CN215932906U

CN215932906U - Flight training is with simulation cockpit

Info

Publication number: CN215932906U
Application number: CN202122556774.0U
Authority: CN
Inventors: 梁琳; 叶亮
Original assignee: Cntech Co ltd
Current assignee: Cntech Co ltd
Priority date: 2021-10-24
Filing date: 2021-10-24
Publication date: 2022-03-01
Anticipated expiration: 2031-10-24

Abstract

The utility model relates to the technical field of flight training equipment and discloses a flight training simulation cockpit which comprises a bottom plate, wherein an operation assembly is arranged at the top of the bottom plate, an action assembly is arranged on the surface of the operation assembly, a driving assembly is arranged at the top of the action assembly, the operation assembly comprises a landing ring movably arranged at the top of the bottom plate, and a gear ring is movably arranged at the top of the bottom plate. According to the simulated cockpit for flight training, the cockpit body rotates around the middle shaft sleeve through the matching of the driving motor, the driving gear, the gear ring, the middle shaft sleeve and the central telescopic rod, so that centrifugal circular simulated motion is provided, in the rotating process of the cockpit body, the two adjusting telescopic rods are used for providing head raising, take-off and landing lamp actions for the cockpit body, and meanwhile, in the landing process, the landing wheels enter the annular groove, so that the cockpit body really experiences a landing feeling, the real feeling of simulated action is comprehensively improved, and the training effect is effectively improved.

Description

Flight training is with simulation cockpit

Technical Field

The utility model relates to the technical field of flight training equipment, in particular to a simulated cockpit for flight training.

Background

Along with the development of economy, roads are more and more congested, traffic transportation is rapidly expanded to a three-dimensional space, the number of aircraft demands is more and more, so that the gap of the number of pilots is caused, the training bases of the pilots are synchronously built, and most of the existing training equipment built or built is relatively lagged behind.

Particularly, in a display part, the situation is not vivid through low projection brightness, the external environment of the display screen arranged on the window has no visual stereoscopic impression, the visual simulation stereoscopic effect is poor, motion simulation is only provided for shaking, the shaking stroke is short, the body feeling is difficult to simulate steering and centrifuging, and the simulation cockpit for flight training is still to be improved.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

Aiming at the defects of the prior art, the utility model provides the flight training simulation cockpit which has the advantages of strong visual impulse, strong motion simulation and the like, and solves the problems of poor display effect and poor motion simulation of the conventional flight training simulation device.

(II) technical scheme

In order to achieve the purposes of strong visual impulse and strong motion simulation, the utility model provides the following technical scheme: a flight training is with simulation cockpit, includes the bottom plate, the top of bottom plate is provided with the operation subassembly, the surface of operation subassembly is provided with the action subassembly, the top of action subassembly is provided with drives the subassembly, the operation subassembly includes movable mounting at the landing ring at bottom plate top, the top movable mounting of bottom plate has the ring gear, the fixed surface of ring gear installs the well axle sleeve with bottom plate swing joint, the inside fixed mounting of well axle sleeve has central telescopic link, the top fixed mounting of bottom plate has driving motor, the bottom fixed mounting of driving motor output shaft has drive gear, the top movable mounting of central telescopic link has the adapter, the avris fixed mounting of adapter has the xarm, the action subassembly includes the rotation sleeve of fixed mounting movable mounting at the xarm other end, the one end fixed mounting that the rotation sleeve kept away from the xarm has the mounting panel, the bottom movable mounting of mounting panel has the regulation telescopic link, the bottom movable mounting who adjusts the telescopic link has the end ring with bottom plate swing joint, drive the subassembly and include the cockpit body of fixed mounting at the mounting panel top, the outside movable mounting of the cockpit body has the dodge gate, the interior diapire fixed mounting of the cockpit body has the encirclement screen, the interior diapire of the cockpit body just is located the inboard movable mounting who encircles the screen has swivel seat, the interior diapire of the cockpit body just is located the inboard fixed mounting who encircles the screen and has the operation panel.

Further, the bottom plate is a circular plate, the landing ring is cylindrical, an annular groove is formed in the top of the landing ring, the gear ring is located in the circle center of the landing ring, and a limiting rotary disc extending to the inside of the bottom plate is fixedly installed at the bottom of the middle shaft sleeve.

