CN218975036U - Stepless adjusting device for simulating pitching and rolling angles of airplane - Google Patents

Stepless adjusting device for simulating pitching and rolling angles of airplane Download PDF

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Publication number
CN218975036U
CN218975036U CN202223481614.5U CN202223481614U CN218975036U CN 218975036 U CN218975036 U CN 218975036U CN 202223481614 U CN202223481614 U CN 202223481614U CN 218975036 U CN218975036 U CN 218975036U
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platform
lifter
pitching
seat
hinged
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CN202223481614.5U
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Chinese (zh)
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任仲峰
韩彬亮
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Xi'an Qing'an Aviation Test Equipment Co ltd
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Xi'an Qing'an Aviation Test Equipment Co ltd
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Abstract

The utility model relates to a stepless regulating device for simulating pitching and rolling angles of an airplane, which mainly solves the problems that the existing simulating device is large in occupied area and inconvenient to use; the change pivot angle frock is complicated, and corresponding pivot angle frock need be changed to different angles, can't realize stepless regulation's technical problem. The device comprises a main body rack, a roll platform, a connecting rod, a first lifter, a guide assembly, a product mounting platform, a pitching platform and a second lifter; the roll platform is arranged above the pitching platform, and the pitching platform is hinged with the roll platform; the product mounting platform is connected to the lower end face of the pitching platform; the main body rack is hinged with the transverse rolling platform; the transverse rolling platform is hinged with one end of a connecting rod, the other end of the connecting rod is hinged with the output end of a first lifter, the first lifter is arranged on a main body rack, the guide assembly is arranged on the main body rack, and the first lifter is connected with the guide assembly; the connecting end of the second lifter is hinged with the transverse rolling platform, and the output end of the second lifter is hinged with the pitching platform.

