sliding plate; 4-a connecting rod; 5, mounting a rod; 51-a first hanging piece; 52-second hanging piece; 6-dovetail clips; 7-a stop block; 8-baffle plate.
Detailed Description
The present invention will be described in further detail with reference to fig. 1.
The utility model provides an aircraft cabin separates check curtain suspension rail for clip separates the check curtain, as shown in figure 1, including mounting groove 2, mounting groove 2 is seted up on the link plate 1 in the aircraft cabin, is provided with slide 3 and dog 7 on mounting groove 2 respectively, slide 3 and mounting groove 2 sliding connection, slide 3 is at mounting groove 2 internal reciprocating sliding. The stop dog 7 is connected with the mounting groove 2 fixed wheel, and the stop dog 7 is used for stopping the slide 3 from sliding to the tail end of the mounting groove 2.
The bottom surface of slide is connected with connecting rod 4, and the lower extreme of connecting rod 4 is connected with the horizontal pole, and the upper surface of horizontal pole is provided with a plurality of first lacing film 51 and a plurality of second lacing film 52 respectively, and first lacing film 51 and second lacing film 52 symmetry lie in the surface of horizontal pole. The first hanging piece 51 forms an included angle of 135 degrees with the surface of the cross rod, and the second hanging piece 52 forms an included angle of 135 degrees with the surface of the cross rod.
The cross rod is connected with a dovetail clip 6, one end of the dovetail clip 6 is sleeved on the first hanging piece 51, and the other end of the dovetail clip 6 is sleeved on the second hanging piece 52.
Furthermore, the cross section of the sliding plate 3 in this embodiment is square, so that the sliding plate 3 can be completely matched with the rail, and the purpose of free sliding without falling off is achieved.
Furthermore, the cross section of the sliding plate 3 in the embodiment is circular, and the circular sliding plate 3 can be completely matched with the track, so that the purpose of free sliding without falling off is achieved.
Furthermore, the installation slot 2 is T-shaped in this embodiment, so that the slide plate 3 can be completely matched with the installation slot 2.
Furthermore, the left end of the installation groove 2 is provided with a baffle plate 8 in the present embodiment, the baffle plate 8 is used for blocking the sliding plate 3 from sliding off the installation groove 2, and when the sliding plate 3 moves to the leftmost end of the installation groove 2, the baffle plate 8 can block the sliding plate 3 from continuing to move, so as to prevent the sliding plate from sliding off the installation groove 2.
To sum up, the utility model discloses a plurality of forked tail clamps 6 are hung to a plurality of first doctor-bars and second doctor-bar on the horizontal pole, press from both sides 6 by the forked tail and carry the check curtain again, the trouble of installing a plurality of sliders on the mounting groove 2 has been saved, be provided with dog 7 at mounting groove 2 right-hand member equally, can prevent that the horizontal pole from following orbital right-hand member slippage, be provided with baffle 8 at mounting groove 2 leftmost end simultaneously, can be fine prevent slide 3 from mounting groove 2 leftmost end slippage, and has simple structure, convenient good characteristics, therefore, the clothes hanger is strong in practicability.
The present embodiment is only for explaining the present invention, and it is not limited to the present invention, and those skilled in the art can make modifications of the present embodiment without inventive contribution as required after reading the present specification, but all of them are protected by patent laws within the scope of the present invention.

Claims (5)

1. The utility model provides an aircraft cabin check curtain suspension rail which characterized in that: the aircraft cabin mounting structure comprises a mounting groove, wherein the mounting groove is formed in a hanging plate in an aircraft cabin, the mounting groove is respectively provided with a sliding plate and a stop block, the sliding plate is connected with the mounting groove in a sliding manner, and the sliding plate slides in the mounting groove in a reciprocating manner; the stop block is connected with the mounting groove fixing wheel and used for stopping the sliding plate from sliding to the tail end of the mounting groove;
the bottom surface of the sliding plate is connected with a connecting rod, the lower end of the connecting rod is connected with a cross rod, the upper surface of the cross rod is respectively provided with a plurality of first hanging pieces and a plurality of second hanging pieces, and the first hanging pieces and the second hanging pieces are symmetrically positioned on the surface of the cross rod; the first hanging piece and the surface of the cross rod form an included angle of 135 degrees, and the second hanging piece and the surface of the cross rod form an included angle of 135 degrees;
the dovetail clip is connected to the cross rod, one end of the dovetail clip is sleeved on the first hanging piece, and the other end of the dovetail clip is sleeved on the second hanging piece.
2. An aircraft cabin barrier curtain suspension rail according to claim 1, wherein: the cross section of the sliding plate is square.
3. The aircraft cabin barrier curtain suspension rail of claim 1, wherein: the cross section of the sliding plate is circular.
4. The aircraft cabin barrier curtain suspension rail of claim 1, wherein: the mounting groove is T-shaped.
5. An aircraft cabin barrier curtain suspension rail according to claim 4, wherein: the left end of mounting groove is provided with the baffle, the baffle is used for blockking the slide follows landing on the mounting groove.
CN202023329227.0U 2020-12-30 2020-12-30 Suspension rail for cabin barrier curtain of airplane Expired - Fee Related CN217907283U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202023329227.0U CN217907283U (en) 2020-12-30 2020-12-30 Suspension rail for cabin barrier curtain of airplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202023329227.0U CN217907283U (en) 2020-12-30 2020-12-30 Suspension rail for cabin barrier curtain of airplane

Publications (1)

Publication Number Publication Date
CN217907283U true CN217907283U (en) 2022-11-29

Family

ID=84146672

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202023329227.0U Expired - Fee Related CN217907283U (en) 2020-12-30 2020-12-30 Suspension rail for cabin barrier curtain of airplane

Country Status (1)

Country Link
CN (1) CN217907283U (en)

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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20221129