KR20210143405A - Air vehicle trainer on ground for educating pilot and helicopter - Google Patents

Abstract

One embodiment of the present invention provides a ground flight equipment trainer which comprises: a mobile driving module moving and driving using rotating wheels; a support body module formed on the upper part of the mobile driving module, rotating based on the mobile driving module, and supporting an object to be tested for performance related to inclination at a preset driving angle or posture balance for achieving balance; a mounting module forming a space in which the object can be mounted; and a balance adjustment module coupled to the support body module and the mounting module, and making the object inclined at a preset driving angle or rotate for achieving balance. According to the present invention, several postures can be provided to a flight body.

Description

Ground Flight Equipment Trainer for Helicopter and Pilot Training {AIR VEHICLE TRAINER ON GROUND FOR EDUCATING PILOT AND HELICOPTER}

The present invention relates to a ground flight equipment trainer, and more particularly, to a ground flight equipment trainer for training helicopters and pilots.

Helicopters are aircraft capable of vertical take-off and landing, and can be used for disaster prevention operations, forest fire extinguishing operations, passenger and cargo transport, and military purposes. In developing a helicopter, the helicopter needs to be maintained in various postures on the ground in order to test the performance such as strength test and fatigue test of the helicopter.

A test apparatus capable of providing various postures for unmanned aerial vehicles and small aircraft as well as helicopters is required.

The technical problem to be achieved by the present invention is to provide a ground flight equipment trainer that provides various postures to an aircraft.

The technical problems to be achieved by the present invention are not limited to the technical problems mentioned above, and other technical problems not mentioned can be clearly understood by those of ordinary skill in the art to which the present invention belongs from the description below. There will be.

In order to achieve the above technical problem, an embodiment of the present invention is a mobile driving module for moving and driving using a rotating wheel, which is formed on the upper part of the mobile driving module, rotates based on the mobile driving module, and is preset A support body module for supporting an object to be tilted at a driving angle or to test a performance related to balancing posture balance, a mounting module for forming a space in which the object can be mounted, and the support body module and the mounting module It is coupled to, the object is inclined at a preset driving angle, or a balance adjustment module that rotates to achieve a balance; provides a ground flight equipment trainer comprising a.

In addition, the support body module is located on the upper surface of the moving travel module, is coupled to one end of the rotary table, which is rotationally driven separately from the moving travel module, and extends upward from the rotary table. , A height adjustment member extending or contracting a length to adjust the height of the object mounted on the mounting module and spaced apart from each other, one side is coupled to the height adjustment member, the lower surface is coupled to the rotary table, It may further include a plurality of load-bearing beams for supporting a load generated by additionally providing a coupling force between the height adjustment member and the rotary table, and rotationally driving the object to be tilted or balanced at the preset driving angle. have.

In addition, the balance adjustment module is rotated by being bolted with a predetermined distance from the mounting module, and is tilted at a preset driving angle or rotates to achieve a balance, and transmits the rotational force by rotation to the mounting module. a rotation driving unit coupled to the rotation driving unit, covering the height adjustment member, and a connecting member in which a joint located at one end of the upper end is drivable in the vertical direction and the joint is driven in the vertical direction, but the balance adjustment module is Adjacent to one side of the height adjustment member to achieve a balance, it may further include a piston movement formed to move the piston.

In addition, the balance adjustment module, formed adjacent to the other side of the height adjustment member, the height adjustment member may further include a tension adjustment unit for adjusting the tension generated in the support wire as the length is extended or contracted. .

In addition, the rotation driving unit, one side is bolted to the mounting module, and the other side receives at least a portion of the ball bearing and a gimbal body in which a ball bearing for rotationally driving based on the height adjustment member is formed, the ball It may further include a bearing housing coupled to the bearing and coupled to the connecting member.

