KR20090084620A

KR20090084620A - Apparatus for flight game

Info

Publication number: KR20090084620A
Application number: KR1020080026943A
Authority: KR
Inventors: 이응준
Original assignee: 이응준
Priority date: 2008-02-01
Filing date: 2008-03-24
Publication date: 2009-08-05

Abstract

The present invention relates to a flight ride. Flight play equipment of the present invention, the mainframe is connected to the cable or wire of the instrument support to float in the air (浮揚); An auxiliary frame positioned inside the main frame and connected to the main frame by a rotating member; A propeller installed inside the auxiliary frame and rotated by an electric motor or an engine; A rudder unit installed at an auxiliary frame facing the propeller and having an angle changed by a control panel installed in the auxiliary frame; And a seat installed inside the auxiliary frame and spaced apart from the propeller so as to be seated by the user, wherein the mainframe suspended on the cable or wire is moved by the rotation of the propeller.

Description

Flight rides {Apparatus for flight game}

The present invention relates to a flight rides, and more particularly to a flight rides that can fly freely in the air by using a propeller.

In general, a ride means a ride of a roller coaster, a monorail, etc. in an amusement park. In other words, the ride is a device that is moved or rotated at high speed in order for the user to feel a thrill, tension, and the like.

Recently, new rides are being developed by users' desire to feel a higher thrill or tension than existing ones.

However, there is a problem in that the rides on which the users are boarded are operated only by a predetermined movement such as being moved along a rail or rotated by a rotating body, so that the users easily lose interest.

The present invention was devised to solve the above problems, and to provide a flying ride that can be rotated or moved in various directions according to the user's choice by being floated in the air to improve the thrill or tension. have.

In order to achieve the above object, the flight play equipment of the present invention includes a main frame connected to the cable or the wire of the instrument support to float in the air (浮揚); An auxiliary frame positioned inside the main frame and connected to the main frame by a rotating member; A propeller installed inside the auxiliary frame and rotated by an electric motor or an engine; A rudder unit installed at an auxiliary frame facing the propeller and having an angle changed by a control panel installed in the auxiliary frame; And a seat installed inside the auxiliary frame and spaced apart from the propeller so as to be seated by the user, wherein the mainframe suspended on the cable or wire is moved by the rotation of the propeller.

In this case, the propeller further comprises a pitch member for changing the blade angle of the propeller, the pitch member includes a connecting member connected to each blade of the propeller, and a cylinder or servomotor connected to the connecting member to reciprocate the connecting member, the cylinder or The direction of the propulsive force of the propeller is changed by moving the connecting member by a predetermined distance using the servomotor to change the wing angle.

On the other hand, the rudder part is provided with a vertical rudder installed on the first fixing bar installed in the auxiliary frame in the vertical direction, and rotated by the first rotating shaft, the vertical rudder is provided with a vertical turning key protruding to both sides It is preferable that the wires are connected so that both sides of the vertical pivot key and the steering wheel are connected so that the vertical rudder is rotated at an angle by the steering wheel.

In addition, the rudder part is provided with a horizontal rudder installed on the second fixing bar installed in the auxiliary frame in the horizontal direction, and rotated by the second rotating shaft, and the horizontal rudder is provided with horizontal turning keys protruding to both sides. It is preferable that the wires are connected so that both sides of the horizontal pivoting key and the steering wheel are connected so that the horizontal rudder is rotated by an angle.

In addition, a brake pedal is installed on the auxiliary frame to stop the rotation of the auxiliary frame, and the rotation of the auxiliary frame is stopped by bringing a piston provided in the rotating member into close contact with the main frame.

In addition, a hand brake is installed in the auxiliary frame to stop the rotation of the auxiliary frame, and the wire moved by the operation of the hand brake stops the rotation of the auxiliary frame by bringing a brake shoe provided on the outside of the rotating member in close contact with the rotating member. .

The auxiliary frame is preferably made of a wire mesh to facilitate ventilation according to the rotation of the propeller.

Preferably, seat belts are installed in the seats.

In addition, it is desirable to provide a radio transceiver to the flight play equipment to wirelessly control the operation of the brake pedal, the pitch member and the rudder part.

In addition, the weight may be further installed on the auxiliary frame in the front of the seat to have a weight corresponding to the propeller and the rudder provided on the back of the seat.

According to an aspect of the present invention, there is provided a flying play equipment including: a main frame connected to a cable or a wire of an apparatus supporter so as to float in the air; An auxiliary frame positioned inside the main frame and connected to the main frame by a rotating member; A propeller installed inside the auxiliary frame and rotated by an electric motor or an engine; A seesaw section installed to rotate with the propeller; A swash plate installed on the rotating shaft of the propeller, the swash plate being connected to each blade and the seesaw of the propeller so as to reciprocate in the longitudinal direction of the rotating shaft; And a seat installed inside the auxiliary frame and spaced apart from the propeller so as to be seated by the user, wherein the mainframe suspended on the cable or wire is moved by the rotation of the propeller.

On the other hand, further comprising a pitch member for changing the inclination of the blade angle of the propeller and the rotational surface of the propeller, the pitch member reciprocating the swash plate and the link portion provided to connect the swash plate and each wing and seesaw portion of the propeller And a cylinder and a servomotor which are moved to have an inclination in the front, rear, left, and right directions, and by moving the swash plate by a predetermined distance using the cylinder or the servomotor to change the vane angle and the plane of rotation so that the propeller's direction and external force are changed. It is preferable that the direction of is changed.

In addition, the brake pedal is provided on the auxiliary frame to stop the rotation of the auxiliary frame, it is preferable that the hydraulic pressure by the brake pedal to stop the rotation of the auxiliary frame by bringing the piston provided in the rotating member in close contact with the main frame.