Description

Stepless adjusting device for simulating pitching and rolling angles of airplane
Technical Field
The utility model relates to a stepless adjusting device, in particular to a stepless adjusting device for simulating pitching and rolling angles of an airplane.
Background
The adjusting device for simulating the pitching and rolling angles of the airplane can adjust the rolling and pitching angles of the airplane by operating the control device on the control panel, so that a person can truly perceive the change conditions of the gesture and the course of the airplane in various flight states, and the adjusting device can be used for beginners and model plane lovers engaged in maintenance work of the airplane to demonstrate the flight process of the airplane, master the flight state of the airplane and simulate the flight faults of the airplane, and has the advantages of simple structure, low cost, convenient operation, certain practicability, ornamental value and operability.
The existing adjusting device generally adopts a mode of matching a main body bench with a fixed swing angle tool, and the device has large occupied area and inconvenient use; changing the swing angle tool is complex, and corresponding swing angle tools need to be changed at different angles, so stepless adjustment cannot be realized.
Disclosure of Invention
The utility model aims to solve the problems that the existing simulation device has large occupied area and is inconvenient to use; the technical problem that the stepless adjustment cannot be realized because the corresponding swing angle tools are required to be replaced at different angles due to the fact that the swing angle tools are complicated to replace is solved, and the stepless adjustment device for simulating the pitching and rolling angles of the airplane is provided.
In order to achieve the above purpose, the technical scheme adopted by the utility model is as follows:
the stepless regulating device for simulating the pitching and rolling angles of the airplane is characterized by comprising the following components: the device comprises a main body rack, a roll platform, a connecting rod, a first lifter, a guide assembly, a product mounting platform, a pitching platform and a second lifter;
the rolling platform is arranged above the pitching platform, a first hinging seat is arranged on the lower end face of the rolling platform, and the pitching platform is hinged with the rolling platform through the first hinging seat; the product mounting platform is connected to the lower end face of the pitching platform and is used for mounting a product to be regulated;
the main body rack is provided with a second hinging seat, and one end of the transverse rolling platform is hinged with the second hinging seat; the other end of the transverse rolling platform is provided with a third hinge seat, the third hinge seat is hinged with one end of a connecting rod, the other end of the connecting rod is hinged with the output end of a first lifter, the first lifter is arranged on a main body rack, the guide component is arranged at a position on the main body rack corresponding to the first lifter, the output end of the first lifter is connected with the moving end of the guide component, and the first lifter is used for driving the transverse rolling platform to transversely roll around the rotating shaft of the second hinge seat;
the roll platform is provided with a fourth hinging seat, a fifth hinging seat is arranged on the pitching platform corresponding to the same side of the fourth hinging seat, the connecting end of the second lifter is hinged with the fourth hinging seat, and the output end of the second lifter is hinged with the fifth hinging seat; the second lifter is used for driving the pitching platform to pitch and rotate around the rotating shaft of the first hinging seat, and the pitching rotating shaft is perpendicular to the rolling rotating shaft.
Further, the guide assembly comprises a guide rail and a sliding block;
the guide rail is connected to the main body rack, the length direction of the guide rail is set along the output direction of the first lifter, one end of the sliding block is connected with the guide rail, and the other end of the sliding block is connected with the output end of the first lifter.
Further, in order to facilitate real-time monitoring of the inclination angle of the product mounting platform, an inclination angle sensor is arranged on the product mounting platform.
Further, the first hinge seat, the second hinge seat, the third hinge seat, the fourth hinge seat and the fifth hinge seat are respectively installed through bolts.
Further, the main body rack comprises a mounting frame, a fixing plate, fixing strips and four supporting legs arranged at four corners of the mounting frame;
the mounting frame is of a rectangular frame body structure, the fixing plate is arranged on one side, far away from the first lifter, of the mounting frame, and the second hinging seat is mounted on the fixing plate;
the fixed strip is arranged on one side of the mounting frame, which is close to the first lifter, two ends of the fixed strip are respectively connected with two supporting legs which are adjacently arranged along the width direction of the mounting frame, the upper end of the guide rail is connected with the mounting frame, and the lower end of the guide rail is connected with the fixed strip.
Further, in order to improve stability of the main body rack, a support seat is provided at a lower end of the support leg.
Further, the supporting seat is in a round table structure, and the diameter of the supporting seat is gradually increased from top to bottom.
Compared with the prior art, the utility model has the beneficial effects that:
1. the first lifter drives the roll platform to rotate around the second hinging seat through the connecting rod, drives the pitching platform and the product mounting platform to synchronously move, and realizes stepless adjustment of the roll angle of the product mounting platform; the second lifter can drive the pitching platform to rotate around the first hinging seat, so as to drive the pitching platform and the product mounting platform to synchronously move, and stepless adjustment of the pitching angle of the product mounting platform is realized; the adjusting mode is simple and reliable, different product mounting platforms can be replaced, pitch angles and roll angles of different products are adjusted, and the applicability is high.
2. According to the utility model, the inclination angle of the product mounting platform can be monitored in real time through the inclination angle sensor, so that a worker can grasp the inclination angle information of the product in real time.
Drawings
