CN214729704U

CN214729704U - Aviation seat with built-in groove

Info

Publication number: CN214729704U
Application number: CN202120461460.XU
Authority: CN
Inventors: 高国华; 杨保国; 张光新; 王卫永; 熊文科
Original assignee: Xinxiang Zhuoying Machinery Co ltd
Current assignee: Xinxiang Zhuoying Machinery Co ltd
Priority date: 2021-03-03
Filing date: 2021-03-03
Publication date: 2021-11-16
Anticipated expiration: 2031-03-03

Abstract

The utility model discloses an aviation seat of built-in recess, including seat body and base, the recess that is the oblique form is seted up to lower part in the back of seat body, and the back of seat body in upper portion articulate has the apron, one side outer wall that the apron is close to the seat body is fixed with first foam-rubber cushion, and one side outer wall that the seat body was kept away from to the seat body is fixed with the second foam-rubber cushion, the bottom outer wall of apron is fixed with the fixed plate. The utility model discloses the seat body is provided with the recess that is the distribution of oblique form, can be used for placing debris or books, and the recess that is the oblique form can not lead to debris or books to fall out, contacts through the metal block on magnetic stripe and the fixed plate, can let the apron cover the recess, debris or books storage stability in the further guarantee recess, apron both sides outer wall is provided with first foam-rubber cushion and second foam-rubber cushion respectively, can avoid causing the influence to the passenger, has improved passenger's the experience of taking.

Description

Aviation seat with built-in groove

Technical Field

The utility model relates to a seat technical field especially relates to an aviation seat of built-in recess.

Background

The chair is a seat with a backrest and armrests. Ancient people sit on the ground without chairs, and the 'chair' originally is a wooden name.

The back of present aviation seat all can be provided with the string bag, and some books or debris can all be placed usually to the string bag, can lead to the practical use space between two seats to reduce around, influence passenger's the experience of taking, and the aviation seat that generally drives built-in recess all can set up the apron and cover it, but the apron does not set up corresponding safeguard measure, collides with the passenger very easily.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the defects existing in the prior art and providing an aviation seat with a built-in groove.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

an aviation seat with a built-in groove comprises a seat body and a base, wherein the middle lower part of the back surface of the seat body is provided with an oblique groove, the middle upper part of the back surface of the seat body is hinged with a cover plate, the outer wall of one side, close to the seat body, of the cover plate is fixed with a first sponge cushion, the outer wall of one side, far away from the seat body, of the seat body is fixed with a second sponge cushion, the outer wall of the bottom of the cover plate is fixed with a fixing plate, the outer wall of the back surface, below the opening of the groove, of the seat body is provided with a mounting groove, the inner wall of the mounting groove is fixed with a magnetic stripe, the outer wall of one side, close to the magnetic stripe, of the fixing plate is fixed with a metal block, the metal block is contacted with the magnetic stripe, the base is positioned below the seat body, the outer wall of the top of the base is fixed with four supporting and limiting parts which are distributed in a rectangular shape, and the middle part of the outer wall of the top of the base is fixed with a shock absorption box, and the inner wall sliding connection of surge tank has the slide, settle the mouth at the top outer wall middle part of surge tank has been seted up, and the inner wall sliding connection who settles the mouth has the connecting block, the spout that the equidistance distributes is seted up to the bottom outer wall of connecting block, and the bottom outer wall and the slide fixed connection of connecting block, the bottom inner wall of surge tank is fixed with the gag lever post that the equidistance distributes, and the outer wall of gag lever post has cup jointed damping spring, the spout that the equidistance distributes is seted up to the top outer wall of slide, and the spout is linked together, the gag lever post forms sliding fit with the inner wall of spout and the inner wall of spout, and the top outer wall of connecting block and the bottom outer wall fixed connection of seat body, the lower part all articulates there is the handrail in the both sides outer wall of seat body.

Preferably, the supporting limiting part comprises a limiting box, the limiting box is fixed on the top outer wall of the base, a return spring is fixed on the bottom inner wall of the limiting box, a sliding block is fixed on the top end of the return spring, a round opening is formed in the top outer wall of the limiting box, a supporting rod is connected to the inner wall of the round opening in a sliding mode, the bottom outer wall of the supporting rod is fixedly connected with the top outer wall of the sliding block, and the top outer wall of the supporting rod is fixedly connected with the bottom outer wall of the seat body.

Preferably, the specification of slider and the specification looks adaptation of spacing case, and the slider forms sliding fit with the inner wall of spacing case.

Preferably, a frame-shaped shock pad is fixed on the outer wall of the top of the shock absorption box, and the frame-shaped shock pad is in contact with the seat body.

Preferably, the outer walls of the two sides of the seat body are fixed with side wing supporting plates, and the outer wall of the waist of the seat body is fixed with a sponge waist rest.

Preferably, the specification of slide and the specification looks adaptation of surge tank, and the surge tank is located between four spacing casees.