In addition, the hand brake is installed on the auxiliary frame to stop the rotation of the auxiliary frame, the wire which is moved by the operation of the hand brake closes the brake shoe provided on the outer side of the rotating member to the rotating member to stop the rotation of the auxiliary frame. It is preferable.

At this time, the auxiliary frame is made of a wire mesh to facilitate ventilation according to the rotation of the propeller, the seat belt is installed on the seat.

In addition, it is desirable to provide a radio transceiver to the flight play equipment to wirelessly control the operation of the brake pedal and the pitch member.

In addition, the weight may be further installed on the auxiliary frame on the front of the seat to have a weight corresponding to the propeller and the pitch member provided on the back of the seat.

The flying rides according to the present invention can be provided to be moved in the air to make the user feel thrill and tension, and the user can add fun as the user directly manipulates the rides. In addition, unlike the existing rides, it is not moved along a predetermined section, it can be selectively moved in various directions. In addition, by changing the propeller blade angle (pitch) and the angle of the rudder can be quickly changed direction and can be rotated, the longer the life of the motor or engine by eliminating the need for reverse rotation of the motor or engine to rotate the propeller Lose.

Hereinafter, exemplary embodiments of the present invention will be described in detail with reference to the accompanying drawings. Prior to this, terms or words used in the specification and claims should not be construed as having a conventional or dictionary meaning, and the inventors should properly explain the concept of terms in order to best explain their own invention. Based on the principle that can be defined, it should be interpreted as meaning and concept corresponding to the technical idea of the present invention. Therefore, the embodiments described in the specification and the drawings shown in the drawings are only the most preferred embodiment of the present invention and do not represent all of the technical idea of the present invention, various modifications that can be replaced at the time of the present application It should be understood that there may be equivalents and variations.

1 is a view showing a state in which a flying rides according to a first embodiment of the present invention is installed on the instrument support, Figure 2 is a side cross-sectional view showing the flying rides, Figure 3 is an auxiliary frame of the flying rides It is a sectional front view which shows the state rotated with respect to this mainframe.

1 to 3, the flight ride 100 is the main frame 101, the auxiliary frame 110, which is located inside the main frame 101 is rotatably coupled by the rotating member 124, auxiliary The angle is changed by the propeller 130 installed inside the frame 110 to rotate, the pitch member 140 for changing the wing angle of the propeller 130, and the control panel 150 installed on the auxiliary frame 110. The rudder unit 160 and the propeller 130 are provided with a seat 170 spaced apart from the predetermined interval.

The main frame 101 is made of a '∩' shape as a rigid material, the cable or wire of the instrument support 10 (hereinafter, for convenience of description, the cable or wire will be described as a 'cable') Connected to (11) is located in the air. In this case, the cable 11 is preferably connected to the upper end of the main frame 101.

In the present specification, the main frame 101 is illustrated and described in a '∩' shape, but is not limited thereto, and the auxiliary frame 110 to be described later is installed to be rotatable inside, and the propeller 130 is rotated. If the output is generated, that is, the wind is formed to pass through any structure and shape can be employed.

The auxiliary frame 110 is located inside the main frame 101 and is coupled by the rotating member 124 to be rotatable to the main frame 101. That is, as shown, the auxiliary frame 110 is made of a sphere (circle) shape, the rotating member 124 is installed on both sides to enable rotation. At this time, the auxiliary frame 110 is preferably made of a wire mesh so that the thrust generated during the rotation of the propeller 130 installed therein, that is, the wind passes. That is, the auxiliary frame 110 may be employed in any shape and structure as long as it is made to protect the components located inside and at the same time through the inside and the outside.

On the other hand, the brake pedal 120 is installed on the auxiliary frame 110 to stop the rotation of the auxiliary frame 110. The method of composing the rotation of the auxiliary frame 110 is a method using hydraulic pressure. When the hydraulic pressure is moved to the main frame 101 by the brake pedal 120, the piston 127 provided on the rotating member 124 is moved. The pad 128 attached to the 127 is in close contact with the main frame 101 to stop the rotation of the auxiliary frame 110. More specifically, with reference to Figure 4, the rotating member 124 is made of a cylindrical shape, the main frame 101 in contact with the rotating member 124, the rotating member 124 is easily rotated so that the bearing ( 115) is installed. At this time, the rotating member 124 is a caliper housing 125 installed in the auxiliary frame 110 to rotate with the main frame 101, the hydraulic chamber 126 provided in the caliper housing 125, and the hydraulic chamber ( A hose 129 for supplying hydraulic pressure to the 126, a piston 127 provided in the hydraulic chamber 126 and moved by hydraulic pressure introduced through the hose 129, and a pad 128 attached to the piston 127. It is provided.

When the auxiliary frame 110 is rotated by the rotating member 124, when pressure is applied to the brake pedal 120 installed on the auxiliary frame 110, the rod 122 installed on the brake pedal 120 is a hydraulic tank ( The fluid stored in the 123 is pushed and moved to the hydraulic chamber 126 through the hose 129. Therefore, when the piston 127 provided in the hydraulic chamber 126 is moved to the main frame 101 by hydraulic pressure, the pad 128 attached to the piston 127 is in close contact with the main frame 101 to assist by friction. Frame 110 is stopped. At this time, the rotating member 124 installed on both sides of the auxiliary frame 110 is operated at the same time. The brake pedal 120 is connected to the return spring 121 to return to the home position when the pressure applied to the brake pedal 120 is removed.

Although the structure for stopping the auxiliary frame 110 using the brake pedal 120 as described above is described with reference to the example using hydraulic pressure, the present invention is not limited thereto, and the auxiliary frame 110 may be used in the pneumatic or mechanical manner. It is obvious that it can be stopped.

