Airplane interior man-machine work efficiency experiment table with multi-direction point position adjustment

Abstract

The utility model discloses an aircraft interior man-machine work efficiency experiment table with multidirectional point position adjustment, an experiment table frame has a length and an arch-shaped longitudinal section, the experiment table frame is installed on a floor skeleton, and a basic slide rail is installed on the inner side of the experiment table frame in the longitudinal direction of the arch. The base sliding rails are arranged in parallel in the length direction of the experiment table frame, the truss sliding rails are arranged in the length direction of the experiment table frame and installed on the base sliding rails, the truss sliding rails are arranged in parallel in the longitudinal direction of the arch, and the sliding blocks are installed on the truss sliding rails; a foundation sliding rail, a truss sliding rail and a sliding block which are the same as those in the longitudinal direction are arranged and mounted in the oblique direction and the transverse direction of the arch; the connecting piece is installed on the sliding block and faces the interior of the experiment table frame. The multi-direction point position adjustable connecting structure of the experiment table has great flexibility and configurability, different sliding rails are installed in all directions of the experiment table frame and matched with the sliding blocks, and various experiment layout requirements are met.

Description

TECHNICAL FIELD

[0001] The utility model relates to the experimental device of aircraft interior design installation, especially a kind of multi-direction point position adjustment's aircraft interior man-machine work efficiency experiment table. BACKGROUND

[0002] In the development of aircraft interior, if direct in the existing aircraft cabin, it will bring great investment cost and experimental limitation, the existing aircraft cabin is fixed, and interior development can need a variety of different test environment and condition, so flexibility is poor, therefore it is necessary to design an experimental table with high flexibility and adaptability, for simulating aircraft cabin, interface position adjustment can be carried out in its interior according to different interior interfaces, match installation a variety of forms of interior product, reach the experimental purpose of watching actual installation effect, so as to facilitate subsequent experiment on the appearance and function of a variety of different interiors by experimental table, it is beneficial to carry out the preliminary research and development of aircraft interior, promote the efficiency and quality of aircraft interior development. UTILITY MODEL CONTENT

[0003] The utility model aims at providing a kind of multi-direction point position adjustment's aircraft interior man-machine work efficiency experiment table, flexible adaptation different interior interface's demand, match installation a variety of forms of aircraft interior product.

[0004] Technical scheme: a kind of multi-direction point position adjustment's aircraft interior man-machine work efficiency experiment table, including floor skeleton, experiment table frame, basic slide rail, beam slide rail, sliding block, connecting piece;

[0005] The experiment table frame has length and the longitudinal section is arched, the experiment table frame is installed on the floor skeleton, the inside of the experiment table frame is installed the basic slide rail in the longitudinal direction of arch, and the basic slide rail is arranged in multiple along the length direction of the experiment table frame, the beam slide rail is arranged along the length direction of the experiment table frame and is installed on the basic slide rail, and the beam slide rail is arranged in multiple in the longitudinal direction of arch, the sliding block is installed on the beam slide rail;

[0006] In the oblique direction of arch, transverse direction, the same basic slide rail, beam slide rail, sliding block as in longitudinal direction are arranged and installed;

[0007] The connecting piece is installed on the sliding block, and the connecting piece is towards the inside of the experiment table frame.

[0008] Further, the basic slide rail and the arched longitudinal direction of the experiment table frame are fixed by frame support, and the frame support is L-shaped.

[0009] Further, the two adapter supports are L-shaped, one of the adapter supports is installed on the bottom surface of the truss rail with one arm, and the other adapter support is installed on the inner side surface of the base rail facing the inside of the experimental table frame with one arm, and the two adapter supports are stacked and installed with the other arms.

[0010] Preferably, the two adapter supports are provided with a strip-shaped groove on the arms for stacking and installation, and the strip-shaped groove faces the inside of the experimental table frame.

[0011] Preferably, the one adapter support installed on the bottom surface of the truss rail is fixedly connected with the one sliding block on the truss rail, and the sliding block can be used as the installation connection point of the adapter support and the truss rail.