The utility model has the advantages that:

1. according to the aviation seat with the built-in grooves, the grooves distributed in an inclined manner are formed in the seat body, sundries or books can be placed in the grooves, the sundries or the books cannot fall out of the grooves, the cover plate can cover the grooves through the contact of the magnetic strips and the metal blocks on the fixing plate, the storage stability of the sundries or the books in the grooves is further guaranteed, the first spongy cushion and the second spongy cushion are arranged on the outer walls of the two sides of the cover plate respectively, the influence on passengers can be avoided, and the riding experience of the passengers is improved;

2. this aviation seat of built-in recess, a plurality of damping spring, a plurality of reset spring and frame form shock pad can realize absorbing effect, and four spacing support component can ensure that the seat body can not take place the dislocation when the shock attenuation, further improve passenger's the experience of taking.

Drawings

Fig. 1 is a schematic side view of a vertical cross-sectional structure of an aviation seat with a built-in groove according to the present invention;

fig. 2 is a schematic back structural view of an aviation seat with a built-in groove provided by the present invention;

fig. 3 is the utility model provides an aviation seat's of built-in recess main view structure schematic diagram.

In the figure: the seat comprises a seat body 1, a groove 2, a cover plate 3, a first spongy cushion 4, a second spongy cushion 5, a fixing plate 6, a metal block 7, a magnetic stripe 8, a base 9, a limiting box 10, a return spring 11, a sliding block 12, a supporting rod 13, a damping box 14, a sliding plate 15, a damping spring 16, a limiting rod 17, a connecting block 18, a sliding groove 19, a frame-shaped damping cushion 20, a handrail 21 and a lateral wing supporting plate 22.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.

Referring to fig. 1-3, an aviation seat with a built-in groove comprises a seat body 1 and a base 9, wherein the middle lower part of the back surface of the seat body 1 is provided with an oblique groove 2, the middle upper part of the back surface of the seat body 1 is hinged with a cover plate 3, the outer wall of one side of the cover plate 3 close to the seat body 1 is fixed with a first sponge cushion 4, the outer wall of one side of the seat body 1 far away from the seat body 1 is fixed with a second sponge cushion 5, the outer wall of the bottom of the cover plate 3 is fixed with a fixing plate 6, the outer wall of the back surface of the seat body 1 below the opening of the groove 2 is provided with a mounting groove, the inner wall of the mounting groove is fixed with a magnetic strip 8, the outer wall of one side of the fixing plate 6 close to the magnetic strip 8 is fixed with a metal block 7, the metal block 7 is in contact with the magnetic strip 8, the base 9 is positioned below the seat body 1, and the outer wall of the top of the base 9 is fixed with four supporting and limiting parts which are distributed in a rectangular shape, a damping box 14 is fixed in the middle of the outer wall of the top of the base 9, a sliding plate 15 is connected to the inner wall of the damping box 14 in a sliding manner, a mounting opening is formed in the middle of the outer wall of the top of the damping box 14, a connecting block 18 is connected to the inner wall of the mounting opening in a sliding manner, sliding grooves 19 are formed in the outer wall of the bottom of the connecting block 18 at equal intervals, the outer wall of the bottom of the connecting block 18 is fixedly connected to the sliding plate 15, limit rods 17 are fixed on the inner wall of the bottom of the damping box 14 at equal intervals, damping springs 16 are sleeved on the outer wall of the limit rods 17, sliding openings are formed in the outer wall of the top of the sliding plate 15 at equal intervals and communicated with the sliding grooves 19, the limit rods 17 are in sliding fit with the inner wall of the sliding openings and the inner wall of the sliding grooves 19, the outer wall of the top of the connecting block 18 is fixedly connected to the outer wall of the bottom of the seat body 1, armrests 21 are hinged to the middle and lower portions of the outer walls of two sides of the seat body 1, grooves 2 are obliquely distributed, the inclined groove 2 can be used for containing sundries or books, the sundries or the books cannot fall out, the cover plate 3 can cover the groove 2 by contacting the magnetic stripe 8 with the metal block 7 on the fixing plate 6, the storage stability of the sundries or the books in the groove 2 is further guaranteed, the first spongy cushion 4 and the second spongy cushion 5 are arranged on the outer walls of the two sides of the cover plate 3 respectively, the influence on passengers can be avoided, and the riding experience of the passengers is improved;

the supporting and limiting component comprises a limiting box 10, the limiting box 10 is fixed on the outer wall of the top of the base 9, a reset spring 11 is fixed on the inner wall of the bottom of the limiting box 10, a sliding block 12 is fixed on the top end of the reset spring 11, a round opening is formed in the outer wall of the top of the limiting box 10, a supporting rod 13 is connected to the inner wall of the round opening in a sliding mode, the outer wall of the bottom end of the supporting rod 13 is fixedly connected with the outer wall of the top of the sliding block 12, the outer wall of the top end of the supporting rod 13 is fixedly connected with the outer wall of the bottom of the seat body 1, the damping springs 16, the reset springs 11 and the frame-shaped damping pad 20 can achieve a damping effect, the four limiting and supporting components can guarantee that the seat body 1 cannot be misplaced during damping, and the riding experience of passengers is further improved;

the specification of slider 12 and the specification looks adaptation of spacing case 10, and slider 12 and the inner wall of spacing case 10 form sliding fit, the top outer wall of surge tank 14 is fixed with frame form shock pad 20, and frame form shock pad 20 contacts with seat body 1, the both sides outer wall of seat body 1 is fixed with flank support plate 22, and the waist outer wall of seat body 1 is fixed with the sponge and leans on the waist, the specification of slide 15 and the specification looks adaptation of surge tank 14, and surge tank 14 is located between four spacing cases 10.