In addition, the height adjustment member may include a plurality of height adjustment pillars arranged to be spaced apart from each other, and the mounting module supports the lower side at a position adjacent to the lower side of the object to be mounted, and is preset to each other. A first lower landing gear and a second lower landing gear spaced apart by an interval distance, connecting gears spaced apart from one side of each gimbal body coupled to each of the height adjustment posts and nut-coupled, and connecting the respective connecting gears, the An upper gear surrounding and fixing an upper portion of an object to be mounted, a first intermediate gear connected to each of the connection gears and the first lower landing gear to support both sides of the mounted object, and each connection gear and the second lower landing gear It may further include a second intermediate gear connected to the gear to support both sides of the mounted object.

In addition, the tension adjusting unit may include a plurality of hydraulic cylinders formed on one side of each of the height adjustment pillars, and the hydraulic cylinders may be connected with a hydraulic hose.

In addition, one end is connected to a portion of each of the height control pillars, in a direction perpendicular to the longitudinal direction of the height control pillar, and the other end is formed in a direction horizontal to the length direction of the height control pillar and is in contact with the floor. It is formed so as to further include a plurality of auxiliary members for supporting the balance of the ground flight equipment trainer.

In addition, the piston movement unit may include a plurality of piston movement units formed adjacent to each of the height adjustment pillars, the plurality of piston movement units, the joint adjacent to each of the height adjustment pillars according to the driving of the gimbal body The piston can move by adjusting the hydraulic pressure so that the parts can be driven in different directions.

In addition, in a state in which the mounting module is separated from the balance control module, after the object is mounted on the mounting module, as the mounting module on which the object is mounted is coupled to the balance control module, the object can be test-flyed. can

In addition, the object may be an air vehicle.

According to an embodiment of the present invention, it is possible to provide various postures to the aircraft.

It should be understood that the effects of the present invention are not limited to the above-described effects, and include all effects that can be inferred from the configuration of the invention described in the detailed description or claims of the present invention.

1 is a view showing a state in which an object is mounted on a ground flight equipment trainer according to an embodiment of the present invention.
2 is a perspective view of a ground flight equipment trainer according to an embodiment of the present invention.
3 is a front view of a ground flight equipment trainer according to an embodiment of the present invention.
4 is a side view of a ground flight equipment trainer according to an embodiment of the present invention.
5 is a view showing an upper surface of a mobile driving module according to an embodiment of the present invention.
6 is a view showing a lower surface of a mobile driving module according to an embodiment of the present invention.
7 is a view illustrating a contact relationship between a moving traveling module and a support body module according to an embodiment of the present invention.
8 is a view showing a support body module and a balance adjustment module according to an embodiment of the present invention.
9 is an enlarged view showing a partial configuration of a ground test equipment trainer according to an embodiment of the present invention.
10 is a view showing a state in which the balance control module and the mounting module are inclined as the balance control module operates according to an embodiment of the present invention.

Hereinafter, the present invention will be described with reference to the accompanying drawings. However, the present invention may be embodied in several different forms, and thus is not limited to the embodiments described herein. And in order to clearly explain the present invention in the drawings, parts irrelevant to the description are omitted, and similar reference numerals are attached to similar parts throughout the specification.

Throughout the specification, when a part is said to be “connected (connected, contacted, coupled)” with another part, it is not only “directly connected” but also “indirectly connected” with another member interposed therebetween. "Including cases where In addition, when a part "includes" a certain component, this means that other components may be further provided without excluding other components unless otherwise stated.

The terms used herein are used only to describe specific embodiments, and are not intended to limit the present invention. The singular expression includes the plural expression unless the context clearly dictates otherwise. In this specification, terms such as "comprises" or "have" are intended to designate that the features, numbers, steps, operations, components, parts, or combinations thereof described in the specification exist, but one or more other features It should be understood that this does not preclude the existence or addition of numbers, steps, operations, components, parts, or combinations thereof.

Hereinafter, embodiments of the present invention will be described in detail with reference to the accompanying drawings.

The ground flight equipment trainer of the present invention is a training device that tests the performance of a helicopter and allows the pilot to train by taking the helicopter in various postures.

1 is a view showing a state in which an object is mounted on a ground flight equipment trainer according to an embodiment of the present invention. In the present invention, an object (hereinafter, an air vehicle) may be an air vehicle (eg, a helicopter). Referring to FIG. 1 , the ground flight equipment trainer (hereinafter, the trainer) 10 according to this embodiment is fixed in contact with the front part of the vehicle 20 , so that the vehicle 20 is fixed to the trainer 10 . Aircraft performance can be tested.

