Aviation soft full-wrapping foot pad structure

Abstract

The utility model discloses an aviation soft full-wrapping foot pad structure which comprises a foot pad body, the foot pad body is composed of a pair of full-wrapping outer skins and an inner filling layer, the pair of full-wrapping outer skins wraps the two sides of the inner filling layer, and a plurality of positioning sleeve grooves are formed in the foot pad body. The plurality of positioning sleeve grooves penetrate through the pair of full-wrapping outer skins and the inner filling layer; the utility model relates to the technical field of aviation foot pads, in particular to an aviation soft full-wrapping foot pad structure, a positioning sleeve groove is formed in the position corresponding to an angle seat installed on an aviation seat, a positioning body is formed through matching of a positioning pipe sleeve and a pair of limiting pieces, a hole position corresponding positioning rod is formed in the position of the angle seat, and the guiding and positioning effects are achieved. On one hand, the aviation cushion is convenient to install, on the other hand, the positioning pipe sleeve serves as an installation channel of the screw rod piece, the structure is simple, and operation is convenient.

Description

Technical Field

[0001] The utility model relates to the technical field of aviation foot pads, in particular to an aviation soft full-coverage foot pad structure. Background Art

[0002] In modern car interiors, floor mats are an important component. At present, most floor mats are aviation soft full-coverage structures. Due to their easy cleaning, comfort, durability and full coverage, they are widely used in car interiors.

[0003] Modern aviation soft, fully enclosed foot pads are mostly installed and positioned manually. However, during the installation process, the seat installation position needs to be fixed with bolts. During the installation of the soft foot pad, the foot pad also needs to be adjusted in position, which can easily cause the foot pad to tilt. In view of this, in-depth research on the above issues has led to the creation of this case. Utility Model Content

[0004] In view of the deficiencies of the prior art, the utility model provides an aviation soft full-cover foot pad structure, which solves the problems of the prior art.

[0005] To achieve the above objectives, the present invention is implemented through the following technical solutions: an aviation soft full-cover foot pad structure, comprising a foot pad body, the foot pad body consisting of a pair of full-cover outer skins and an inner filling layer, the pair of full-cover outer skins wrapped around both sides of the inner filling layer, the foot pad body being provided with a plurality of positioning sleeves, the plurality of positioning sleeves penetrating the pair of full-cover outer skins and the inner filling layer;

[0006] A positioning sleeve is installed on the positioning sleeve groove, and a pair of limiting plates are provided on both sides of the positioning sleeve, the pair of limiting plates are clamped on both sides of the positioning sleeve groove, and at least one positioning rod is protruding from the back side of the positioning sleeve;

[0007] A limiting protrusion is provided at the end of the positioning rod, the limiting protrusion is a wasp waist-shaped structure, and the limiting protrusion and the positioning rod are an integrated structure;

[0008] A guide ring is protruding from a limiting piece on one side of the positioning sleeve.

[0009] Preferably, the positioning sleeve is a columnar plate and is a separate structure from a pair of limiting plates.

[0010] Preferably, the outer edges of the pair of fully covered outer skins are sealed by an outer ring sleeve, and the outer ring sleeve is sewn to wrap around both sides of the pair of fully covered outer skins.

[0011] Preferably, a plurality of fixing pins are connected between a pair of limiting plates of the positioning sleeve.

[0012] Preferably, the plurality of fixing needles are arranged in a circular array on the limiting plate on one side, and the corresponding limiting plate on the other side is provided with a plurality of connectors corresponding to the plurality of fixing needles, and the plurality of fixing needles pass through a pair of fully wrapped outer skins and an inner filling layer.

[0013] Preferably, the guide ring is a plate with an annular structure, and the outer side of the guide ring is a sloped edge structure.

[0014] Beneficial effects

[0015] The utility model provides a soft, fully enclosed aviation foot pad structure. It has the following beneficial effects: The soft, fully enclosed aviation foot pad structure has a positioning sleeve groove at the corner seat corresponding to the aviation seat installation position. A positioning sleeve and a pair of limit plates form a positioning body. Holes are provided at the corner seat position corresponding to positioning rods, which serve as a guide and positioning function. This facilitates the installation of the aviation seat cushion and, on the other hand, the positioning sleeve serves as an installation channel for the screw rod. The structure is simple and easy to operate. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 This is a three-dimensional structural diagram of an aviation soft full-cover foot pad structure described in the utility model.