The working principle is as follows: during the use, can open apron 3 and place debris or books in the recess 2 that is the slope form and distributes, recess 2 is the slope form and can not lead to debris or books to fall out, then put down apron 3, can let metal block 7 on the fixed plate 6 contact with magnetic stripe 8, can let apron 3 cover recess 2, debris or books deposit stability in the further guarantee recess 2, first foam-rubber cushion 4 and second foam-rubber cushion 5 on the apron 3, can avoid causing the influence to the passenger, passenger's the experience of taking has been improved, a plurality of damping spring 16 in the surge-box 14, a plurality of reset spring 11 and frame form damping cushion 20 can carry out the shock attenuation to seat body 1, four spacing support component can ensure that seat body 1 can not take place the dislocation when the shock attenuation, further improve passenger's the experience of taking.

In the description of the present invention, it is to 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", 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 to simplify the description, but do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore should not be construed as limiting the present invention.

Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically limited otherwise.

The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims

1. An aviation seat with a built-in groove comprises a seat body (1) and a base (9), and is characterized in that the middle lower part of the back of the seat body (1) is provided with an oblique groove (2), the middle upper part of the back of the seat body (1) is hinged with a cover plate (3), the outer wall of one side, close to the seat body (1), of the cover plate (3) is fixed with a first sponge cushion (4), the outer wall of one side, far away from the seat body (1), of the seat body (1) is fixed with a second sponge cushion (5), the outer wall of the bottom of the cover plate (3) is fixed with a fixing plate (6), the outer wall of the back, below the opening of the groove (2), of the seat body (1) is provided with a mounting groove, the inner wall of the mounting groove is fixed with a magnetic stripe (8), the outer wall of one side, close to the magnetic stripe (8), of the fixing plate (6) is fixed with a metal block (7), and the metal block (7) is in contact with the magnetic stripe (8), the seat is characterized in that the base (9) is positioned below the seat body (1), four supporting and limiting components which are distributed in a rectangular shape are fixed on the outer wall of the top of the base (9), a damping box (14) is fixed in the middle of the outer wall of the top of the base (9), a sliding plate (15) is connected to the inner wall of the damping box (14) in a sliding manner, an accommodating opening is formed in the middle of the outer wall of the top of the damping box (14), a connecting block (18) is connected to the inner wall of the accommodating opening in a sliding manner, sliding grooves (19) which are distributed equidistantly are formed in the outer wall of the bottom of the connecting block (18), the outer wall of the bottom of the connecting block (18) is fixedly connected with the sliding plate (15), limiting rods (17) which are distributed equidistantly are fixed to the inner wall of the bottom of the damping box (14), damping springs (16) are sleeved on the outer wall of the limiting rods (17), sliding openings which are distributed equidistantly are formed in the outer wall of the top of the sliding plate (15), and the sliding opening is communicated with the sliding groove (19), the limiting rod (17) is in sliding fit with the inner wall of the sliding opening and the inner wall of the sliding groove (19), the outer wall of the top of the connecting block (18) is fixedly connected with the outer wall of the bottom of the seat body (1), and the middle lower parts of the outer walls of the two sides of the seat body (1) are hinged with handrails (21).

2. The aircraft seat with the built-in groove as claimed in claim 1, wherein the supporting and limiting component comprises a limiting box (10), the limiting box (10) is fixed on the outer wall of the top of the base (9), a return spring (11) is fixed on the inner wall of the bottom of the limiting box (10), a sliding block (12) is fixed on the top end of the return spring (11), a round opening is formed in the outer wall of the top of the limiting box (10), a supporting rod (13) is connected to the inner wall of the round opening in a sliding manner, the outer wall of the bottom end of the supporting rod (13) is fixedly connected with the outer wall of the top of the sliding block (12), and the outer wall of the top end of the supporting rod (13) is fixedly connected with the outer wall of the bottom of the seat body (1).

3. An aircraft seat with a built-in groove as claimed in claim 2, characterized in that the specification of the slider (12) is matched with that of the limit box (10), and the slider (12) is in sliding fit with the inner wall of the limit box (10).

4. An aircraft seat with a built-in groove according to claim 1, characterized in that a frame-shaped shock absorption pad (20) is fixed on the outer wall of the top of the shock absorption box (14), and the frame-shaped shock absorption pad (20) is in contact with the seat body (1).

5. The aircraft seat with the built-in groove as claimed in claim 1, wherein the outer walls of two sides of the seat body (1) are fixed with side wing supporting plates (22), and the outer wall of the waist part of the seat body (1) is fixed with a sponge waist rest.

6. A recess aircraft seat according to claim 1, characterised in that the dimensions of the slide plate (15) are adapted to the dimensions of the damping box (14), and that the damping box (14) is located between four restraining boxes (10).