Figure 2 is a perspective view of a trainer according to an embodiment of the present invention, Figure 3 is a front view of the trainer according to an embodiment of the present invention, Figure 4 is a side view of the trainer according to an embodiment of the present invention.

2 to 4 , the trainer 10 according to an embodiment of the present invention includes a moving driving module 100 , a support body module 200 , balance adjustment modules 300 and 400 , and a mounting module 500 . , and may be configured to include an auxiliary member (600).

The moving driving module 100 may move and travel on the ground and the floor using a rotating wheel. The moving driving module 100 may form a lower portion of the trainer 10 . In addition, the moving traveling module 100 may be coupled to the support body module 200 to support the support body module 200 . And, the moving driving module 100 may transmit a load to the ground.

The support body module 200 is formed on the upper part of the moving driving module 100, rotating based on the moving driving module 100, tilting at a preset driving angle, or balancing performance related to posture balance. It can support the vehicle 20 to be tested.

The balance adjustment module 300, 400 is coupled to the support body module 200 and the mounting module 500, and tilts the aircraft 20 at a preset driving angle, or rotates to achieve a balance, by rotation Rotational power may be transmitted to the mounting module 500 .

The mounting module 500 may form a space in which the aircraft 20 can be mounted therein.

The plurality of auxiliary members 600 may be connected to the support body module 200 to support the balance of the trainer 10 .

The moving traveling module 100 according to the present embodiment may include an upper plate 110 , a rotating part 120 , a bearing wheel part 130 , a lower plate support structure 140 , and a driving wheel 150 . . In order to describe in more detail the mobile driving module 100 of the present invention, reference is made to FIGS. 5 to 6 .

5 is a view showing an upper surface of the mobile traveling module according to an embodiment of the present invention, and FIG. 6 is a view showing a lower surface of the mobile traveling module according to an embodiment of the present invention.

The upper plate 110 may be positioned under the support body module 200 to form an upper surface of the moving traveling module 100 . The upper plate 110 has a plate shape, and may be formed in a donut shape with a hole in the center. The upper plate 110 according to an embodiment is formed in the shape of a lid so that the side of the rim has a height compared to the upper surface, and the center may be formed in a holed form.

And, the upper plate 110 may have rigidity. For example, the upper plate 110 may withstand the load of the support body module 200 , the balance adjustment modules 300 and 400 , the mounting module 500 , and the aircraft 20 .

In addition, the upper plate 110 may be parallel to the horizontal plane. The upper plate 110 may be located in or parallel to the XY plane in the XYZ coordinate system. The XY plane may mean a horizontal plane. The XYZ coordinate system may mean a Cartesian coordinate system.

The rotating part 120 may be formed in the center of the moving traveling module 100 . The rotating part 120 may correspond to the central part of the rotating table 210 of the support body module 200 in FIG. 2 . The rotating part 120 may accommodate the central part of the rotating table 210 . In the rotating part 120 , the central part may rotate.

Referring to FIG. 5 , the bearing wheel unit 130 may include a first load supporting member 131 , a second load supporting member 132 , and a plurality of bearing wheels 133 .

The bearing wheels 133 according to the present embodiment are arranged to be spaced apart from each other by a predetermined distance, and the bearing wheel 133 is in contact with the support body module 200 from below, and directly transmits the load of the support body module 220 . can receive

When the support body module 200 positioned above the bearing wheel 133 tries to rotate, each bearing wheel rotates itself, so that the support body module 200 rotates separately from the moving driving module 100 . be able to

The first load bearing member 131 and the second load bearing member 132 form holes through which the plurality of bearing wheels 133 may pass, and as the plurality of bearing wheels are inserted through the holes, a plurality of By connecting bearing wheels of

Next, reference is made to FIG. The lower plate support structure 140 is connected to the lower portion of the side of the upper plate, and the first support bar 141 is formed to extend in a direction perpendicular to the direction in which the lower end of the side of the upper plate 110 faces. , said to be formed adjacent to the first support bar 141, the side of the second support bar 142 is formed adjacent to the side of the upper plate 110, and is formed on the lower surface of the upper plate 110 A third support bar 143 may be included.

