CN216145299U

CN216145299U - Three-axis simulation flight simulator actuating mechanism

Info

Publication number: CN216145299U
Application number: CN202122419957.8U
Authority: CN
Inventors: 付强
Original assignee: Harbin Wright Brothers Flight Technology Co ltd
Current assignee: Harbin Wright Brothers Flight Technology Co ltd
Priority date: 2021-10-08
Filing date: 2021-10-08
Publication date: 2022-03-29
Anticipated expiration: 2031-10-08

Abstract

The utility model discloses a three-axis simulation flight simulator actuating mechanism, which relates to the technical field of mechanical structure simulation equipment and comprises a supporting plate, vertical rings, a sliding block, a rotating mechanism arranged on the supporting plate and an omnibearing display mechanism arranged on the vertical rings, wherein the rotating mechanism comprises a motor, a rotating column and a fixed seat, the supporting plate is provided with a rotating hole, the rotating column is movably connected with the rotating hole, the motor is provided with a motor shaft, the rotating column is movably connected with the motor through the motor shaft, the omnibearing display mechanism comprises a first connecting frame, a first mounting plate, a second connecting frame and a second mounting plate, the two first connecting frames are respectively arranged on the outer side walls of the two vertical rings, the other ends of the two first connecting frames are respectively connected with the side walls of the two first mounting plates, the second connecting frame is arranged on the side wall of the sliding block, and the other end of the second connecting frame is connected with the side wall of the second mounting plate, in the utility model, the first display screens are respectively arranged on the outer sides of the two vertical rings, and then displaying the simulation process in real time for one direction of the simulation experiment.

Description

Three-axis simulation flight simulator actuating mechanism

Technical Field

The utility model relates to the technical field of mechanical structure simulation equipment, in particular to an actuating mechanism of a three-axis simulation flight simulator.

Background

The three-axis simulation flight simulator executing mechanism is a main component of the three-axis simulation flight simulator, can simulate a single person to control an aircraft by combining related flight software and a numerical control driving technology, performs three-degree-of-freedom motion of rolling, pitching and yawing, realizes a simulation flight function, and facilitates necessary and important flight simulation experiments on the flight simulator before operation, so that on one hand, all functions of the flight simulator can be ensured to meet the actual use requirements, on the other hand, experimental data of a first hand can be obtained, and the follow-up research and development reference use is facilitated.

The existing three-axis simulation flight simulator executing mechanism is often provided with the problems that an integral rotating mechanism is too complex, a necessary display mechanism is lacked and the like, and therefore the three-axis simulation flight simulator executing mechanism is provided.

SUMMERY OF THE UTILITY MODEL

The utility model mainly aims to provide an actuating mechanism of a three-axis simulation flight simulator, which can effectively solve the problems that the integral rotating mechanism is too complex and lacks a necessary display mechanism in the background technology.

In order to achieve the purpose, the utility model adopts the technical scheme that: a three-axis simulation flight simulator actuating mechanism comprises a supporting plate, a vertical ring, a slide block, a rotating mechanism arranged on the supporting plate and an omnibearing display mechanism arranged on the vertical ring, the rotating mechanism comprises a motor, a rotating column and a fixed seat, the supporting plate is provided with a rotating hole, the rotating column is movably connected with the rotating hole, the motor is provided with a motor shaft, the rotary column is movably connected with the motor through the motor shaft, the fixed seat is arranged between the supporting plate and the motor, the omnibearing display mechanism comprises a first connecting frame, a first mounting plate, a second connecting frame and a second mounting plate, wherein the two first connecting frames are respectively arranged on the outer side walls of the two vertical rings, and is positioned at one side far away from the supporting plate, the other ends of the two first connecting frames are respectively connected with the side walls of the two first mounting plates, the second link is located the slider lateral wall, the second link other end is connected with second mounting panel lateral wall.

Preferably, the support plate further comprises straight rods, the four straight rods are arranged below the support plate and located at four corners of the support plate, and the straight rods support the support plate.

Preferably, the supporting plate further comprises a bracket assembly, the bracket assembly is arranged above the supporting plate, and the bracket assembly forms a necessary three-axis simulation device.