On the other hand, the hand brake 190 is further installed on the auxiliary frame 110 to stop the rotation of the auxiliary frame 110. A method of composing the rotation of the auxiliary frame 110 is a method using a brake shoe 193, and the brake shoe 193 pulled by the hand brake 190 is provided on the outside of the rotating member 124. By stopping the contact with the rotating member 124 to stop the rotation. More specifically, as shown in FIG. 5, the cover 192 is installed on the main frame 101 connected to the rotating member 124, and the brake is in close contact with the rotating member 124 inside the cover 192. A shoe 193 is provided and has a brake belt 194 connected to move the brake shoe 193. At this time, the brake shoe 193 is provided in the cover 192 in a state spaced apart along the outer circumferential surface of the rotating member 124. In addition, the brake shoe 193 is installed on the cover 192 by the return spring 195 to return to the correct position when the pressure by the hand brake 190 is removed. The brake shoe 193 is connected to the brake belt 194 to be in close contact with the rotating member 124 by the rotation operation of the hand brake 190 to control the rotation of the auxiliary frame 110. The structure for stopping the auxiliary frame 110 by using the hand brake 190 as described above is generally made of a structure similar to the hand brake of a vehicle, and thus a detailed description thereof will be omitted.

An electric motor or an engine (hereinafter, the electric motor or the engine will be described as a 'engine' for convenience of explanation) 141 is installed inside the auxiliary frame 110 and rotates the rotary shaft 131 of the propeller 130. Let's do it. Preferably, the rotating shaft 131 may be rotated by being coupled to the drive shaft of the engine 141, the drive shaft of the engine 141 may be directly connected to the propeller 130. Therefore, the rotation shaft 131 of the propeller 130 will be described as being the drive shaft of the engine.

Accordingly, the propeller 130 is rotated by the engine 141, and when the propeller 130 is rotated, thrust is generated to move the main frame 101 suspended on the cable 11.

On the other hand, the auxiliary frame 110 supports the rotating shaft 131, the bearing 135 is installed so that the rotating shaft 131 is inserted and rotated.

The propeller 130 as described above is composed of a rotating shaft 131, a boss 133 inserted into and fixed to the rotating shaft 131, and a plurality of wings 132 installed on the boss 133. That is, as the rotary shaft 131 rotates, the boss 133 fixed to the rotary shaft 131 is rotated at the same time, and the blade 132 installed in the boss 133 rotates. At this time, the wing 132 is installed to rotate a predetermined angle with respect to the boss 133.

At this time, the change of the moving direction of the play equipment 100 is made by a change in the blade angle, that is, the pitch of the propeller 130. The pitch is changed by the sebum member 140. The blade angle is changed because the blade 132 is rotated by a predetermined angle along the connecting member 142 connected to the piston 148 reciprocated by the pressure of the cylinder 144 of the pitch member 140.

In addition, since the moving speed of the main frame 101 and the rotational speed of the auxiliary frame 110 vary depending on the rotational speed of the propeller 130 and the wing angle of the propeller 130, the moving speed and the auxiliary speed of the main frame 101 are changed. The rotational speed of the frame 110 can be freely changed. In addition, when the main frame 101 is to be suddenly stopped, the pitch may be changed. In other words, by changing the blade angle (pitch) without changing the rotation direction of the engine 141, the engine 141 does not need to be reversely rotated, thereby improving the life of the engine 141.

The pitch member 140 for changing the wing angle of the propeller 130 as described above, the cylinder 144 to move the connecting member 142 and the connecting member 142 connected to each blade 132 of the propeller 130. Or servomotor. Hereinafter, a cylinder or servomotor for moving the connecting member 142 will be described as using a cylinder for convenience of description. That is, when the connecting member 142 connected to each blade 132 is moved using the cylinder 144, the blade 132 is connected to the connecting member 142 and receives a force in one direction, so the pitch of the blade 132 is increased. Is changed.

At this time, it is preferable that two wings 132, the connection member 142 is more preferably connected to the opposite side to the two wings 132. That is, when the connecting member 142 is moved by the cylinder 144, each wing 132 connected to the connecting member 142 is connected to the connecting member 142 on the opposite side, so that the wings 132 move in opposite directions to each other. The pitch of 132 is changed.

More specifically, the movement of the connection member 142 is made by the cylinder 144, the cylinder 144 is formed on one side and the other side of the cover 146, cover 146, the tube 145 is built in pneumatic The first port 146a and the second port 146b, which are introduced or discharged, and a piston 148 provided inside the tube 145 to be moved by pneumatic and having a piston rod 149. At this time, the piston rod 149 is coupled to the connecting member 142. Therefore, when air is introduced into the first port 146a formed at one side of the cylinder 144 and pneumatic pressure is generated, the piston 148 is pushed in the direction in which the propeller 130 is installed and the connecting member coupled to the piston rod 149 ( 142 is moved. At this time, the air escapes to the second port 146b formed on the other side of the cylinder 144. Similarly, when air flows into the second port 146b formed at the other side of the cylinder 144, the piston 148 is moved in a direction away from the propeller 130. Here, the forward movement of the piston 148 in the direction of the propeller 130 is called, and the backward movement of the piston 148 is moved away from the propeller 130.

As the piston 148 of the cylinder 144 is reciprocated, the connecting member 142 coupled with the piston rod 149 is reciprocated together in the longitudinal direction of the rotation shaft 131. Thus, the pitch of the blade 132 connected with the connecting member 142 is changed. At this time, since the bearing 147 is installed between the connecting member 142 and the piston rod 149, only the connecting member 142 is rotated according to the rotation of the rotating shaft 131. In addition, a bearing 143 is installed between the rotating shaft 131 and the cylinder 144, so that the cylinder 144 is not rotated. In addition, although not shown, a bearing is preferably installed between the rotation shaft 131 and the piston rod 149.