The driving wheel 150 is disposed as it is coupled to the inner space of the lid-shaped upper plate 110 , and can travel to move the trainer 10 and the aircraft 20 as well as the moving driving module 100 . .

Referring again to FIGS. 2 to 4 , the support body module 200 will be described in detail.

The support body module 200 according to the present embodiment includes a rotary table 210 , a plurality of load support beams 220 , a height adjustment member 230 , a support wire winding part 240 , and an auxiliary member connection part 250 . can do.

The rotary table 210 may be positioned on the upper surface of the moving traveling module 100 and may be rotated separately from the moving traveling module 100 .

7 is a view illustrating a contact relationship between a moving traveling module and a support body module according to an embodiment of the present invention.

The rotary table 210 may include a base 211 , a lower support beam 212 , and a bearing wheel contact plate 213 . Referring to FIG. 7 , the bearing wheel contact plate 213 may be positioned below the edge of the lower support beam 212 and disposed above the bearing wheel 133 . In addition, the base 211 and the lower support beam 212 are stacked on the bearing wheel contact plate 213 , and disposed to be spaced apart from the upper plate 110 at a predetermined distance, the moving driving module 100 . ) can be rotated separately.

Referring back to FIGS. 2 to 4 , each of the load-bearing beams 220 is spaced apart from each other, one side is coupled to the height adjusting member 230 , and the lower surface is coupled to the rotary table 210 , the height adjusting member The coupling force between the 230 and the rotary table 210 is additionally applied, and the vehicle 20 can support a load generated as the vehicle 20 is tilted at a preset driving angle or rotated to achieve a balance.

The height adjustment member 230 is coupled to one end of the turn table 210 and extends upwardly from the turn table 210 to adjust the height of the aircraft 20 mounted on the mounting module 500 . It can be stretched or retracted its entire length.

The height adjustment member 230 according to the present embodiment may include a plurality of height adjustment pillars. More specifically, the height adjustment member 230 may be composed of height adjustment columns spaced apart from each other and a column connection part disposed therebetween, and the load-bearing beams 220 may be implemented to be coupled to the column connection part. can

Each height adjustment column 230 is composed of an outer column that covers the inner column of the balance control module, and raises the inner column to be exposed from the outer column in order to extend or contract the entire length, or lift the raised inner column to the outside Through the operation of reinserting into the column, the entire length can be stretched or contracted. For example, the inner pillar of the balance adjustment module according to an embodiment of the present invention is preferably formed to have a longer length than the outer pillar of the height adjustment pillar.

The support wire winding unit 240 may be formed on both ends of the side portion of each external pillar so as to wind or wind the support wire connected to the tension control unit 340 .

The auxiliary member connection part 250 is for coupling the support body module 200 and the auxiliary member 600 .

And, the balance adjustment module 300, 400 according to an embodiment of the present invention is connected to each height adjustment pole and the mounting module 500, and the aircraft 20 is tilted at a certain driving angle, or rotates to achieve a balance and rotational power by rotation may be transmitted to the mounting module 500 .

In this embodiment, the balance adjustment module coupled to the height adjustment pillar on the right in FIG. 2 is called a first balance adjustment module 300, and the balance adjustment module coupled to the height adjustment pillar on the left side in FIG. 2 is a second It will be described as a balance adjustment module 400 .

The first balance adjustment module 300 may include a first connection member, a first piston movement unit 320 , a first reservoir tank 330 , a first tension adjustment unit 340 , and a first rotation drive unit 350 . have.

In addition, the second balance adjustment module 400 includes a second connection member, a second piston movement unit 420 , a second reservoir tank 430 , a second tension adjustment unit 440 , and a second rotation drive unit 450 . can do.