Furthermore, the middle shaft sleeve is rotatably connected with the bottom plate through a limiting rotary table, the cross section of the limiting rotary table is in a shape like a Chinese character 'tu', the bottom surface of a gear ring is in contact with the bottom plate, the gear ring is meshed with a driving gear, and a driving motor is fixedly installed at the top of the bottom plate through a placing frame.

Furthermore, the adapter is connected with the central telescopic rod in a rotating mode, the cross arm is connected with the rotating sleeve in a rotating mode, one end, far away from the rotating sleeve, of the mounting plate is located on the inner side of the landing ring, and the mounting plate is close to one end of the rotating sleeve and located on two sides of the rotating sleeve and fixedly provided with reinforcing arms.

Furthermore, the bottom ring is circular, the diameter of the bottom ring is smaller than that of the landing ring, a limiting rotating ring extending to the inside of the bottom plate is fixedly mounted at the bottom of the bottom ring, the width of the limiting rotating ring is larger than that of the bottom ring, the limiting rotating ring is circular, and the bottom ring is rotatably connected with the bottom plate through the limiting rotating ring.

Furthermore, the top of bottom plate is seted up the ring groove that corresponds with bottom ring and spacing change, and the bottom of spacing change rotates installs movable steel ball, adjusts the upper and lower both ends of telescopic link and all rotates and install universal seat, two universal seats respectively with bottom ring and mounting panel fixed connection.

Furthermore, the landing plates are fixedly mounted at the bottom of the cab body and on two sides of the mounting plate, landing frames are movably mounted at the bottoms of the landing plates, and landing wheels are movably mounted at the bottoms of the landing frames.

Further, the bottom fixed mounting of landing slab has the pivot seat, and the pivot seat rotates with landing frame to be connected, and landing frame rotates with the landing wheel to be connected, and the landing wheel is located the ring channel inboard, landing wheel and ring channel sliding connection, and the bottom of landing slab and the avris fixed mounting that is located the pivot seat have with the electron of landing frame joint press from both sides.

Further, the dodge gate rotates with the cockpit body to be connected, and the outside fixed mounting of dodge gate has the handle, and the inboard fixed mounting of dodge gate has the compensation display screen, and the compensation display screen with encircle screen looks adaptation, encircle the screen and be the arc, encircle the central angle of screen and be 300 degrees, and rotatory seat rotates with the cockpit body to be connected, and the inside of the cockpit body just is located the outside fixed mounting who encircles the screen and has the controller.

Advantageous effects

Compared with the prior art, the utility model provides a simulated cockpit depression for flight training, which has the following beneficial effects:

according to the simulated cockpit for flight training, the display effect surrounds flight training personnel for 360 degrees through the surrounding screen and the compensation display screen, and the 3D image is displayed through the surrounding screen and the compensation display screen, so that a pilot is personally on the scene, the visual impulsive force effect is greatly improved.

Drawings

FIG. 1 is a schematic cross-sectional view of a simulation cockpit for flight training according to the present invention;

FIG. 2 is a schematic top view of a flight training simulation cockpit according to the present invention;

FIG. 3 is an enlarged schematic view of a simulated cockpit for flight training shown at A in FIG. 1;

FIG. 4 is an enlarged schematic view of a flight training simulation cockpit at B in FIG. 1 according to the present invention;

FIG. 5 is an enlarged schematic view of a flight training simulation cockpit at C in FIG. 1 according to the present invention;

fig. 6 is a schematic top sectional view of a cockpit body of a flight training simulator according to the present invention.

In the figure: the landing platform comprises a base plate 1, a landing ring 2, an annular groove 3, a gear ring 4, a middle shaft sleeve 5, a central telescopic rod 6, a driving motor 7, a driving gear 8, a switching joint 9, a cross arm 10, a rotating sleeve 11, a mounting plate 12, a reinforcing arm 13, a cockpit 14, a circular groove 15, a bottom ring 16, a limiting rotating ring 17, an adjusting telescopic rod 18, a universal seat 181, a landing plate 19, a landing frame 20, a landing wheel 21, a movable door 22, a surrounding screen 23, a rotating seat 24, an operating platform 25, a compensation display screen 26 and a controller 27.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Referring to fig. 1-6, a flight training simulation cockpit comprises a bottom plate 1, wherein the bottom plate 1 is a circular plate, a running assembly is arranged on the top of the bottom plate 1, an action assembly is arranged on the surface of the running assembly, and a piloting assembly is arranged on the top of the action assembly.