Preferably, the bracket component includes base, stand, solid fixed ring, support frame and filler ring, the backup pad top is located to the base, and is located central point and puts, the base other end and stand swing joint, the stand other end is connected with solid fixed ring lateral wall, gu fixed ring inside central point puts and is equipped with first mounting hole, the support frame lateral wall is connected with first mounting hole, two the support frame both ends are located respectively to the filler ring, and sets up along the support frame symmetry, and the filler ring is fixed with the contact of founding the ring lateral wall to its support of going on, ensures that the simulation experiment process is stable.

Preferably, rotary mechanism still includes driving gear 5 and driven gear, the rotary column lateral wall is located to driving gear 5, the inside central point of driven gear puts and is equipped with the second mounting hole, the vertical column lateral wall is connected with the second mounting hole, driving gear 5 meshes with driven gear mutually, and driving gear 5 meshes with driven gear mutually, realizes rotary transmission.

Preferably, found the ring and still include slide, slide 5, balladeur train and simulation aircraft rack, two the bearing ring is connected with two upright ring lateral walls respectively, and is located the one side near the backup pad, two the slide is located two respectively and is found the ring inside wall, two the slide other end respectively with two slide 5 swing joint, the balladeur train is located between two slides 5, the slider is connected with the balladeur train movable rod, simulation aircraft places to erect in the slider lateral wall, and is located the one side near the backup pad, and the free rotation slides between slide 5 and the slide realizes the unilateral simulation experiment, slides between balladeur train and the slider, realizes the ascending simulation experiment of another side.

Preferably, all-round display mechanism still includes first display screen and second display screen, two one side that two first mounting panels are close to the slider is located respectively to first display screen, one side that the second mounting panel is close to the slider is located to the second display screen, and first display screen and second display screen can realize omnidirectional experiment simulation display work.

Compared with the prior art, the utility model has the following beneficial effects:

1. according to the utility model, the motor rotates to drive the rotary column to rotate, so that the driving gear is driven to rotate, the function of driving the upright column to rotate is realized through the meshing action of the driving gear and the driven gear, the whole support assembly and the plane simulation assembly are driven to rotate, the traditional complex mechanical transmission structure is avoided, and the structure is greatly simplified;

2. according to the utility model, the first display screens are respectively arranged at the outer sides of the two vertical rings, so that the simulation process of one direction of the simulation experiment is displayed in real time, the second display screen is fixedly connected with the sliding block through the second connecting frame, namely, the second display screen and the sliding block realize synchronous motion tracks, namely, the second display screen and the flight simulator synchronously move, so that the real-time display of the simulation process of the aircraft experiment in the other two directions is realized, and the first display screen and the second display screen are matched for use, so that the omnibearing display of the simulation process is realized.

Drawings

FIG. 1 is a schematic diagram of the overall structure of an actuator of a three-axis simulated flight simulator according to the present invention;

FIG. 2 is a front view of a three-axis simulated flight simulator actuator of the present invention;

FIG. 3 is a top view of a three-axis simulated flight simulator actuator of the present invention;

FIG. 4 is a side view of a three-axis simulated flight simulator actuator of the present invention;

fig. 5 is a schematic view of the enlarged structure of a portion a in fig. 1 according to the present invention.

In the figure: 1. a support plate; 2. a straight rod; 3. a motor; 4. turning the column; 5. a driving gear; 6. a driven gear; 7. a fixed seat; 8. a base; 9. a column; 10. a fixing ring; 11. a support frame; 12. a ring; 13. standing a ring; 14. a slideway; 15. a slide base; 16. a carriage; 17. a slider; 18. simulating an aircraft placement rack; 19. a first connecting frame; 20. a first mounting plate; 21. a first display screen; 22. a second link frame; 23. a second mounting plate; 24. and a second display screen.

Detailed Description

In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the utility model easy to understand, the utility model is further described with the specific embodiments.