In this case, the bearings 143 and 147 are installed, but only the connecting member 142 is expressed as being rotated. However, the present invention is not limited thereto, and the cylinder 144 is rotated together with the rotating shaft 131 to connect the connecting member 142. Various embodiments may be applied, such as being configured to move.

In addition, the cylinder 144 is represented as moving the connection member 142, but is not limited to this, by moving the connection member 142, such as moving the connection member 142 using a servo motor propeller ( If the wing angle of 130) can be changed, any structure may be employed.

More specifically, the pitch of the propellers will be described with reference to FIGS. 6A to 6C.

6A shows a state in which the pitch of the blade 132 of the propeller 130 is not changed. Therefore, even if the propeller 130 is rotated by the rotating shaft 131, the main frame 101 and the auxiliary frame 110 is stopped in place because the blade 132 does not have an angle. This is because pitch is not formed in the blade 132, and thrust is not generated.

6B shows a state in which the propeller 130 whose pitch of the blade 132 is changed is rotated by the rotation of the rotation shaft 131. At this time, the blade 132 is the pitch of the cross section is changed, the connection member 142 connected to the blade 132 is to change the pitch of the blade 132 by the pressure of the cylinder 144. For example, when pressure is introduced into the first port 146a and the piston 148 is advanced, the connecting member 142 connected to the piston rod 149 is extended in the longitudinal direction of the rotation shaft 131, that is, in the direction of the propeller 130. It is moved, the blade 132 connected to the connecting member 142 is rotated by a predetermined angle in the opposite direction with respect to the boss 133. Therefore, since the blade 132 has a pitch, as the propeller 130 is rotated by the rotation shaft 131, thrust is generated in the direction of the arrow A. FIG. Therefore, the main frame 101 is moved or the auxiliary frame 110 is rotated.

6C shows a state in which the blade 132 of the propeller 130 is rotated in another direction. As mentioned above, the pitch of the vanes 132 is converted by the pressure of the cylinder 144. For example, in the blade 132 of FIG. 6B, when the pressure flows into the second port 146b of the cylinder 144, the piston 148 retreats to move the connecting member 142. The wing 132 connected with the 142 rotates in opposite directions with respect to the boss 133. That is, the pitch is formed so as to face in the opposite direction to the blade 132 in Fig. 6b. Thus, as the propeller 130 is rotated by the rotation shaft 131, the thrust is generated in the direction of the arrow B. Here, the pitch of the vanes 132 of the propeller 130 is changed while the propeller 130 is being rotated. That is, by changing the pitch of the wing 132 without rotating the engine 141, it is possible to change the direction of the flight rides 100, and also does not give the engine 141, the flight rides 100 ) Can be easily stopped.

On the other hand, the piston 148 of the cylinder 144 for changing the pitch of the blade 132 as shown above is shown and expressed as rotating the blade 132 by moving forward or backward to one end and the other end by the pressure, but It is not limited, it is possible to adjust the pitch of the blade 132 by adjusting the moving distance of the piston 148 by adjusting the pressure. Therefore, the thrust generated according to the pitch of the wing 132 is changed to adjust the moving speed of the flight rides (100).

Such pitch adjustment may be controlled by the pitch control lever 180. That is, when the pitch control lever 180 is pushed forward, pressure is introduced into the first port 146a, and when the pitch is adjusted backward, pressure is introduced into the second port 146b. Since this structure is a well known technique, a detailed description thereof will be omitted.

1 to 3 again, the auxiliary frame 110 is provided with a rudder unit 160 for changing the direction. The rudder unit 160 is installed at a position facing the propeller 130 so as to rotate together with the rotation of the auxiliary frame 110. This is to switch the moving direction of the main frame 101 and the rotation direction of the auxiliary frame 110 by using the thrust generated by the rotation of the propeller (130). The rudder unit 160 is changed in angle by the steering wheel 150.

Here, the rudder unit 160 according to the present invention described below is preferably made of at least one of the vertical rudder 161 or the horizontal rudder 165, both the vertical rudder 161 and the horizontal rudder 165 is installed Since this is the most preferred embodiment mode, the rudder unit 160 in which the vertical rudder 161 and the horizontal rudder 165 are installed will be described as an example for convenience of description. That is, the rudder unit 160 may be formed of any one of the vertical rudder 161 and the horizontal rudder 165.

More specifically, referring to FIG. 7, the rudder unit 160 is formed by the vertical rudder 161 rotated by the first rotating shaft 163 installed in the vertical direction and the second rotating shaft 167 installed in the horizontal direction. A horizontal rudder 165 is rotated.

The vertical rudder 161 is provided on the first rotation shaft 163 installed to rotate on the first fixing bar 162 installed on the auxiliary frame 110. At this time, the vertical rudder 161 is provided with a vertical pivot key 164 protruding to both sides of the direction intersecting the first rotation shaft 163. Wires 169a are connected to both sides of the vertical pivot key 164, respectively, and are connected to the vertical keys 154 of the steering wheel 150. Here, the vertical pivot key 164 and the wire 169a connecting the vertical key 154 of the steering wheel 150 are connected to cross each other. The vertical rudder 161 is rotated by the steering wheel 150 and the angle is converted to change the direction so that the main frame 101 moves in the left and right directions. That is, when the vertical rudder 161 is rotated to the right by the steering wheel 150, the thrust of the propeller 130 is switched by the vertical rudder 161 whose angle is changed to move the play equipment 100 in the right direction. Is changed. In addition, when the vertical rudder 161 is rotated to the left by the steering wheel, the movement of the play equipment 100 is changed to the left direction.