The operation subassembly includes landing ring 2 of movable mounting at bottom plate 1 top, the top movable mounting of bottom plate 1 has ring gear 4, ring gear 4's fixed surface install with 1 swing joint's of bottom plate well axle sleeve 5, the inside fixed mounting of well axle sleeve 5 has central telescopic link 6, the top fixed mounting of bottom plate 1 has driving motor 7, the bottom fixed mounting of driving motor 7 output shaft has drive gear 8, adapter 9 is installed in the top rotation of central telescopic link 6, the avris fixed mounting of adapter 9 has xarm 10.

In this embodiment, landing ring 2 is cylindric, ring channel 3 has been seted up at landing ring 2's top, be used for landing, ring channel 3 is the ring form, gear ring 4 is located landing ring 2's centre of a circle department, the bottom fixed mounting of well axle sleeve 5 has the spacing carousel that extends to bottom plate 1 inside, well axle sleeve 5 rotates with bottom plate 1 through spacing carousel and is connected, spacing carousel cross sectional shape is ' protruding ' font, gear ring 4's bottom surface contacts with bottom plate 1, gear ring 4 meshes with drive gear 8 mutually, driving motor 7 is through the top of placer frame fixed mounting at bottom plate 1, when operating, drive gear 8 rotates through driving motor 7 drive, and then make gear ring 4 rotate, drive whole well axle sleeve 5 by gear ring 4 and rotate.

The action assembly comprises a rotating sleeve 11 which is fixedly installed at the other end of the cross arm 10 in a rotating mode, a mounting plate 12 is fixedly installed at one end, away from the cross arm 10, of the rotating sleeve 11, an adjusting telescopic rod 18 is movably installed at the bottom of the mounting plate 12, a circular bottom ring 16 which is movably connected with the bottom plate 1 is movably installed at the bottom of the adjusting telescopic rod 18, and a limiting rotating ring 17 which extends to the inside of the bottom plate 1 is fixedly installed at the bottom of the bottom ring 16.

In this embodiment, the one end that rotating sleeve 11 was kept away from to mounting panel 12 is located the inboard of landing ring 2, and mounting panel 12 is close to rotating sleeve 11's one end and is located rotating sleeve 11's both sides fixed mounting and strengthens arm 13, and two strengthen arms 13 and mounting panel 12 become isosceles trapezoid shape and rotating sleeve 11 fixed connection, provide stronger stability for mounting panel 12.

In this embodiment, the diameter of the bottom ring 16 is smaller than that of the landing ring 2, the width of the limiting rotary ring 17 is larger than that of the bottom ring 16, the limiting rotary ring 17 is circular, and the bottom ring 16 is rotatably connected with the bottom plate 1 through the limiting rotary ring 17.

In addition, the top of bottom plate 1 is seted up with the ring groove 15 that corresponds with end ring 16 and spacing swivel 17, and the bottom at spacing swivel 17 has rotated and has installed movable steel ball, the quantity of movable steel ball is 40, 40 movable steel balls equally divide into 4 groups, every group all distributes with the ring-type, frictional force when reducing spacing swivel 17 and rotating with this, adjust the upper and lower both ends of telescopic link 18 and all rotate and install universal seat 181, two universal seats 181 respectively with end ring 16 and mounting panel 12 fixed connection, when adjusting telescopic link 18 automatic adjustment, the universal seat 181 of adjusting the both ends of telescopic link 18 can automatic compensation.