In this embodiment, the first balance adjustment module 300 and the second balance adjustment module 400 have the same configuration, structure, and operation principle, so here, the first balance adjustment module 300 with reference to Figs. ) to represent

8 is a view showing a support body module and a balance adjustment module according to an embodiment of the present invention, Figure 9 is an enlarged view showing a part of the configuration of the ground test equipment trainer according to an embodiment of the present invention. 8 and 9 according to an embodiment show a state in which the inner column of the balance adjustment module is inserted into the outer column 230 of the support body module 200 .

The first connecting member according to an embodiment of the present invention is formed at the upper end of the inner column (not shown), the inner column inserted into the outer column 230 of the support body module 200, although not shown separately in the drawing. , In a state in which the inner pillar is inserted into the outer pillar, a cover member formed to cover a portion of the outer pillar, is located on the upper portion of the cover member, is connected to the cover member, and includes a joint 310 connected to the piston moving part. can

Although not shown in the drawings, a power source may be located within the inner pillars of each of the balance control modules 300 and 400 . For example, an electric motor or a hydraulic motor may be located inside the inner column. The power source may be referred to as a pitch motor. The pitch motor may be installed in the inner space of the inner pillar to provide power to each of the rotation driving units 350 and 450 and each of the inner pillars.

Referring to FIG. 9 , the front end of the joint 310 according to an embodiment is lowered or raised by the pitch motor.

Accordingly, the first piston movement unit 320 is formed adjacent to one side of the cover member so that the joint 310 is driven in the up/down direction, and the balance adjustment module 300 achieves a balance, so that the piston can move. have. For example, the first piston moving unit 320 and the second piston moving unit 420 of the present invention may be hydraulic cylinders.

The first piston movement unit 320 may include a first hydraulic hose 321 and a first hose valve 322 connected to the lower end, and the second piston movement unit 420 is a second hydraulic hose connected to the lower end ( 421 and a second hose valve 422 may be included. The first and second piston movement units 320 and the second piston movement unit 420 may be connected according to the fastening of the first and second hose valves 322 and 422 to perform a piston movement using hydraulic pressure.

The first tension adjustment unit 340 is formed adjacent to the other side of the height adjustment column 230, and the inner column of the balance adjustment module 300 rises up or down, so that the height adjustment member extends the length. Alternatively, the tension generated in the support wire can be adjusted as it contracts. The first tension adjusting unit 330 according to the present embodiment may adjust the tension of the supporting wire between the supporting wires wound around the supporting wire winding unit 240 located on both ends of the outer pillar. For example, the first tension adjusting unit 330 of the present invention may be implemented as a turnbuckle.

The first rotation driving unit 350 may be rotated by being bolted to the mounting module 500 at a predetermined distance and rotated, tilted at a preset driving angle, or rotated by the balanced mounting module 500 . .

As shown in FIGS. 8 and 9 , the first rotation driving unit 350 according to the present embodiment may include a bearing housing 351 and a gimbal body 352 .

One side of the gimbal body 352 according to the present embodiment may be bolted to the mounting module 500 , and the other side may include a ball bearing that rotates based on the height adjustment member 230 .

The bearing housing 351 may receive at least a portion of the ball bearing of the gimbal body 352 , and may be coupled to the ball bearing and coupled to the first connecting member connected to one end of the joint.

According to an embodiment, the gimbal body 352 of the present invention may rotate 360 degrees based on the horizontal central axis of the bearing housing 351 fixed using a ball bearing. The gimbal body 352 rotates by receiving power from the pitch motor, thereby maintaining the balance of the mounting module 500 and the balance adjustment module 300 .

Reference is again made to FIGS. 2 to 4 .

The mounting module 500 according to an embodiment of the present invention includes the connecting gears 510 and 520 , the upper gear 530 , the first intermediate gears 540 , the second intermediate gears 550 , and the first lower landing gear. 560 , a second lower landing gear 570 , and a third lower landing gear 580 may be included.

The connection gear is composed of a first connection gear 510 and a second connection gear 520 , the first connection gear 510 is spaced apart from the first rotation driving unit 350 and nut-coupled, and the second connection gear 520 . ) may be spaced apart from the second rotation driving unit 450 and nut-coupled.