The horizontal rudder 165 is provided on the second rotating shaft 167 installed to rotate on the second fixing bar 166 installed on the auxiliary frame 110. At this time, the horizontal rudder 165 is provided with a horizontal pivot key 168 protruding to both sides of the direction intersecting the second rotation shaft 167. Wires 169b are connected to both sides of the horizontal pivot key 168, respectively, and are connected to the horizontal keys 158 of the steering wheel 150. The horizontal rudder 165 serves to rotate the auxiliary frame 110 as well as the function of raising and lowering the play equipment 100. For example, when the horizontal rudder 165 is rotated by the steering wheel 150 and rotated upward, the thrust of the propeller 130 is changed by the horizontal rudder 165 whose angle is changed to move the play equipment 100. This changes in the upward direction. In this case, the auxiliary frame 110 may be installed to rotate on the main frame 101 so that the auxiliary frame 110 may be rotated. Similarly, when the horizontal rudder 165 is rotated downward by the steering wheel 150, the movement of the play equipment 100 is changed downward.

The operation in which the vertical rudder 161 and the horizontal rudder 165 are rotated by the steering wheel 150 will be described with reference to FIGS. 8 and 9.

8 illustrates a state in which the vertical rudder 161 is rotated by the steering wheel 150. The control panel 150 is composed of a handle 151 and a moving shaft 152 that can be gripped by a user in a stick shape, and a vertical key connected to the wire 169a connected to the vertical rudder 161 on the moving shaft 152. 154 is provided. At this time, the steering wheel 150 is rotated by the pin 152 'is made to rotate as well as rotate forward and backward. Here, the steering wheel 150 is rotated to rotate the vertical rudder 161. For example, as shown in FIG. 8A, wires 169a connected to both sides of the vertical key 154 of the control panel 150 so as to intersect the vertical pivot key 164 of the vertical rudder 161, respectively. Since the connected state, when rotating the steering wheel 150 to the left side is moved to the left side of the vertical key 154 to the rear, the right side of the vertical key 154 is moved to the front. Accordingly, as the vertical key 154 is rotated, the vertical pivot keys 164 connected by the crossed wires 169a are rotated together. That is, the left portion of the vertical pivot key 164 is moved forward and the right portion is moved backward so that the vertical rudder 161 is rotated leftward. Similarly, as shown in (b) of FIG. 8, when the control panel 150 is rotated to the right, the right side of the vertical key 154 rotates toward the rear, and the right side of the vertical pivot key 164 rotates to the front. As a result, the vertical rudder 161 is rotated to the right. At this time, it is obvious that the rotation angle of the vertical rudder 161 is rotated so as not to hit the horizontal rudder 165.

9 illustrates a state in which the horizontal rudder 165 is rotated by the steering wheel 150. At this time, the moving shaft 152 of the control panel 150 is made to be rotatable by the pin 152 ', the moving shaft 152 is connected to the horizontal key 158 by the connecting bar 153. The moving shaft 152 is rotated forward and backward to adjust the angle of the horizontal rudder 165. For example, wires 169b connected to both sides of the horizontal pivot key 168 are connected to both sides of the horizontal key 158. Accordingly, as shown in (a) of FIG. 9, when the control panel 150 is pushed forward, the lower side of the horizontal key 158 is moved forward by the connecting bar 153 connected to the horizontal key 158. And the upper side is moved to face rearward. Accordingly, the lower side of the horizontal turning key 168 is moved forward by the wire 169b connected to the horizontal key 158, and the upper side is moved rearward so that the horizontal rudder 165 is rotated downward. . Similarly, as shown in (b) of FIG. 9, when the steering wheel 150 is pulled backward, the upper part of the horizontal key 158 and the lower part of the horizontal pivot key 168 are rotated to face rearwards so that the horizontal rudder ( 165) is rotated upwards.

According to the angle change of the vertical rudder 161 and the horizontal rudder 165 as described above, it is possible to switch the flight direction, that is, change the direction of movement of the main frame 101 and the rotation direction of the auxiliary frame 110.

Referring back to FIGS. 1 to 3, a seat 170 is provided inside the auxiliary frame 110. The seat 170 is provided to be seated by the user riding on the flight rides 100, it is preferable that the seat belt 172 is installed. In this case, the seat 170 is provided at a position spaced apart from the propeller 130 provided at the rear of the seat 170 by a predetermined interval. This is to prevent the user's body from hitting the propeller (130). In addition, a protective plate (not shown) may be installed between the seat 170 and the propeller 130 to prevent the occurrence of a safety accident for the user.

The flying rides 100 as described above, the user directly manipulates the movement of the ride in a state floated in the air, by being moved or rotated by the thrust generated by the rotation of the propeller 130, the user feels a thrill, a sense of tension It can satisfy even the fun of manipulating the rides directly. These rides can be moved in the direction of the arrow, as shown in Figure 10 (a) and (b), the auxiliary frame 110 is rotated while moving in the direction of the arrow to increase the fun. In addition, the movement direction shown in FIG. 10 is represented as an example, and it may be apparent that the movement direction may be rotated or moved in various directions according to a user's manipulation.

In addition, the flight ride 100 is shown as one seat 170 is provided, but is not limited to this, by providing a plurality of seats to operate a professional skilled in the operation of the ride 100 is operated ride 100 ) May make the ride a lot more fun, thrills, and tension.