[0017] Figure 2 This is a schematic diagram of the first blasting structure of the aviation soft all-enclosed foot pad structure described in the utility model.

[0018] Figure 3 This is a schematic diagram of the second blasting structure of the aviation soft all-enclosed foot pad structure described in the utility model.

[0019] In the figure: 1. Foot pad body; 11. Full outer skin; 12. Inner filling layer; 13. Positioning sleeve groove; 14. Outer ring; 2. Positioning tube sleeve; 21. Limiting piece; 22. Positioning rod; 23. Limiting protrusion; 24. Guide ring; 25. Fixing pin. DETAILED DESCRIPTION

[0020] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0021] See also Figure 1-3The utility model provides an implementation scheme: in the use of modern aviation soft full-cover foot pads, the soft full-cover foot pads need to be placed under the seats, and the seat position usually needs to be fixed with bolts, so holes are usually opened on the soft full-cover foot pads. However, at the current stage, there is no limit on the position of the holes during installation, and the soft full-cover foot pads are relatively large, so the problem of stringing is very easy to occur during installation.

[0022] In response to the above problems, the present application discloses an aviation soft full-cover foot pad structure. Specifically, the foot pad body 1 is used as the main support of the aviation soft full-cover foot pad. The foot pad body 1 is composed of a pair of full-cover outer skins 11 and an inner filling layer 12. The pair of full-cover outer skins 11 are wrapped on both sides of the inner filling layer 12. The pair of full-cover outer skins 11 are made of soft imitation leather material and play a role in protecting and covering the inner filling layer 12. A plurality of positioning sleeves 13 are provided on the foot pad body 1. The plurality of positioning sleeves 13 pass through the pair of full-cover outer skins 11 and the inner filling layer 12. The positioning sleeves 13 correspond to the threaded holes of the seat fixing positions of the foot pad installation positions.

[0023] According to the instruction manual Figure 1-3 It can be seen that a positioning sleeve 2 is installed on the positioning sleeve groove 13, and a pair of limiting pieces 21 are provided on both sides of the positioning sleeve 2. The pair of limiting pieces 21 are clamped on both sides of the positioning sleeve groove 13, and together with the positioning sleeve 2, an I-shaped cross-section component is formed. The pair of limiting pieces 21 relatively wrap the full-cover outer skin 11, on the one hand, play a pulling and limiting role on the full-cover outer skin 11, so that the full-cover outer skin 11 only fits the inner filling layer 12, and then at least one positioning rod 22 is protrudingly provided on the back side of the positioning sleeve 2, which can be connected to the installation position of the seat correspondingly through the positioning rod 22, so as to play a role of limiting and guiding;

[0024] Furthermore, a limiting protrusion 23 is provided at the end of the positioning rod 22. The limiting protrusion 23 is a wasp waist-shaped structure. The limiting protrusion 23 and the positioning rod 22 are an integrated structure. During the installation of the full-coverage foot pad, the positioning rod 22 is inserted into the installation position of the foot pad corresponding to the seat. A positioning hole is provided on the seat installation position corresponding to the positioning rod 22. The positioning rod 22 is inserted into the positioning hole so that the limiting protrusion 23 on the positioning rod 22 is connected with the positioning hole for limiting the position.

[0025] Furthermore, a guide ring 24 is protrudingly provided on the limiting piece 21 on one side of the positioning sleeve. The guide ring 24 corresponds to the inner diameter of the hole on the seat installation position and plays a guiding role.

[0026] As a preferred solution, further, the positioning sleeve 2 is a columnar plate and is a split structure with a pair of limiting plates 21 so that it can be quickly assembled and disassembled during use.

[0027] As a preferred solution, further, the outer edges of the pair of fully covered outer skins 11 are sealed by outer rings 14, and the outer rings 14 are sewn and wrapped around both sides of the pair of fully covered outer skins 11 to prevent the side edges of the inner filling layer 12 from being worn.