[0012] Preferably, the sliding block is also installed on the base rail, and the one adapter support installed on the base rail is fixedly connected with the one sliding block on the base rail, so that the truss rail can be translated along the base rail through the sliding block in the base rail.

[0013] Further, the experimental table frame comprises a plurality of cross-section frames arranged in parallel along the length direction, the cross-section frames are arched, and the adjacent cross-section frames are fixedly connected with cross beams.

[0014] Further, the bottom of the experimental table frame is fixedly connected with the upper surface of the floor framework through triangular supports.

[0015] Further, the floor framework comprises a plurality of rectangular grid units formed by square tubes, and the adjacent rectangular grid units are fixedly connected with corner pieces.

[0016] Further, the bottom of the floor framework is provided with ground anchors, the ground anchors can elevate the entire floor framework, play a role in adjusting the horizontal height, ensure that the contact between the floor framework and the ground is more uniform, and thus improve the stability of the entire experimental table.

[0017] Beneficial effects: the multi-directional point adjusting and connecting structure of the aircraft interior design ergonomics experimental table has great flexibility and configurability, different types of rails can be installed at various directions and positions of the experimental table frame, and the sliding blocks can be used for accurate point adjustment and matching at any position in the experimental table frame, so that various complex experimental layout requirements can be met, and various forms of interior decoration products can be matched and installed. BRIEF DESCRIPTION OF DRAWINGS

[0018] Figure 1 It is a structural schematic view of the utility model;

[0019] Figure 2 This is a schematic diagram of the floor frame structure;

[0020] Figure 3 for Figure 2 A magnified view of part E in the image;

[0021] Figure 4 This is a schematic diagram of the experimental platform frame structure;

[0022] Figure 5 This is a schematic diagram of the cross-sectional frame structure;

[0023] Figure 6 for Figure 4 A magnified view of part F in the image;

[0024] Figure 7 for Figure 4 G, a magnified view within the text;

[0025] Figure 8 for Figure 1 A magnified view of part I in the image;

[0026] Figure 9 for Figure 1 A magnified view of a portion of the image;

[0027] Figure 10 for Figure 1 A magnified view of part B in the image;

[0028] Figure 11 for Figure 1 A magnified view of part C in the image. Detailed Implementation

[0029] The present invention will be further explained below with reference to the accompanying drawings and specific embodiments.

[0030] A multi-directional, point-adjustable aircraft interior ergonomics test bench, as shown in the attached document. Figure 1 As shown, it includes a floor frame 1 and an experimental table frame 2, with the experimental table frame 2 installed on the floor frame 1.

[0031] As attached Figure 2 As shown, the floor frame 1 is constructed by welding square tubes 11 together to form rectangular grid units. Several rectangular grid units are then connected to form the floor frame, as shown in the attached diagram. Figure 3 As shown, adjacent rectangular grid units are connected and fixed by placing a corner piece 12 on each side of their respective long rectangular side, and then fastening them with bolts. This process breaks down the entire floor frame into smaller parts, allowing for easy disassembly and transportation. The floor frame 1 has feet 13 at the bottom, which can be used to raise the entire floor frame and adjust its level.

[0032] As attachedFigure 4 As shown, the experimental platform frame 2 has a certain length and an arched longitudinal section, with its internal arched surface simulating the interior surface of an aircraft cabin. The experimental platform frame 2 includes multiple cross-sectional frames 21, as shown in the attached diagram. Figure 5 As shown, the cross-sectional frame 21 is arched in shape, with longitudinal frame rods 211, diagonal frame rods 212, and transverse frame rods 213. These five frame rods are fixed together. Multiple cross-sectional frames 21 are arranged in parallel to form the length of the experimental platform frame 2. Adjacent cross-sectional frames 21 are connected and fixed by crossbeams 22, which are arranged transversely. The crossbeams 22 can be as shown in the attached diagram. Figure 6 The welding fixation shown can also be as attached. Figure 7 The bolted connection shown is a detachable fixing mechanism. This detachable fixing can be implemented when there are several cross-sectional frames separated by a certain distance, allowing the entire experimental platform frame to be disassembled and disassembled, facilitating the transportation and handling of the entire experimental platform frame. (See attached image) Figure 8 As shown, the experimental table frame 2 is connected and fixed to the upper surface of the floor frame 1 through the triangular support 23 set at the bottom of the frame rod 211.