Meanwhile, the flight ride 100 includes a wireless communication device to be adjusted wirelessly. To this end, the flight ride 100 is provided with a receiving circuit unit (not shown) and is controlled by a controller which is a transmitting circuit unit. That is, the controller controls the pitch member 140, the engine 141, the steering wheel 150, and the rotation member 124 of the flight ride 100. Such a structure using a wireless is commonly used, detailed description thereof will be omitted.

Additionally, although not shown in the figures, weights may be further installed in the subframe 110 in front of the seat 170. The weight has a weight corresponding to that of the propeller 130 and the rudder 160 provided at the rear of the seat 170. This is to easily maintain the center of gravity by having the same weight on both sides, that is, the front side and the rear side around the seat 170. Thus, the auxiliary frame 110 can be rotated with little force. Therefore, the weight is formed by the same weight as the weight of the propeller 130 and the rudder 160, the engine for transmitting the rotational energy of the propeller 130 and the propeller 130 to rotate the auxiliary frame 110 ( 141) saves energy and facilitates the change of direction movement.

FIG. 11 is a side cross-sectional view showing a flying rides according to a second embodiment of the present invention, FIG. 12 is a partial side view of the flying rides, FIG. 13 is a sectional view showing a swash plate of the flying rides, FIG. 14 is a view showing a state in which the rotation surface of the propeller is inclined by the pitch member of the flying play equipment.

11 to 14, the flight ride 200 is the main frame 101, the auxiliary frame 110, which is located inside the main frame 101 is rotatably coupled by the rotating member 124, It is connected to the propeller 130 is installed and rotated in the auxiliary frame 110, the seesaw unit 260 installed to rotate with the propeller 130, each wing 132 and the seesaw unit 260 of the propeller 130 A swash plate 250 configured to reciprocate in the longitudinal direction of the rotation shaft 131 of the propeller 130, a pitch member 240 for changing the blade angle and the inclination of the rotation surface of the propeller 130, and the propeller 130. And a seat 170 installed at a predetermined interval apart. 11 to 14, the main frame 101, the auxiliary frame 110, the brake pedal 120, the rotation member 124, the propeller 130, the seat 170, and the hand in FIG. The brake 190 denotes the same reference numeral and the same component. That is, the flying rides 200 has substantially the same function as the flying rides 100 shown in FIGS. 1 to 10. However, the swash plate 250 and the seesaw section 260 are different in the structure of changing the inclination of the pitch angle and the rotation surface of the propeller 130 by the pitch member 240.

According to the second embodiment of the present invention, the propeller 130 is rotated by receiving the rotational power of the engine 141. Here, the propeller 130 is composed of a rotating shaft 131, a boss 133 inserted into and fixed to the rotating shaft 131, and a plurality of blades 132 provided on the boss 133. That is, as the rotary shaft 131 rotates, the boss 133 fixed to the rotary shaft 131 is rotated at the same time, and the blade 132 installed in the boss 133 rotates. At this time, the wing 132 is installed to rotate a predetermined angle with respect to the boss 133. In addition, the rotation shaft 131 is installed to be supported by the auxiliary frame 110 to rotate. The seesaw unit 260 is installed to rotate together with the propeller 130.

The seesaw section 260 is installed in a direction crossing the propeller 130, and auxiliary wings 262 are formed at both ends of the seesaw section 260. The seesaw 260 is rotated at a predetermined angle in the longitudinal direction of the rotary shaft 131, the auxiliary blade 262 is installed to rotate a predetermined angle relative to the rotary shaft 131. The seesaw 260 serves to return the rotation surface of the propeller 130 to its original position when the engine 131 rotates.

The swash plate 250 is installed on the rotation shaft 131, preferably on the rotation shaft 131 between the engine 141 and the propeller 130. More specifically, the swash plate 250 is the upper plate 252 is inserted into the rotating shaft 131 of the propeller 130, and the sperry disposed between the inner diameter of the upper plate 252 and the outer diameter of the rotating shaft 131 Curl bearing 253, the lower plate 254 is fastened to surround the outer diameter surface of the lower end of the upper plate 252, and the ball bearing 256 disposed between the inner diameter of the lower plate 254 and the outer diameter of the upper plate 252. It is provided. At this time, the upper fastening portion 251 for connecting to the propeller 130 and the seesaw portion 260 is formed on the outer circumferential surface of the upper plate 252, the pitch member 240 to be described later on the outer circumferential surface of the lower plate 254 The lower fastening part 255 is formed to be connected to the servomotor. Therefore, the swash plate 250 adjusts the angle of the wing 132, the seesaw 260, and the auxiliary wing 262 of the propeller 130 by the pitch member 240.

The swash plate 250 is installed to reciprocate in the longitudinal direction of the rotation shaft 131. In addition, the lower plate 254 is not rotated together with the rotation shaft 131 by the ball bearing 256, it is made to be inclined by a predetermined angle relative to the rotation shaft 131.

The swash plate 250 as described above is a device for controlling the inclination of the wing angle and the rotation surface of the propeller of the helicopter, which is already well known, and adjusts the inclination of the wing angle and the rotation surface of the propeller 130 by the sebum member 240 do.

On the other hand, the pitch member 240 for changing the inclination of the blade angle and the rotation surface of the propeller 130, so that each blade 132 and the seesaw 260 and the swash plate 250 of the propeller 130 is connected An installed link unit 242 and a cylinder or servomotor (not shown) for reciprocating the swash plate 250 or moving them to have an inclination in the front and rear directions. Hereinafter, it will be described as using a servo motor for convenience of description among cylinders or servomotors for moving the swash plate 250. That is, when the swash plate 250 is moved in the longitudinal direction of the rotation shaft 131 by a predetermined distance using a servo motor, the blades of the propeller 130 may be moved by the link unit 242 connected to the swash plate 250. Since the 132 is forced in one direction, the pitch of the wings 132 is changed. In addition, as the swash plate 250 is inclined, the rotational surface of the propeller 130 is changed to change the direction of the external force of the propeller 130.

