Novel simulation flight rocker
By designing hydraulic damping components, rudder components and throttle rod components in simulated flight joysticks, the problem that existing simulated flight joysticks cannot simulate real flight damping, and improve the experience and realism of simulated flights.
Patent Information
- Application Number
- CN202421244988.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-06-03
- Publication Date
- 2025-04-22
- Estimated Expiration
- 2034-06-03
AI Technical Summary
Existing simulated flight rockers cannot simulate the torque and damping feeling in real flight, resulting in a poor sense of simulated flight experience.
A new simulated flight rocker was designed, using hydraulic damping components, rudder components and throttle rod components, through which damping forces are added between the rotating joints of the control rod to simulate the damping feeling in real flight.
It improves the experience of simulated flight, and users can feel the damping force in real flight, enhancing the authenticity and market versatility of simulated flight.
Smart Images
Figure CN222777603U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of flight rockers, in particular to a novel simulation flight rocker. Background Art
[0002] A simulated flight joystick is a control device used for simulated flight games or remote-controlled drone flight. It usually simulates the flight control stick in real flight and is used to control the attitude, direction and altitude of the aircraft. Flight simulators and remote-controlled drone first-person flight have become a popular entertainment and training tool, providing players with an experience close to real flight. It is also widely used in pilot training, aircraft design and testing and other fields.
[0003] A simulated flight joystick is a control device used for computer-based simulated flight games or remote control of unmanned aerial vehicles. Because the flight joystick is for remote control or simulated flight, the operator cannot feel the control feel with a certain torque and damping in real flight through the joystick, resulting in a poor simulated flight experience. At the same time, in the simulation of real flight, the torque and damping force transmitted to the joystick by the aircraft's control surface due to wind resistance cannot be truly felt by the user, which greatly reduces the simulated flight experience.
[0004] Therefore, it is urgent to provide a novel simulation flight rocker to solve the above problems. Utility Model Content
[0005] The technical problem to be solved by the utility model is to overcome the disadvantages of the above-mentioned prior art and provide a new type of simulated flight rocker.
[0006] In order to solve the above technical problems, a technical solution adopted by the utility model is: to provide a new type of simulated flight rocker, including a horizontal support rod, a first vertical support rod is fixedly connected to one end of the Y-axis at the top of the horizontal support rod, and a seat cushion is fixedly connected to the top of the first vertical support rod;
[0007] The horizontal support rod is fixedly connected with mesh plates on both sides of the X-axis, the middle end of the top of the horizontal support rod is fixedly connected with an operating rod bottom plate, the top of the operating rod bottom plate is installed with an operating rod base bracket, the top of the operating rod base bracket is movably connected with a universal joint bracket, the top of the operating rod base bracket is movably connected with a joystick body, and two damping components are installed on the top of the operating rod base bracket;
[0008] A foot rudder assembly is installed on the other end of the top Y-axis of the horizontal support rod, and a second vertical support rod is fixedly connected to one side of the X-axis of one of the mesh plates, and a throttle lever assembly is installed on the top of the second vertical support rod.
[0009] The utility model is further configured as follows: the damping assembly includes a damping cylinder body, a piston rod is fixedly connected to the output end of the damping cylinder body, a second fulcrum is fixedly connected to the outer wall of the damping cylinder body, and a third fulcrum is fixedly connected to the bottom of the damping cylinder body. One group of the second fulcrums of the damping assembly is rotatably connected to the universal joint bracket, and the third fulcrum is rotatably connected to the bottom plate of the operating rod, and another group of the second fulcrums of the damping assembly are rotatably connected to the operating rod body, and the third fulcrum is rotatably connected to the universal joint bracket through a connecting block. The operating rod base bracket includes a first fulcrum, and an eighth fulcrum is provided at the other end of the universal joint bracket Y-axis, and the first fulcrum is rotatably connected to the universal joint bracket.
[0010] Through the above technical solution, when in use, the control rod rotates in two axial directions, X and Y, and the hydraulic damping rods provide damping force in both X axial directions. The hydraulic damping rod is composed of a damping cylinder and a piston rod. The piston rod moves linearly along the cylinder. Joint bearings are arranged on the cylinder and the piston rod of the damping rod. The three fulcrums of the first fulcrum, the second fulcrum and the third fulcrum and another group of the second fulcrum, the third fulcrum and the eighth fulcrum respectively form a triangular geometric structure. When the X axis rotates, it rotates around the first fulcrum as the center. At this time, the distance between the second fulcrum and the third fulcrum changes, and a damping force is generated between the piston rod and the damping cylinder, so that a damping force is generated in the X-axis direction. When the Y axis rotates, it rotates around the eighth fulcrum as the center. At this time, the distance between the other group of the second fulcrum and the third fulcrum changes, so that a damping force is generated in the Y-axis direction.