[0033] Once the floor frame 1 and the experimental table frame 2 are installed, they form a fixed whole.

[0034] Combined with appendix Figure 1 , 9 As shown, a base slide rail 3 is installed on the inner side of the experimental platform frame 2 in the longitudinal direction of the arch. That is, on the frame rod 211 in the longitudinal direction, the base slide rail 3 is arranged in the same direction as the frame rod 211. The base slide rail 3 is located on the inner side of the frame rod 211 facing the inside of the experimental platform frame 2. The base slide rail 3 and the frame rod 211 are fixed together by an L-shaped frame bracket 31. The base slide rail 3 can be arranged on the frame rod 211 of multiple cross-section frames, and each base slide rail is parallel to the length of the experimental platform frame. The truss slide rail 4 is arranged along the length of the experimental platform frame 2 and installed on the base slide rail 3. The truss slide rail 4 is parallel to the crossbeam 22. The length of the truss slide rail 4 can be the length of the entire experimental platform frame. The length can also be less than the length of the entire experimental platform frame. By designing the experimental platform frame by dividing its length into smaller parts, the truss slide rail 4 can be fixed to two or three basic slide rails 3. Multiple truss slide rails 4 are arranged sequentially along the entire length of the experimental platform frame. Simultaneously, multiple truss slide rails 4 are arranged parallel to each other on the longitudinal frame rods 211. The truss slide rail 4 and the basic slide rail 3 are connected by two L-shaped adapter brackets 32. One adapter bracket has one arm mounted on the bottom surface of the truss slide rail 4, and the other adapter bracket has one arm mounted on the inner side of the basic slide rail 3 facing the interior of the experimental platform frame 2. The two adapter brackets are stacked together with their other arms, as shown in the attached diagram. Figure 10As shown, a strip-shaped slot 321 is formed on the two arms, and the length direction of the strip-shaped slot 321 is towards the inside of the experiment table frame 2; a plurality of sliding blocks 5 are installed on the beam slide rail 4, the sliding blocks 5 can move along the beam slide rail 4, that is, move in the length direction of the experiment table frame, a connecting piece 6 can be installed on the sliding block 5, the connecting piece 6 is towards the inside of the experiment table frame 2, the position adjustment of the connecting piece is realized, so that the adjustment of the interior trim interface is realized, the connecting piece 6 can be replaced according to the structure of the interior trim piece, and a conversion support 32 installed on the bottom surface of the beam slide rail 4 can also be connected and fixed with the sliding block 5 by screwing. The sliding block 5 can also be installed on the base slide rail 3, and the sliding block 5 can move along the base slide rail 3; a conversion support installed on the base slide rail 3 can also be connected and fixed with the sliding block 5 on the base slide rail 3 by screwing, so that the beam slide rail 4 can move in the longitudinal direction.

[0035] The base slide rail 3, the beam slide rail 4, the sliding block 5 and the connecting piece 6 are installed on the frame rod 211 in the longitudinal direction, and the base slide rail 3 is arranged in the same direction as the frame rod 211. Figure 10 The base slide rail 3, the beam slide rail 4, the sliding block 5 and the connecting piece 6 are installed on the frame rod 212 in the oblique direction, and the installation is the same as that on the frame rod 211 in the longitudinal direction, and the base slide rail 3 is arranged in the same direction as the frame rod 212.

[0036] Figure 11 The base slide rail 3, the beam slide rail 4, the sliding block 5 and the connecting piece 6 are installed on the frame rod 213 in the transverse direction, and the installation is the same as that on the frame rod 211 in the longitudinal direction, and the base slide rail 3 is arranged in the same direction as the frame rod 213.

