Practical training device for airplane structure assembly

Abstract

The utility model discloses a practical training device for airplane structure assembly. The practical training device comprises an operation table, an obliquely arranged supporting base, an outer plate clamping assembly installed on the supporting base, an airplane body clamping assembly and a distance adjusting assembly, wherein the airplane body clamping assembly and the distance adjusting assembly are arranged on the operation table. The aircraft outer plate is fixed to the supporting base through the outer plate clamping assembly, meanwhile, the aircraft body to be assembled is moved into a clamping area of the aircraft body clamping assembly through the distance adjusting assembly, and assembly of the aircraft body and the outer plate is simulated. An aircraft body needing to be assembled with an aircraft outer plate is placed on the surface of a bearing plate, the power output end of a motor drives a screw to rotate, through connection of a connection plate, a bearing sleeve does linear motion, the bearing plate is driven to move to the position between two aircraft body clamping assemblies, a second handle is pulled, a second movable buckle piece is driven to rotate, and a limiting head moves in the direction of a guide pipe; the limiting head abuts against the aircraft body to complete fixation of the aircraft body, at the moment, students can perform simulated assembly on the aircraft outer plate and the aircraft body, and the proficiency degree is improved.

Description

TECHNICAL FIELD

[0001] The utility model relates to an airplane structure assembly practical training device. BACKGROUND

[0002] Airplane maintenance is a kind of work, including airplane body structure and accessory repair, assembly and debugging, airplane test flight and its fault diagnosis and troubleshooting, airplane repair technology management, airplane outfield maintenance and other work contents.

[0003] In the learning airplane structure assembly process, learning personnel cannot contact the real airplane in the first time, need to use airplane's model sheet and same configuration to carry out simulation assembly to improve the maintenance ability of students, and therefore we propose an airplane structure assembly practical training device UTILITY MODEL CONTENT

[0004] The utility model aims at providing an airplane structure assembly practical training device to solve the problems in the above background technology.

[0005] To achieve the above object, the utility model provides the following technical scheme: an airplane structure assembly practical training device, including operation platform, oblique support base, the outer plate clamping assembly of installing on support base, the body clamping assembly of setting on operation platform and distance adjusting assembly;

[0006] Among them, airplane outer plate is fixed on support base through outer plate clamping assembly, and the body to be assembled is moved to the body clamping assembly clamping area in distance adjusting assembly, and the assembly of body and outer plate is simulated.

[0007] Preferably, the outer plate clamping assembly includes a first clamping seat arranged on the support base, a first movable buckle arranged on the first clamping seat, a first handle arranged on the upper surface of the first movable buckle, and a rubber limiting block arranged on the end of the first movable buckle close to the outer plate.

[0008] Preferably, the body clamping assembly includes a second clamping seat arranged on the upper surface of the operation platform, a guide pipe arranged on the upper surface of the second clamping seat close to the body, and a second movable buckle arranged on the end of the second clamping seat away from the guide pipe.

[0009] Preferably, the second movable buckle is provided with a limiting head at the end close to the guide pipe, and a second handle is arranged on the upper surface of the second movable buckle.

[0010] Preferably, the outer plate clamping assembly and the body clamping assembly are arranged in two groups and are symmetrically arranged respectively.

[0011] Preferably, the distance adjusting assembly comprises a groove opened on the upper surface of the operation table, the groove is open at one end, and a screw rod is arranged in the groove, a bearing sleeve is arranged outside the screw rod, and the screw rod is connected with a motor at the end close to the opening.

[0012] Preferably, protrusions are arranged on the upper surface of the operation table and located on both sides of the groove, a slidable bearing plate is arranged on the protrusions, and the lower surface of the bearing plate is connected with the bearing sleeve through a connecting plate.