The driving assembly comprises a driving cabin body 14 fixedly mounted at the top of a mounting plate 12, landing plates 19 are fixedly mounted at the bottom of the driving cabin body 14 and on two sides of the mounting plate 12, landing frames 20 are rotatably mounted at the bottom of the landing plates 19 through rotating shaft seats, landing wheels 21 are rotatably mounted at the bottom of the landing frames 20, a movable door 22 is rotatably mounted on the outer side of the driving cabin body 14, a surrounding screen 23 is fixedly mounted on the inner bottom wall of the driving cabin body 14, a rotating seat 24 is rotatably mounted on the inner side of the surrounding screen 23 on the inner bottom wall of the driving cabin body 14, an operating platform 25 is fixedly mounted on the inner side of the surrounding screen 23 on the inner bottom wall of the driving cabin body 14, a compensation display screen 26 is fixedly mounted on the inner side of the movable door 22, and a controller 27 is fixedly mounted on the outer side of the surrounding screen 23 inside of the driving cabin body 14.

In this embodiment, in a normal state, the landing wheel 21 is located inside the annular groove 3, and after taking off, the landing frame 20 rotates, so that the landing wheel 21 is separated from the annular groove 3, the landing wheel 21 is connected with the annular groove 3 in a sliding manner, the bottom of the landing plate 19 and the side of the rotating shaft seat are fixedly provided with the electronic clamp clamped with the landing frame 20, after taking off, the landing frame 20 automatically receives the inside of the electronic clamp, before landing, the electronic clamp automatically releases the landing frame 20, and the landing wheel 21 can smoothly enter the annular groove 3.

In this embodiment, the outside fixed mounting of dodge gate 22 has the handle, and compensation display screen 26 and the adaptation of surrounding screen 23 encircle screen 23, and surrounding screen 23 is the arc, and the central angle of surrounding screen 23 is 300 degrees, and swivel seat 24 rotates with cockpit body 14 and is connected, and after the pilot sat into swivel seat 24, swivel seat 24 can rotate voluntarily, makes the orientation of pilot rotate suitable angle, facilitates the use of each part on the operation panel 25.

In summary, the following steps: the display effect is that the flight training personnel is surrounded by 360 degrees through the surrounding screen 23 and the compensation display screen 26, the surrounding screen 23 and the compensation display screen 26 are utilized to display 3D images, a pilot is in the scene, after the trained flight training personnel enters the interior of the cockpit body 14, the rotary seat 24 can automatically rotate, the orientation of the pilot rotates to a proper angle, the parts on the operation table 25 are convenient to use, along with the operation of the pilot, the driving motor 7 drives the driving gear 8 to rotate, further the gear ring 4 rotates, the whole middle shaft sleeve 5 is driven by the gear ring 4 to rotate, further, the cockpit body 14 rotates, after taking off, the landing frame 20 can automatically receive the interior of the electronic clamp, the head raising, taking off and landing lamp actions are provided for the cockpit body 14 through the two adjusting telescopic rods 18, before landing is carried out, the electronic clamp can automatically loosen the landing frame 20 to enable the wheel 21 to smoothly enter the annular groove 3, when landing, the landing wheel 21 enters the annular groove 3, so that the cockpit body 14 really experiences a landing feeling.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims

1. A flight training is with simulation cockpit, includes bottom plate (1), its characterized in that: the top of the bottom plate (1) is provided with an operation assembly, the surface of the operation assembly is provided with an action assembly, and the top of the action assembly is provided with a driving assembly;

the operation assembly comprises a landing ring (2) movably mounted at the top of a bottom plate (1), a gear ring (4) is movably mounted at the top of the bottom plate (1), a middle shaft sleeve (5) movably connected with the bottom plate (1) is fixedly mounted on the surface of the gear ring (4), a central telescopic rod (6) is fixedly mounted inside the middle shaft sleeve (5), a driving motor (7) is fixedly mounted at the top of the bottom plate (1), a driving gear (8) is fixedly mounted at the bottom of an output shaft of the driving motor (7), an adapter (9) is movably mounted at the top of the central telescopic rod (6), and a cross arm (10) is fixedly mounted at the side of the adapter (9);

the action assembly comprises a rotating sleeve (11) which is fixedly installed at the other end of the cross arm (10) in a movable mode, one end, far away from the cross arm (10), of the rotating sleeve (11) is fixedly installed with an installation plate (12), the bottom of the installation plate (12) is movably installed with an adjusting telescopic rod (18), and the bottom of the adjusting telescopic rod (18) is movably installed with a bottom ring (16) movably connected with the bottom plate (1);

the driving assembly comprises a driving cabin body (14) fixedly installed at the top of the installing plate (12), the outer side movable mounting of the driving cabin body (14) is provided with a movable door (22), the inner bottom wall fixed mounting of the driving cabin body (14) surrounds a screen (23), the inner bottom wall of the driving cabin body (14) is provided with a rotating seat (24) and is located at the inner side movable mounting of the surrounding screen (23), and the inner bottom wall of the driving cabin body (14) is provided with an operating board (25) and is located at the inner side fixed mounting of the surrounding screen (23).