[0037] The multi-directional point adjustment connecting structure of the aircraft interior man-machine efficiency experiment table can be spliced, assembled and adjusted according to the site, function and carrying demand, has great flexibility and configurability, different types of slide rails are installed on each direction and part of the experiment table frame, and the sliding block can be matched to accurately adjust and match the point at any position in the experiment table frame, so as to meet the complex experimental layout demand and match and install various forms of interior trim products.​

Claims

1. A multi-directional point adjustment experimental table for the man-machine ergonomics of aircraft interiors, characterized in that: It comprises a floor skeleton (1), a lab bench frame (2), a base slide rail (3), a beam slide rail (4), a slide block (5), a connecting piece (6); The lab bench frame (2) has a length and an arch-shaped longitudinal section, is installed on the floor skeleton (1), and has the base slide rail (3) installed on the inner side in the longitudinal direction of the arch shape, and multiple base slide rails (3) are arranged in parallel along the length direction of the lab bench frame (2), the beam slide rail (4) is arranged along the length direction of the lab bench frame (2) and is installed on the base slide rail (3), and multiple beam slide rails (4) are arranged in parallel in the longitudinal direction of the arch shape, and the slide block (5) is installed on the beam slide rail (4). In the oblique direction and the transverse direction of the arch shape, the base slide rail (3), the beam slide rail (4), and the slide block (5) are arranged and installed in the same way as in the longitudinal direction. The connecting piece (6) is installed on the slide block (5) and faces the inside of the lab bench frame (2).

2. The multi-directional point adjustment aircraft interior ergonomic test bench according to claim 1, characterized in that: The base slide rail (3) and the longitudinal direction of the arch shape of the lab bench frame (2) are fixedly installed by a frame support (31), and the frame support (31) is L-shaped.

3. The multi-directional point adjustment aircraft interior ergonomic test bench of claim 1, wherein: The beam slide rail (4) and the base slide rail (3) are connected and installed by two adapter supports (32), the adapter supports (32) are L-shaped, one adapter support (32) is installed on the bottom surface of the beam slide rail (4) by one arm, the other adapter support (32) is installed on the inner side surface of the base slide rail (3) facing the inside of the lab bench frame (2) by one arm, and the two adapter supports (32) are installed in a stacked manner by the other arms.

4. The multi-directional point adjustment aircraft interior ergonomic test bench according to claim 3, characterized in that: Strip-shaped grooves (321) are formed on the arms for stacked installation of the two adapter supports (32), and the strip-shaped grooves (321) face the inside of the lab bench frame (2).

5. The multi-directional point adjustment aircraft interior ergonomic test bench according to claim 3, characterized in that: One adapter support (32) installed on the bottom surface of the beam slide rail (4) is connected and fixed with one slide block (5) on the beam slide rail (4).

6. The multi-directional point adjustment aircraft interior ergonomic test bench according to claim 3, characterized in that: The slide block (5) is also installed on the base slide rail (3), and one adapter support (32) installed on the base slide rail (3) is connected and fixed with one slide block (5) on the base slide rail (3).

7. The multi-directional point adjustment aircraft interior ergonomic test bench according to claim 1, characterized in that: The lab bench frame (2) comprises multiple cross-section frames (21) arranged in parallel along the length direction, the cross-section frames (21) are arch-shaped, and the adjacent cross-section frames (21) are connected and fixed by cross beams (22).

8. The multi-directional point adjustment aircraft interior ergonomic test bench of claim 1, wherein: The bottom of the lab bench frame (2) and the upper surface of the floor skeleton (1) are connected and fixed by a triangular support (23).

9. The multi-directional point adjustment aircraft interior ergonomic test bench according to claim 1, characterized in that: The floor skeleton (1) comprises several rectangular grid units spliced by square tubes (11), and the adjacent rectangular grid units are connected and fixed by corner pieces (12).

10. The multi-directional point adjustment aircraft interior ergonomic test bench of claim 1, wherein: The bottom of the floor skeleton (1) is provided with a footing (13).

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