[0013] The technical effects and advantages of the utility model are as follows: the aircraft structure assembly training device is used for leaning the aircraft outer plate to be assembled on the surface of the supporting base, rotating the first movable buckle by pulling the first handle, making the rubber limiting block abut against the aircraft outer plate, fixing the aircraft outer plate, placing the aircraft body to be assembled with the aircraft outer plate on the surface of the bearing plate, driving the screw rod to rotate through the power output end of the motor, making the bearing sleeve do linear motion through the connection of the connecting plate, moving the bearing plate to the position between the two aircraft body clamping assemblies, rotating the second movable buckle by pulling the second handle, making the limiting head move along the direction of the guide pipe, making the limiting head abut against the aircraft body, fixing the aircraft body, and then the student can simulate the assembly of the aircraft outer plate and the aircraft body, and the proficiency is improved. BRIEF DESCRIPTION OF DRAWINGS

[0014] Figure 1 It is a whole structure schematic view of the utility model;

[0015] Figure 2 It is a structure schematic view of the outer plate clamping assembly of the utility model;

[0016] Figure 3 It is a structure schematic view of the aircraft body clamping assembly of the utility model;

[0017] Figure 4 It is a structure schematic view of the distance adjusting assembly of the utility model.

[0018] In the drawing: 1, operation table; 2, supporting base; 3, first clamping seat; 4, first movable buckle; 5, first handle; 6, rubber limiting block; 7, second clamping seat; 8, guide pipe; 9, second movable buckle; 10, limiting head; 11, second handle; 12, groove; 13, screw rod; 14, bearing sleeve; 15, motor; 16, protrusion; 17, bearing plate; 18, connecting plate. DETAILED DESCRIPTION

[0019] The technical scheme in the utility model embodiment will be clearly and completely described in combination with the drawings in the utility model embodiment.

[0020] In order to facilitate the students to simulate the training of aircraft assembly, reference Figure 1 ,Figure 2 and Figure 3 As shown in the drawings, it comprises an operating table 1, a support base 2 arranged obliquely, an outer plate clamping assembly mounted on the support base 2, a body clamping assembly arranged on the operating table 1 and a distance adjusting assembly; wherein the aircraft outer plate is fixed on the support base 2 through the outer plate clamping assembly, and the body to be assembled is moved into the clamping area of the body clamping assembly through the distance adjusting assembly, the assembly of the body and the outer plate is simulated, the aircraft outer plate to be assembled is obliquely placed on the surface of the support base 2, the rotation of the first movable buckle 4 is driven by pulling the first handle 5, the rubber limiting block 6 is in abutment with the aircraft outer plate, the fixing of the aircraft outer plate is completed, then the body to be assembled with the aircraft outer plate is placed on the surface of the bearing plate 17, the rotation of the screw rod 13 is driven by the power output end of the motor 15, the bearing sleeve 14 makes linear motion through the connection of the link plate 18, the bearing plate 17 is moved between the two body clamping assemblies, the rotation of the second movable buckle 9 is driven by pulling the second handle 11, the limiting head 10 moves along the direction of the guide pipe 8, the limiting head 10 is in abutment with the body, the fixing of the body is completed, at this time, the student can simulate the assembly of the aircraft outer plate and the body.

[0021] In order to improve the stability in the assembly process, refer to Figure 1 , Figure 2 , Figure 3 and Figure 4As shown, the outer plate clamping assembly comprises a first clamping seat 3 arranged on the support base 2, a first movable buckle 4 is arranged on the first clamping seat 3, a first handle 5 is arranged on the upper surface of the first movable buckle 4, a rubber limiting block 6 is arranged on one end of the first movable buckle 4 close to the outer plate, the first handle 5 is buckled to rotate the first movable buckle 4 and drive the movement of the rubber limiting block 6, so that the aircraft outer plate can be fixed. Since the aircraft outer plate is arc-shaped, the inclined support base 2 is more conducive to placing the aircraft outer plate. The body clamping assembly comprises a second clamping seat 7 arranged on the upper surface of the operation table 1, a guide pipe 8 is arranged on the upper surface of the second clamping seat 7 close to one side of the body, and a second movable buckle 9 is arranged on one end of the second clamping seat 7 away from the guide pipe 8. When the body moves to the clamping area of the two body clamping assemblies, the second handle 11 is buckled to drive the rotation of the second movable buckle 9. The second movable buckle 9 is provided with a limiting head 10 at one end close to the guide pipe 8, and the second handle 11 is arranged on the upper surface of the second movable buckle. The limiting head 10 can move along the guide pipe 8 to the body under the guidance of the guide pipe 8 and abut against the body to complete the fixation of the body. The outer plate clamping assembly and the body clamping assembly are both arranged in two groups and symmetrically arranged. The outer plate clamping assembly and the body clamping assembly improve the stability in the assembly process. The distance adjusting assembly comprises a groove 12 opened on the upper surface of the operation table 1, one end of the groove 12 is open, a screw rod 13 is arranged in the groove 12, a bearing sleeve 14 is arranged on the outer side of the screw rod 13, a motor 15 is connected to one end of the screw rod 13 close to the opening, a protrusion 16 is arranged on the upper surface of the operation table 1 and located on both sides of the groove 12, a load-bearing plate 17 is arranged on the protrusion 16 and can slide, and the lower surface of the load-bearing plate 17 is connected to the bearing sleeve 14 through a connecting plate 18. When the body and the aircraft outer plate are fixed, the motor 15 drives the screw rod 13 to rotate, the rotating motion is converted into linear motion through the connection of the connecting plate 18, the bearing sleeve 14 slides on the screw rod 13, thereby driving the movement of the load-bearing plate 17, and the student can assemble the body and the aircraft outer plate.