The first connection gear 510 and the second connection gear 520 are implemented to be coupled with the first and second rotation driving units 350 and 450 at a predetermined interval, so that the first and second rotation driving units rotate 360 degrees. By (350, 450), the vehicle 20 is not driven only left and right, and the vehicle 20 can be driven forward and backward by the predetermined interval.

At this time, for example, one end of the connecting bar connecting the first connecting gear 510 and the second connecting gear 520 and the first and second rotation driving units 350 and 450 using a bolt is of the gimbal body 351 . Rather than being fixedly coupled to the side, it may be implemented to pass through the gimbal body 351 while moving left and right by the predetermined interval.

The upper gear 530 connects the first and second connecting gears 510 and 520 , and surrounds the upper portion of the vehicle 20 mounted on the mounting module 500 to fix the vehicle 20 .

The first intermediate gears 540 are connected to the first and second connecting gears 510 and 520 and the first lower landing gear 560 to support both sides of the aircraft 20 mounted on the mounting module 500 . can do. In addition, the second intermediate gears 550 are connected to the first and second connecting gears 510 and 520 and the second lower landing gear 570, both sides of the aircraft 20 mounted on the mounting module 500 . can support wealth. The first intermediate gears 540 and the second intermediate gears 550 may be implemented as two intermediate gears respectively connected to the first connecting gear 510 and the second connecting gear 520 .

The first lower landing gear 560 and the second lower landing gear 570 may support the lower side of the aircraft 20 at a position adjacent to the lower side of the aircraft 20 mounted on the mounting module 500 . The first lower landing gear 560 may be connected to the first intermediate gears 540 , and the second lower landing gear 570 may be connected to the second intermediate gears 550 .

The third lower landing gear 580 is a landing gear connecting the first lower landing gear 560 and the second howw landing gear 570, and may be located on both sides as shown in FIG. 2 .

For example, the mounting module 500 of the present invention is separated from the balance control modules 300 and 400, after mounting the vehicle 20, the mounting module 500 and the balance control module on which the vehicle 20 is mounted. (300, 400) can be combined through a bolt and a nut.

Auxiliary members 600 have one end connected to a portion of each of the height adjusting posts 230 in a direction perpendicular to the longitudinal direction of the height adjusting post 230 , and the other end in the longitudinal direction of the height adjusting post 230 . As it is formed in a horizontal direction and is formed to contact the floor, it is possible to support the balance of the trainer 10 .

The auxiliary member 600 according to the present embodiment may operate by being connected to the auxiliary member connection part 250 as shown in FIG. 2 . The auxiliary member 600 is a coupling member 610 connected to the auxiliary member connection part 250, the auxiliary member body 620 and the auxiliary member body 620 connected to the coupling member 610 to form a 'L' shape. It may be composed of an auxiliary member wheel 630 connected to the end of the.

Such an auxiliary member 600 may be provided with a plurality of auxiliary members connected to each of the plurality of height adjustment pillars.

10 is a view showing a state in which the balance adjustment module and the mounting module are inclined as the balance adjustment module operates according to an embodiment of the present invention. 10 (a) is a state inclined to the left, (b) is a state inclined to the right.

The above description of the present invention is for illustration, and those of ordinary skill in the art to which the present invention pertains can understand that it can be easily modified into other specific forms without changing the technical spirit or essential features of the present invention. will be. Therefore, it should be understood that the embodiments described above are illustrative in all respects and not restrictive. For example, each component described as a single type may be implemented in a dispersed form, and likewise components described as distributed may be implemented in a combined form.

The scope of the present invention is indicated by the following claims, and all changes or modifications derived from the meaning and scope of the claims and their equivalent concepts should be construed as being included in the scope of the present invention.