[0028] As a preferred solution, further, a plurality of fixing pins 25 are connected between a pair of limiting pieces 21 of the positioning sleeve 2 .

[0029] As a preferred solution, further, a number of fixing needles 25 are arranged in a circular array on the limiting piece 21 on one side, and a number of connectors are provided on the corresponding limiting piece 21 on the other side corresponding to the number of fixing needles 25. The number of fixing needles 25 pass through a pair of fully wrapped outer skins 11 and an inner filling layer 12. The limiting piece 21 on one side of the fixing needles 25 is integrally arranged with the end of the positioning sleeve 2, and a number of connectors corresponding to the number of fixing needles 25 are provided on the limiting plate at the other end of the positioning sleeve 2. During installation, the positioning sleeve 2 is passed through the positioning sleeve groove 13 to make the number of fixing needles 25 pass through a pair of fully wrapped outer skins 11 and the inner filling layer 12, and the pair of limiting pieces 21 are connected accordingly.

[0030] As a preferred solution, further, the guide ring 24 is a plate with an annular structure, and the outer side of the guide ring 24 is a sloped edge structure.

[0031] From the above, it can be seen that the aviation soft full-cover foot pad structure has a positioning sleeve groove 13 at the corner seat position corresponding to the installation of the aviation seat. The positioning main body is formed by the combination of the positioning sleeve and a pair of limit plates 21. The hole position corresponding to the positioning rod 22 is set at the corner seat position to play a guiding and positioning role. On the one hand, it is convenient for the installation of the aviation seat cushion. On the other hand, the positioning sleeve 2 is used as the installation channel of the screw rod, which has a simple structure and is easy to operate.

[0032] Although the embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations may be made to these embodiments without departing from the principles and spirit of the present invention, and the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An aviation soft all-inclusive foot pad structure, comprising a foot pad body (1), the foot pad body (1) consisting of a pair of all-inclusive outer skins (11) and an inner filling layer (12), wherein the pair of all-inclusive outer skins (11) are wrapped around both sides of the inner filling layer (12), and the foot pad body (1) is provided with a plurality of positioning sleeve grooves (13), characterized in that: A plurality of positioning sleeve grooves (13) penetrate a pair of fully enclosed outer skins (11) and an inner filling layer (12); A positioning sleeve (2) is installed on the positioning sleeve groove (13), and a pair of limiting pieces (21) are provided on both sides of the positioning sleeve (2). The pair of limiting pieces (21) are clamped on both sides of the positioning sleeve groove (13), and at least one positioning rod (22) is protrudingly provided on the back side of the positioning sleeve (2); A limiting protrusion (23) is provided at the end of the positioning rod (22), the limiting protrusion (23) is a wasp waist-shaped structure, and the limiting protrusion (23) and the positioning rod (22) are an integrated structure; A guide ring (24) is protrudingly provided on a limiting piece (21) on one side of the positioning sleeve.

2. The aviation soft full-cover foot pad structure according to claim 1, characterized in that: The positioning sleeve (2) is a plate with a columnar structure and is a separate structure with a pair of limiting plates (21).

3. The aviation soft full-cover foot pad structure according to claim 2, characterized in that: The outer edges of the pair of fully covered outer skins (11) are sealed by an outer ring (14), and the outer ring (14) is sewn to wrap around both sides of the pair of fully covered outer skins (11).

4. The aviation soft full-cover foot pad structure according to claim 3, characterized in that: A plurality of fixing pins (25) are connected between a pair of limiting pieces (21) of the positioning sleeve (2).

5. The aviation soft full-cover foot pad structure according to claim 4, characterized in that: The plurality of fixing needles (25) are arranged in a circular array on the limiting plate (21) on one side, and the corresponding plurality of fixing needles (25) are provided with a plurality of connectors on the limiting plate (21) on the other side. The plurality of fixing needles (25) penetrate a pair of fully enclosed outer skins (11) and an inner filling layer (12).

6. The aviation soft full-cover foot pad structure according to claim 5, characterized in that: The guide ring (24) is a plate with an annular structure, and the outer side of the guide ring (24) is a sloped edge structure.

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