[0022] In use, first, the aircraft outer plate to be assembled is inclined on the surface of the support base 2, the first handle 5 is buckled to drive the rotation of the first movable buckle 4, the rubber limiting block 6 abuts against the aircraft outer plate, the fixation of the aircraft outer plate is completed, then the body to be assembled with the aircraft outer plate is placed on the surface of the load-bearing plate 17, the motor 15 drives the screw rod 13 to rotate through the power output end, the bearing sleeve 14 moves linearly through the connection of the connecting plate 18, the load-bearing plate 17 moves between the two body clamping assemblies, the second handle 11 is buckled to drive the rotation of the second movable buckle 9, the limiting head 10 moves along the direction of the guide pipe 8, the limiting head 10 abuts against the body, and the fixation of the body is completed.

[0023] It should be noted that the above only the preferred embodiments of the present application, and is not intended to limit the present application.

Claims

1. An aircraft structure assembly training device, characterized in that, It includes an operating table (1), an inclined support base (2), an outer plate clamping assembly installed on the support base (2), a body clamping assembly and a distance adjustment assembly installed on the operating table (1); The aircraft outer panel is fixed to the support base (2) by the outer panel clamping assembly, while the fuselage to be assembled is moved to the clamping area of ​​the fuselage clamping assembly by the distance adjustment assembly to simulate the assembly of the fuselage and the outer panel.

2. The aircraft structure assembly training device according to claim 1, characterized in that: The outer plate clamping assembly includes a first clamping seat (3) disposed on the support base (2), a first movable fastener (4) disposed on the first clamping seat (3), a first handle (5) disposed on the upper surface of the first movable fastener (4), and a rubber limiting block (6) disposed on one end of the first movable fastener (4) near the outer plate.

3. The aircraft structure assembly training device according to claim 1, characterized in that: The machine body clamping assembly includes a second clamping seat (7) disposed on the upper surface of the operating table (1). A guide tube (8) is disposed on the upper surface of the second clamping seat (7) near the machine body. A second movable fastener (9) is disposed at the end of the second clamping seat (7) away from the guide tube (8).

4. The aircraft structure assembly training device according to claim 3, characterized in that: The second movable buckle (9) is provided with a limit head (10) at one end facing the guide tube (8), and a second handle (11) is provided on the upper surface of the second movable buckle.

5. The aircraft structure assembly training device according to claim 1, characterized in that: Both the outer plate clamping assembly and the body clamping assembly are configured in two sets, and are arranged symmetrically.

6. The aircraft structure assembly training device according to claim 1, characterized in that: The distance adjustment component includes a groove (12) formed on the upper surface of the operating table (1). One end of the groove (12) is open, and a screw (13) is provided inside the groove (12). A bearing sleeve (14) is fitted on the outside of the screw (13), and a motor (15) is connected to the end of the screw (13) near the opening.

7. The aircraft structure assembly training device according to claim 6, characterized in that: The upper surface of the operating table (1) and the sides of the groove (12) are provided with protrusions (16), and a slidable support plate (17) is provided on the protrusions (16). The lower surface of the support plate (17) is connected to the bearing sleeve (14) through a connecting plate (18).

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