More specifically, the link unit 242 may include a first link stage 243 connecting the lower fastening unit 255 of the lower plate 254 and the moving unit 246 of the servo motor, and an upper plate 252 to each other. It consists of a second link end 244 connecting the blade 132 and the seesaw 260, the second link end 244 is each wing 132 and the seesaw 260 by a link arm 245 Is connected to rotate. At this time, the lower plate 254 of the swash plate 250 is inclined to have an inclination by the first link end 243 connected to the servomotor, or the swash plate 250 is moved in the longitudinal direction of the rotation shaft 131. It is to change the inclination of the blade angle and the rotation surface of the propeller (130).

As described above, the structure for changing the inclination of the wing angle and the rotation surface of the propeller with the swash plate 250 is described in Korean Utility Model No. 295729 and 2006-0052643.

Controlling the blade angle of the propeller 130 is referred to as collective pitch control, and controlling the tilt of the rotating surface of the propeller 130 is referred to as cyclic pitch control.

The collective pitch control changes the direction of the propulsion force generated as the propeller 130 rotates by changing the wing angle of the propeller 130. As described above, as the swash plate 250 moves in the longitudinal direction of the rotation shaft 131, the pitch of the blade 132 is changed by the second link end 244 connected to the swash plate 250. This structure is the same as the structure for changing the blade angle of the propeller 130 described in the first embodiment will be omitted detailed description. However, in the first embodiment, the pitch of the propeller 130 and the blade 132 is adjusted by using the cylinder 144. However, in the second embodiment using the swash plate 250, there is a difference in using the servo motor. . The control of the servomotor can be controlled by the operation button 270 using a wireless or wired, the control structure using a wired / wireless is already known technology, so the detailed description will be omitted.

The cyclic pitch control changes the direction by using the lifting force of the propeller 130 by changing the inclination of the rotation surface of the propeller 130. That is, it provides a balance and an unbalanced lifting force of the left and right and the front and rear of the rotating surface. This structure uses a gyro presession, which means that the force is generated at a point 90 ° late in the rotation direction when a force is transmitted to any part. Referring to FIG. 15, when the pitch of the blade 132 is 0 ° and the lower plate 254 is inclined by a predetermined angle in the 90 ° direction of the rotation surface, the 180 ° direction is caused by the action of the second link end 244. The pitch of the auxiliary wing 262 is a positive pitch, the pitch of the auxiliary wing 262 in the 0 ° direction is converted to a negative pitch. At this time, the pitch of the blade 132 of the propeller 130 is not changed.

In the above state, when the wing 132 of the propeller 130 and the auxiliary wing 262 of the seesaw 260 rotates, the pitch of the wing 132 or the auxiliary wing 162 reaching the position of 90 ° is It becomes zero (0) and the pitch increases as it rotates in the 180 ° direction to become the highest positive pitch at 180 °, and if it continues to rotate, the pitch decreases and becomes the pitch of zero again in the 270 ° direction. It will continue to rotate and become the minimum negative pitch in the 0 ° direction. The pitch increases again as it passes through 0 °, again becoming a zero pitch at the 90 ° position. That is, the blade 132 and the auxiliary wing 162 is changed in pitch every cycle. At this time, the lift caused by the change in pitch has a phase difference of 90 ° with the pitch, and the effect appears later. Therefore, since lift is generated in the upward direction at the 180 ° position and lift is generated in the downward direction at the 0 ° position, the auxiliary frame 110 can be rotated and the main frame 101 can be moved left and right. That is, the movement of the flight rides 200 is controlled by the phase difference generated according to the inclination direction of the swash plate 250.

As a result, the swash plate 250 is connected to the propeller 130 and the seesaw part 260 by the pitch member 240 and operated by the operation button 270 provided in the auxiliary frame 110.

In addition, the flight ride 200 is shown as one seat 170 is provided, but is not limited to this, by providing a plurality of seats to operate the play equipment 100 by a professional skilled in operating the ride 200 ) May make the user more fun, thrilling, and nervous.

In addition, although not shown in the figure, the weight may be further installed in the auxiliary frame 110 in front of the seat 170. The weight has a weight corresponding to the propeller 130 and the pitch member 240 provided on the back of the seat 170. This is to easily maintain the center of gravity by having the same weight on both sides, that is, the front side and the rear side around the seat 170. Thus, the auxiliary frame 110 can be rotated with little force. Therefore, the weight is formed by the same weight as the weight of the propeller 130 and the pitch member 240, the engine for transmitting the rotational energy of the propeller 130 and the propeller 130 to rotate the auxiliary frame 110 ( 141) saves energy and facilitates the change of direction movement.

As described above, although the present invention has been described by way of limited embodiments and drawings, the present invention is not limited thereto and is intended by those skilled in the art to which the present invention pertains. Of course, various modifications and variations are possible within the scope of equivalents of the claims to be described.

1 is a view showing a state in which a flight rides according to a first embodiment of the present invention is installed on the equipment support.

2 is a side cross-sectional view showing a flight ride according to a first preferred embodiment of the present invention.

Figure 3 is a front sectional view showing a state in which the auxiliary frame of the flight ride according to the first embodiment of the present invention is rotated with respect to the main frame.

4 is a view showing a state of stopping the auxiliary frame of the flight rides according to the first embodiment of the present invention.

5 is a view showing another state of stopping the auxiliary frame of the flight rides according to the first embodiment of the present invention.