2. The simulated cockpit for flight training of claim 1, wherein: the landing gear is characterized in that the bottom plate (1) is a circular plate, the landing ring (2) is cylindrical, the annular groove (3) is formed in the top of the landing ring (2), the gear ring (4) is located at the circle center of the landing ring (2), and the bottom of the middle shaft sleeve (5) is fixedly provided with a limiting rotary table extending to the inside of the bottom plate (1).

3. A flight training simulation cockpit according to claim 2 wherein: well axle sleeve (5) are connected through spacing carousel and bottom plate (1) rotation, and spacing carousel cross sectional shape is 'protruding' font, and the bottom surface of gear ring (4) contacts with bottom plate (1), and gear ring (4) and drive gear (8) mesh mutually, and driving motor (7) are through the top of placer fixed mounting at bottom plate (1).

4. The simulated cockpit for flight training of claim 1, wherein: adapter (9) are rotated with central telescopic link (6) and are connected, and xarm (10) are rotated with rotation sleeve (11) and are connected, and the one end that rotation sleeve (11) was kept away from in mounting panel (12) is located the inboard of landing ring (2), and mounting panel (12) are close to the one end of rotation sleeve (11) and are located the both sides fixed mounting that rotates sleeve (11) and strengthen arm (13).

5. The simulated cockpit for flight training of claim 1, wherein: the bottom ring (16) is circular, the diameter of the bottom ring (16) is smaller than that of the landing ring (2), the bottom of the bottom ring (16) is fixedly provided with a limiting rotating ring (17) extending to the inside of the bottom plate (1), the width of the limiting rotating ring (17) is larger than that of the bottom ring (16), the limiting rotating ring (17) is circular, and the bottom ring (16) is rotatably connected with the bottom plate (1) through the limiting rotating ring (17).

6. The simulated cockpit for flight training of claim 5, wherein: the top of the bottom plate (1) is provided with a circular groove (15) corresponding to the bottom ring (16) and the limiting rotating ring (17), the bottom of the limiting rotating ring (17) is rotatably provided with a movable steel ball, the upper end and the lower end of the adjusting telescopic rod (18) are rotatably provided with universal seats (181), and the two universal seats (181) are respectively and fixedly connected with the bottom ring (16) and the mounting plate (12).

7. The simulated cockpit for flight training of claim 1, wherein: the landing board (19) is fixedly mounted at the bottom of the cab body (14) and on two sides of the mounting plate (12), the landing frame (20) is movably mounted at the bottom of the landing board (19), and the landing wheels (21) are movably mounted at the bottom of the landing frame (20).

8. The simulated cockpit for flight training of claim 7, wherein: the bottom fixed mounting of landing slab (19) has the pivot seat, and the pivot seat rotates with landing frame (20) to be connected, and landing frame (20) rotates with landing wheel (21) to be connected, and landing wheel (21) are located ring channel (3) inboard, and landing wheel (21) and ring channel (3) sliding connection, the bottom of landing slab (19) and the avris fixed mounting that is located the pivot seat have with the electron clamp of landing frame (20) joint.

9. The simulated cockpit for flight training of claim 1, wherein: activity door (22) rotate with the cockpit body (14) and are connected, the outside fixed mounting of activity door (22) has the handle, the inboard fixed mounting of activity door (22) has compensation display screen (26), compensation display screen (26) with encircle screen (23) looks adaptation, it is the arc to encircle screen (23), the central angle that encircles screen (23) is 300 degrees, swivel seat (24) rotate with the cockpit body (14) and are connected, the inside of cockpit body (14) and the outside fixed mounting that is located around screen (23) have controller (27).