In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, such as "connected," which may be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Referring to fig. 1-5, the present invention is a three-axis simulation flight simulator actuator, comprising a support plate 1, vertical rings 13, a slide block 17, a rotating mechanism disposed on the support plate 1, and an omnidirectional display mechanism disposed on the vertical rings 13, wherein the rotating mechanism includes a motor 3, a rotary column 4, and a fixing base 7, the support plate 1 is provided with a rotary hole, the rotary column 4 is movably connected with the rotary hole, the motor 3 is provided with a motor shaft, the rotary column 4 is movably connected with the motor 3 through the motor shaft, the fixing base 7 is disposed between the support plate 1 and the motor 3, the omnidirectional display mechanism includes a first connecting frame 19, a first mounting plate 20, a second connecting frame 22, and a second mounting plate 23, the two first connecting frames 19 are respectively disposed on the outer side walls of the two vertical rings 13 and are located on the side away from the support plate 1, the other ends of the two first connecting frames 19 are respectively connected with the side walls of the two first mounting plates 20, the second link 22 is arranged on the side wall of the slide block 17, and the other end of the second link 22 is connected with the side wall of the second mounting plate 23.

Further, the supporting plate 1 further comprises straight rods 2, the four straight rods 2 are arranged below the supporting plate 1 and located at four corners of the supporting plate 1, and the straight rods 2 support the supporting plate 1.

Furthermore, the supporting plate 1 further comprises a bracket assembly, the bracket assembly is arranged above the supporting plate 1, and the bracket assembly forms a necessary three-axis simulation device.

Further, the bracket component includes base 8, stand 9, solid fixed ring 10, support frame 11 and filler ring 12, 1 top in backup pad is located to base 8, and be located central point and put, the 8 other end of base and stand 9 swing joint, the 9 other ends of stand and solid fixed ring 10 lateral walls are connected, gu fixed ring 10 inside central point puts and is equipped with first mounting hole, 11 lateral walls of support frame and first mounting hole are connected, 11 both ends of support frame are located respectively to two filler rings 12, and set up along 11 symmetries of support frame, filler ring 12 and the contact of standing 13 lateral walls of ring support it fixedly, ensure that simulation experiment process is stable.

Further, rotary mechanism still includes driving gear 5 and driven

gear

6, and 4 lateral walls of rotary column are located to driving

gear

5, and 6 inside central points of driven gear put and are equipped with the second mounting hole, and 9 lateral walls of stand are connected with the second mounting hole, and driving gear 5 meshes with driven gear 6 mutually, realizes rotary drive.

Further, found ring 13 and still include slide 14, slide 15, balladeur train 16 and simulation aircraft rack 18, two trunnion rings 12 are connected with two upright 13 lateral walls of ring respectively, and be located the one side that is close to backup pad 1, two riser 13 inside walls are located respectively to two slide 14, two slide 14 other ends respectively with two slide 15 swing joint, balladeur train 16 locates between two slide 15, slider 17 is connected with the balladeur train 16 movable rod, simulation aircraft rack 18 locates the slider 17 lateral wall, and be located the one side that is close to backup pad 1, the rotational sliding between slide 15 and the slide 14, realize unilateral simulation experiment, slide between balladeur train 16 and the slider 17, realize the ascending simulation experiment in another side.

Further, all-round display mechanism still includes first display screen 21 and second display screen 24, and two first display screens 21 are located one side that two first mounting panels 20 are close to slider 17 respectively, and second display screen 24 is located one side that second mounting panel 23 is close to slider 17, and first display screen 21 and second display screen 24 can realize omnidirectional experiment simulation display work.

The working principle of the utility model is as follows: the model of the motor 3 is 57GY, the models of the first display screen 21 and the second display screen 24 are JSF12864-17005, the slide seat 15 and the slide way 14 rotate and slide to realize unidirectional simulation experiments, the slide frame 16 and the slide block 17 slide to realize simulation experiments in the other direction, the motor 3 rotates to drive the rotary column 4 to rotate so as to drive the driving gear 5 to rotate, the function of driving the stand column 9 to rotate is realized through the meshing action of the driving gear 5 and the driven gear 6, the whole bracket assembly and the plane simulation assembly are further driven to rotate, simulation experiments in the last direction of three axes are realized, simulation requirements are met, the first display screen 21 is respectively arranged at the outer sides of the two vertical rings 13, the simulation process of one direction of the simulation experiments is further displayed in real time, the second display screen 24 is fixedly connected with the slide block 17 through the second connecting frame 22, namely, the synchronous motion track with the slide block 17 is simultaneously realized, namely, the flight simulator moves synchronously, real-time display of the experimental simulation process of the aircraft in the other two directions is realized, and the first display screen 21 and the second display screen 24 are matched for use, so that the omnibearing display of the simulation process is realized.