6a to 6c are views showing a state in which the propeller of the flight rides according to the first embodiment of the present invention is operated.

7 is a view showing a state in which the steering wheel and the rudder portion of the flight play equipment according to the first embodiment of the present invention.

8 is a view showing a state in which the vertical rudder of the flight rides according to the first embodiment of the present invention is operated.

9 is a view showing a state in which the horizontal rudder of the flight rides according to the first embodiment of the present invention is operated.

10 is an exemplary view showing a movement state of the flight rides according to the first embodiment of the present invention.

Fig. 11 is a side sectional view showing a flying play equipment according to a second preferred embodiment of the present invention.

12 is a partial side view showing a flight ride according to a second preferred embodiment of the present invention.

Fig. 13 is a sectional view showing a swash plate of a flight ride according to a second preferred embodiment of the present invention.

14 is a view showing a state in which the rotation surface of the propeller is inclined by the pitch member of the flight play equipment according to the second embodiment of the present invention.

15 is a reference diagram showing a state in which the rotation surface of the propeller is inclined by the gyro presession used in the second embodiment of the present invention.

10: instrument support 11: cable (wire)

100, 200: flight ride 101: mainframe

110: auxiliary frame 120: brake pedal

124: rotating member 130: propeller

140: pitch member 141: engine (motor)

142: connecting member 144: cylinder

150: steering wheel 160: rudder

161: vertical rudder 165: horizontal rudder

170: seat 180: pitch adjustment lever

190: Hand brake 193: Brake shoe

240: pitch member 242: link portion

250: swash plate 260: seesaw

270: operation button

Claims

A mainframe connected with a cable or a wire of the instrument support so as to float in the air;

An auxiliary frame positioned inside the main frame and connected to the main frame by a rotating member;

A propeller installed inside the auxiliary frame and rotated by an electric motor or an engine;

A rudder unit installed at an auxiliary frame facing the propeller and having an angle changed by a control panel installed in the auxiliary frame; And

A seat installed in the auxiliary frame and spaced apart from the propeller at a predetermined interval so that the user is seated;

A flight ride, characterized in that the mainframe suspended on the cable or wire is moved by the rotation of the propeller.

The method of claim 1,

Further comprising a pitch member for changing the wing angle of the propeller,

The pitch member includes a connecting member connected to each blade of the propeller, and a cylinder or servomotor connected to the connecting member to reciprocate the connecting member, and move the connecting member by a predetermined distance by using a cylinder or servomotor. Flight rides characterized in that the direction of propulsion of the propeller is changed by changing the.

The method of claim 1,

The rudder part includes a vertical rudder installed on the first fixing bar installed in the auxiliary frame in the vertical direction, and installed with the first rudder to be rotated by the first rotating shaft, and the vertical rudder provided with vertical turning keys protruding to both sides, and vertical The flight rides characterized in that the vertical rudder is rotated by a predetermined angle by the wire is connected so that both sides of the pivoting key and the steering wheel.

The method of claim 1,

The rudder part includes a horizontal rudder installed on the second fixing bar installed in the auxiliary frame in the horizontal direction and installed to be rotated by the second rotating shaft, and the horizontal rudder is provided with horizontal pivoting keys protruding to both sides. The flight rides, characterized in that the horizontal rudder is rotated by a certain angle by the wire is connected so that both sides of the pivoting key and the steering wheel is connected.

The method according to any one of claims 1 to 4,

A brake pedal is installed on the auxiliary frame to stop the rotation of the auxiliary frame, and the hydraulic ride by the brake pedal is characterized in that the flying play equipment characterized in that the rotation of the auxiliary frame is stopped by bringing the piston provided in close contact with the main frame.

The method of claim 5,

A hand brake is installed in the auxiliary frame to stop the rotation of the auxiliary frame, and the wire moved by the operation of the hand brake stops the rotation of the auxiliary frame by bringing a brake shoe provided on the outer side of the rotating member into close contact with the rotating member. Flying rides.

The method of claim 5,

The auxiliary frame is a flight ride, characterized in that made of a wire mesh to facilitate ventilation according to the rotation of the propeller.

The method of claim 5,

Flight rides characterized in that the seat belt is installed on the seat.

The method of claim 5,

A flight ride, characterized in that the radio transceiver is installed on the flight ride to wirelessly control the operation of the brake pedal, the pitch member and the rudder.

The method of claim 5,

The flight rides characterized in that the weight is further installed on the auxiliary frame in the front of the seat to have a weight corresponding to the propeller and the rudder provided on the back of the seat.

A seesaw section installed to rotate with the propeller;

A swash plate installed on the rotating shaft of the propeller, the swash plate being connected to each blade and the seesaw of the propeller so as to reciprocate in the longitudinal direction of the rotating shaft; And

The method of claim 11,

Further comprising a pitch member for changing the inclination of the blade angle of the propeller and the rotational surface of the propeller,

The pitch member includes a link portion provided to connect each blade and seesaw portion of the propeller with the swash plate, and a cylinder and a servo motor for reciprocating the swash plate or moving them to have an inclination in the front and rear directions. A flight ride, characterized in that the direction of the propulsive force of the propeller and the direction of the external force are changed by moving the swash plate by a predetermined distance using a motor to change the wing angle and the rotation surface.

The method according to claim 11 or 12, wherein

The method of claim 13,

Flight rides characterized in that the seat belt is installed on the seat.

The method of claim 13,

A flight ride, characterized in that the radio transceiver is installed on the flight ride to wirelessly control the operation of the brake pedal and the pitch member.

The method of claim 13,

The flight rides characterized in that the weight is further installed on the auxiliary frame in the front of the seat to have a weight corresponding to the propeller and the pitch member provided on the back of the seat.