FIG. 1 is a schematic view of the configuration of roll platform, pitch platform, first lift, second lift and guide assembly of an embodiment of a stepless adjustment device for simulating pitch and roll angles of an aircraft of the present utility model;
FIG. 2 is a front view of an embodiment of a stepless adjustment device for simulating pitch and roll angles of an aircraft according to the present utility model;
fig. 3 is a left side view of fig. 2.
In the figure: 1-a main body rack, 101-a mounting frame, 102-a fixing plate, 103-a fixing strip, 104-a supporting leg and 105-a supporting seat;
2-a transverse rolling platform, 3-a connecting rod and 4-a first lifter;
5-guiding components, 51-guide rails and 52-sliding blocks;
the device comprises a 6-pitching platform, a 7-second lifter, an 8-product mounting platform, a 9-first hinging seat, a 10-second hinging seat, a 11-third hinging seat, a 12-fourth hinging seat and a 13-fifth hinging seat.
Detailed Description
To make the objects, advantages and features of the present utility model more apparent, a stepless adjustment device for simulating pitch and roll angles of an aircraft according to the present utility model will be described in further detail with reference to the accompanying drawings and the detailed description. The advantages and features of the present utility model will become more apparent from the following detailed description.
As shown in fig. 1 to 3, the stepless adjusting device for simulating the pitch and roll angles of the aircraft comprises a main body rack 1, a roll platform 2, a connecting rod 3, a first lifter 4, a guide assembly 5, a product mounting platform 8, a pitch platform 6 and a second lifter 7.
As shown in fig. 1, the roll platform 2 is arranged above the pitch platform 6, a first hinge seat 9 is arranged in the middle of the lower end surface of the roll platform 2, the first hinge seat 9 is connected to the roll platform 2 and the pitch platform 6 through bolts, and the center of the pitch platform 6 is hinged with the roll platform 2 through the first hinge seat 9; the product mounting platform 8 is connected to the center position of the lower surface of the pitching platform 6 and is used for mounting a product to be regulated, and different product mounting requirements can be met by replacing different product mounting platforms 8.
As shown in fig. 2 and 3, the main body stage 1 includes a mounting frame 101, a fixing plate 102, fixing bars 103, four support legs 104 mounted at four corners of the mounting frame 101; the mounting frame 101 is a rectangular frame body, and the fixing plate 102 is arranged on one side of the mounting frame 101 far away from the first lifter 4; the fixing strip 103 is arranged on one side of the mounting frame 101 close to the first lifter 4, two ends of the fixing strip 103 are respectively connected with two supporting legs 104 arranged adjacently along the width direction of the mounting frame 101, and the lower ends of the supporting legs 104 are provided with supporting seats 105; in other embodiments of the present utility model, the support base 105 may be configured as a prismatic table, a prismatic column, a cylinder, or the like.
As shown in fig. 1 to 3, a second hinge seat 10 is installed on the fixed plate 102 at a position corresponding to one end of the roll platform 2, the second hinge seat 10 is installed on the fixed plate 102 through bolts, and one end of the roll platform 2 is hinged with the second hinge seat 10; the other end of the transverse rolling platform 2 is provided with a third hinging seat 11, the third hinging seat 11 is arranged on the transverse rolling platform 2 through bolts, the third hinging seat 11 is hinged with one end of a connecting rod 3, the other end of the connecting rod 3 is hinged with the output end of a first lifter 4, the first lifter 4 is arranged on a main body rack 1 and is used for driving the transverse rolling platform to transversely roll around the rotating shaft of the second hinging seat, and a guide component 5 is arranged on the main body rack 1 at a position corresponding to the first lifter 4; the guide assembly 5 comprises a guide rail 51 and a slider 52; the guide rail 51 is connected to the main body rack 1, the length direction of the guide rail is along the output direction of the first lifter 4, one end of the sliding block 52 is connected with the guide rail 51, and the other end is connected with the output end of the first lifter 4; the upper end of the guide rail 51 is connected with the mounting frame 101, and the lower end is connected with the fixing bar 103 for improving the stability of the output of the first lifter 4.
As shown in fig. 1 and 2, a fourth hinging seat 12 is installed on the roll platform 2, the fourth hinging seat 12 is installed on the roll platform 2 through a bolt, a fifth hinging seat 13 is installed on the pitching platform 6 at a position corresponding to the same side of the fourth hinging seat 12, the fifth hinging seat 13 is installed on the pitching platform 6 through a bolt, the connecting end of the second lifter 7 is hinged with the fourth hinging seat 12, the output end of the second lifter 7 is hinged with the fifth hinging seat 13, the second lifter is used for driving the pitching platform to pitch and rotate around the rotating shaft of the first hinging seat, and the pitching rotating shaft is perpendicular to the rolling rotating shaft; specifically, the planes of the second hinging seat 10 and the third hinging seat 11 in the rotation direction are located in the planes of the mounting frame 101 in the width direction, the planes of the first hinging seat 9, the fourth hinging seat 12 and the fifth hinging seat 13 in the rotation direction are located in the planes of the mounting frame 101 in the length direction, and when the first lifter 4 drives one end of the rolling platform 2 to rotate around the second hinging seat 10 through the connecting rod 3, the pitching platform 6 can synchronously move with the rolling platform 2, so that the product mounting platform 8 is driven to perform the rolling motion; when the second lifter 7 drives the pitching platform 6 to move around the first hinging seat 9, the rolling platform 2 is kept motionless, and the pitching platform 6 drives the product mounting platform 8 to perform pitching motion, so that the pitch angle and the roll angle of the product mounting platform 8 are adjusted in an infinitely variable manner.
In a preferred embodiment of the present utility model, the bolts may be quick-release bolts to further facilitate installation and removal.
In a preferred embodiment of the present utility model, in order to monitor the inclination of the product mounting platform 8 in real time, an inclination sensor is provided on the product mounting platform 8, and the inclination sensor is connected to an external computer, so that the inclination of the product mounting platform 8 can be displayed in real time.