The foregoing shows and describes the general principles and broad features of the present invention and advantages thereof. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the utility model as claimed. The scope of the utility model is defined by the appended claims and equivalents thereof.

Claims

1. The utility model provides a triaxial emulation flight simulator actuating mechanism which characterized in that: comprises a supporting plate (1), a vertical ring (13), a sliding block (17), a rotating mechanism arranged on the supporting plate (1) and an omnibearing display mechanism arranged on the vertical ring (13), wherein the rotating mechanism comprises a motor (3), a rotary column (4) and a fixed seat (7), the supporting plate (1) is provided with a rotating hole, the rotary column (4) is movably connected with the rotating hole, the motor (3) is provided with a motor shaft, the rotary column (4) is movably connected with the motor (3) through the motor shaft, the fixed seat (7) is arranged between the supporting plate (1) and the motor (3), the omnibearing display mechanism comprises a first connecting frame (19), a first mounting plate (20), a second connecting frame (22) and a second mounting plate (23), the two first connecting frames (19) are respectively arranged on the outer side walls of the two vertical rings (13) and are positioned on one side far away from the supporting plate (1), two first link (19) other end is connected with two first mounting panel (20) lateral walls respectively, slider (17) lateral wall is located in second link (22), the second link (22) other end is connected with second mounting panel (23) lateral wall.

2. The three-axis simulated flight simulator actuator of claim 1, wherein: the supporting plate (1) further comprises straight rods (2), and the four straight rods (2) are arranged below the supporting plate (1) and located at four corners of the supporting plate (1).

3. The three-axis simulated flight simulator actuator of claim 2, wherein: the support plate (1) further comprises a support assembly, and the support assembly is arranged above the support plate (1).

4. The three-axis simulated flight simulator actuator of claim 3, wherein: the bracket component comprises a base (8), a stand column (9), a fixing ring (10), a support frame (11) and a supporting ring (12), wherein the base (8) is arranged above the support plate (1) and is located at the center position, the other end of the base (8) is movably connected with the stand column (9), the other end of the stand column (9) is connected with the side wall of the fixing ring (10), a first mounting hole is formed in the center position inside the fixing ring (10), the side wall of the support frame (11) is connected with the first mounting hole, and the supporting ring (12) is arranged at two ends of the support frame (11) respectively and is symmetrically arranged along the support frame (11).

5. The three-axis simulated flight simulator actuator of claim 4, wherein: the rotating mechanism further comprises a driving gear (5) and a driven gear (6), the driving gear (5) is arranged on the side wall of the rotating column (4), a second mounting hole is formed in the center of the interior of the driven gear (6), the side wall of the upright column (9) is connected with the second mounting hole, and the driving gear (5) is meshed with the driven gear (6).

6. The three-axis simulated flight simulator actuator of claim 5, wherein: found ring (13) and still include slide (14), slide (15), balladeur train (16) and simulation aircraft rack (18), two the trunnion ring (12) are connected with two upright ring (13) lateral walls respectively, and are located the one side that is close to backup pad (1), two found ring (13) inside wall, two are located respectively in slide (14) the other end respectively with two slide (15) swing joint, between two slide (15) are located in balladeur train (16), slider (17) are connected with balladeur train (16) movable rod, slider (17) lateral wall is located in simulation aircraft rack (18), and is located the one side that is close to backup pad (1).

7. The three-axis simulated flight simulator actuator of claim 6, wherein: all-round display mechanism still includes first display screen (21) and second display screen (24), two one side that two first mounting panel (20) are close to slider (17) is located respectively in first display screen (21), one side that second mounting panel (23) are close to slider (17) is located in second display screen (24).