100: mobile driving module
200: support body module
300: first balance adjustment module
400: second balance adjustment module
500: mounting module
600: secondary member

Claims (11)

a mobile driving module for moving and driving using a rotating wheel;
a support body module formed on the upper part of the moving driving module, rotating based on the moving driving module, inclined at a preset driving angle, or supporting an object to be tested for performance related to balancing posture balance;
a mounting module forming a space in which the object can be mounted; and
A ground flight equipment trainer comprising a; coupled to the support body module and the mounting module, the object is inclined at a preset driving angle, or a balance adjustment module that rotates to achieve a balance.
According to claim 1,
The support body module,
a rotary table positioned on the upper surface of the moving travel module and rotationally driven separately from the moving travel module;
a height adjusting member coupled to one end of the rotary table and extending upward from the rotary table to extend or contract the length to adjust the height of the object mounted on the mounting module; and
Spaced apart from each other, one side is coupled to the height adjusting member, and the lower surface is coupled to the rotary table, thereby additionally providing a coupling force between the height adjusting member and the rotary table, and the object is set at the preset driving angle. Ground flight equipment trainer, characterized in that it further comprises; a plurality of load-bearing beams for supporting a load generated by rotationally driven to be tilted or balanced.
3. The method of claim 2,
The balance control module,
a rotation driving unit which rotates at a predetermined driving angle, or rotates to achieve a balance, as it is bolted and rotates at a predetermined distance from the mounting module, and transmits the rotational force due to rotation to the mounting module;
a connecting member coupled to the rotation driving unit, covering the height adjustment member, and operable in the vertical direction with a joint positioned at one end of the upper end; and
The joint part is driven in the vertical direction, adjacent to one side of the height adjustment member so that the balance adjustment module is balanced, a piston movement part formed and performing a piston movement; Ground flight equipment trainer comprising a further comprising.
4. The method of claim 3,
The height adjustment member includes a plurality of height adjustment columns spaced apart from each other,
The balance control module,
Formed adjacent to the other side of the height adjustment member, the height adjustment member is a tension adjustment unit for adjusting the tension generated in the support wire as the length is extended or contracted; Ground flight equipment trainer comprising a further comprising: .
4. The method of claim 3,
The rotary drive unit,
a gimbal body in which one side is bolted to the mounting module, and the other side is formed with a ball bearing rotating based on the height adjustment member; and
Ground flight equipment trainer, characterized in that it further comprises; receiving at least a portion of the ball bearing, coupled to the ball bearing, the bearing housing coupled to the connection member.
6. The method of claim 5,
The height adjustment member includes a plurality of height adjustment columns spaced apart from each other,
The mounting module is
a first lower landing gear and a second lower landing gear supporting the lower side at a position adjacent to the lower side of the mounted object and spaced apart from each other by a predetermined distance;
Connection gears spaced apart from one side of each gimbal body coupled to each of the height adjustment pillars and nut-coupled;
an upper gear connecting each of the connecting gears, and enclosing and fixing an upper portion of the mounted object;
a first intermediate gear connected to each of the connecting gears and the first lower landing gear to support both sides of the mounted object; and
Ground flight equipment trainer further comprising a; a second intermediate gear connected to each of the connection gears and the second lower landing gear to support both sides of the mounted object.
7. The method of claim 6,
One end is connected to a portion of each of the height adjustment pillars, in a direction perpendicular to the longitudinal direction of the height adjustment pillar, and the other end is formed in contact with the floor as it is formed in the longitudinal direction and the horizontal direction of the height adjustment pillar The ground flight equipment trainer, characterized in that it further comprises; a plurality of auxiliary members to support the balance of the ground flight equipment trainer.
7. The method of claim 6,
The piston movement unit includes a plurality of piston movement units formed adjacent to each of the height adjustment pillars,
The plurality of piston movement parts, ground flight equipment trainer, characterized in that the piston movement by adjusting the hydraulic pressure so that the joint parts adjacent to each of the height adjustment posts can be driven in different directions according to the driving of the gimbal body
5. The method of claim 4,
The tension control unit includes a plurality of hydraulic cylinders formed on one side of each of the height adjustment pillars,
The hydraulic cylinders are ground flight equipment trainer, characterized in that connected by a hydraulic hose.
According to claim 1,
In a state in which the mounting module is separated from the balance control module, after the object is mounted on the mounting module, as the mounting module on which the object is mounted is coupled to the balance control module, the object is test-flyed ground flight equipment trainer.
According to claim 1,
The object is a ground flight equipment trainer, characterized in that the flight body.

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