Claims (7)

1. A stepless regulating device for simulating pitching and rolling angles of an airplane is characterized in that: the device comprises a main body rack (1), a transverse rolling platform (2), a connecting rod (3), a first lifter (4), a guide assembly (5), a product mounting platform (8), a pitching platform (6) and a second lifter (7);
the horizontal rolling platform (2) is arranged above the pitching platform (6), a first hinging seat (9) is arranged on the lower end face of the horizontal rolling platform (2), and the pitching platform (6) is hinged with the horizontal rolling platform (2) through the first hinging seat (9); the product mounting platform (8) is connected to the lower end face of the pitching platform (6) and is used for mounting a product to be regulated;
a second hinging seat (10) is arranged on the main body rack (1), and one end of the transverse rolling platform (2) is hinged with the second hinging seat (10); the novel horizontal rolling platform is characterized in that a third hinging seat (11) is arranged at the other end of the horizontal rolling platform (2), the third hinging seat (11) is hinged with one end of a connecting rod (3), the other end of the connecting rod (3) is hinged with the output end of a first lifter (4), the first lifter (4) is arranged on a main body bench (1), a guide component (5) is arranged at a position on the main body bench (1) corresponding to the first lifter (4), the output end of the first lifter (4) is connected with the moving end of the guide component (5), and the first lifter (4) is used for driving the horizontal rolling platform (2) to horizontally roll around the rotating shaft of the second hinging seat (10);
a fourth hinging seat (12) is arranged on the transverse rolling platform (2), a fifth hinging seat (13) is arranged on the pitching platform (6) corresponding to the same side of the fourth hinging seat (12), the connecting end of the second lifter (7) is hinged with the fourth hinging seat (12), and the output end of the second lifter (7) is hinged with the fifth hinging seat (13); the second lifter (7) is used for driving the pitching platform (6) to pitch and rotate around the rotating shaft of the first hinging seat (9), and the rotating shaft of pitching and rotating is perpendicular to the rotating shaft of rolling and rotating.
2. A stepless adjustment device for simulating aircraft pitch and roll angles according to claim 1, wherein:
the guide assembly (5) comprises a guide rail (51) and a sliding block (52);
the guide rail (51) is connected to the main body rack (1), the length direction of the guide rail is arranged along the output direction of the first lifter (4), one end of the sliding block (52) is connected with the guide rail (51), and the other end of the sliding block is connected with the output end of the first lifter (4).
3. A stepless adjustment device for simulating aircraft pitch and roll angles according to claim 2, wherein:
and an inclination sensor is arranged on the product mounting platform (8).
4. A stepless adjustment device for simulating aircraft pitch and roll angles according to claim 3, wherein:
the first hinge seat (9), the second hinge seat (10), the third hinge seat (11), the fourth hinge seat (12) and the fifth hinge seat (13) are respectively installed through bolts.
5. A stepless adjustment device for simulating aircraft pitch and roll angles according to any one of claims 2-4, wherein:
the main body rack (1) comprises a mounting frame (101), a fixing plate (102), fixing strips (103) and four supporting legs (104) arranged at four corners of the mounting frame (101);
the mounting frame (101) is of a rectangular structure, the fixing plate (102) is arranged on one side, far away from the first lifter (4), of the mounting frame (101), and the second hinging seat (10) is mounted on the fixing plate (102);
the fixing strip (103) is arranged on one side, close to the first lifter (4), of the mounting frame (101), two ends of the fixing strip (103) are respectively connected with two supporting legs (104) which are adjacently arranged along the width direction of the mounting frame (101), the upper end of the guide rail (51) is connected with the mounting frame (101), and the lower end of the guide rail is connected with the fixing strip (103).
6. A stepless adjustment device for simulating aircraft pitch and roll angles according to claim 5, wherein:
the lower ends of the supporting legs (104) are provided with supporting seats (105).
7. A stepless adjustment device for simulating aircraft pitch and roll angles according to claim 6, wherein:
the supporting seat (105) is in a truncated cone structure, and the diameter of the supporting seat is gradually increased along the up-down direction.
CN202223481614.5U 2022-12-26 2022-12-26 Stepless adjusting device for simulating pitching and rolling angles of airplane Active CN218975036U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202223481614.5U CN218975036U (en) 2022-12-26 2022-12-26 Stepless adjusting device for simulating pitching and rolling angles of airplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202223481614.5U CN218975036U (en) 2022-12-26 2022-12-26 Stepless adjusting device for simulating pitching and rolling angles of airplane

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Publication Number Publication Date
CN218975036U true CN218975036U (en) 2023-05-05

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116513378A (en) * 2023-05-22 2023-08-01 上海新纪元机器人有限公司 Parallel anti-rolling anti-corona seat system and transport tool

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116513378A (en) * 2023-05-22 2023-08-01 上海新纪元机器人有限公司 Parallel anti-rolling anti-corona seat system and transport tool
CN116513378B (en) * 2023-05-22 2024-02-23 上海新纪元机器人有限公司 Parallel anti-rolling anti-corona seat system and transport tool

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