[0011] The utility model is further configured as follows: the rudder foot assembly includes a rudder foot bottom plate fixedly connected to the other end of the Y-axis direction of the top of the horizontal support rod, the top of the rudder foot bottom plate is fixedly connected to a rudder foot base, fourth fulcrums are provided at both ends of the Y-axis direction of the rudder foot base, two first swing arms are rotatably connected inside the two fourth fulcrums, two fifth fulcrums are fixedly connected to the top of the rudder foot base, two fifth fulcrums are rotatably connected inside the two fifth fulcrums, two second swing arms are fixedly connected to the outer wall of the rotating shaft, two second swing arms are rotatably connected to the first connecting rods at both ends of the Y-axis direction of the two second swing arms, pedal rods are fixedly connected to both sides of the X-axis direction of the rotating shaft, a damping assembly is installed between the rudder foot base and the first swing arm, the second fulcrum is rotatably connected to the rudder foot base through a connecting shaft, and the third fulcrum is rotatably connected to the first swing arm.
[0012] Through the above technical solution, when in use, when the pedal rod is subjected to force, it drives the rotating shaft to make circular motion around the two fifth fulcrums, and the two second swing arms are placed on the rotating shaft. The rotational motion of the rotating shaft drives the two second swing arms to move up and down. The two second swing arms drive the first swing arm to move up and down through the first connecting rod. The other end of the first swing arm is connected to one of the third fulcrums. The fourth fulcrum, the third fulcrum and the second fulcrum form a triangular geometric shape. When the pedal rod is pushed forward and backward, the distance between the third fulcrum and the second fulcrum changes, and a damping force is generated between the damping cylinder and the piston rod, so that the rudder has a damping force, so that the user has a sufficient realistic feeling.
[0013] The utility model is further configured as follows: the throttle lever assembly includes a throttle lever base plate fixedly connected to the top of the second vertical support rod, the other end of the Y-axis of the top of the throttle lever base plate is fixedly connected to a throttle lever base bracket, a sixth fulcrum is provided inside the throttle lever base bracket, a third swing arm is rotatably connected inside the sixth fulcrum, the third swing arm is rotatably connected to the throttle lever body on one side of the X-axis, a seventh fulcrum is fixedly connected to one end of the Y-axis of the top of the throttle lever base plate, a fourth swing arm is rotatably connected to the outer wall of the seventh fulcrum, the fourth swing arm is rotatably connected to the second connecting rod on the other side of the X-axis, a damping assembly is installed on one side of the X-axis of the top of the throttle lever base plate, the seventh fulcrum is rotatably connected to the second fulcrum on one side of the X-axis, and the third fulcrum is rotatably connected to the throttle lever base plate inside.
[0014] Through the above technical solution, when in use, the throttle lever drives the third swing arm to make a circular motion around the sixth fulcrum after being subjected to force, and the third swing arm drives the third swing arm to make a circular motion around the seventh fulcrum through the second connecting rod. The other end of the third swing arm is connected to one of the third fulcrums of the piston rod, and one of the second fulcrums and the seventh fulcrum form a triangular geometric shape. When the throttle lever is pushed forward and backward, when the distance between the second fulcrum and the third fulcrum changes, a damping force is generated between the piston rod and the cylinder body, so that the throttle lever has a damping force.
[0015] The beneficial effects of the utility model are as follows:
[0016] 1. The utility model designs simple damping components, rudder pedal components and throttle lever components, so that users can use the flight joystick to add hydraulic damping rods between various rotating joints when using the flight joystick, thereby increasing the user's sense of real feel in simulated flight, thereby greatly improving the simulated flight experience.
[0017] 2. The utility model allows the user to perform manual operation through the damping component, so that the user has a real sense of operation damping, so that the simulated flight has a certain real feeling, and the simulated flight joystick can simulate the flight more realistically, thereby greatly improving the market versatility of the simulated flight joystick. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] Figure 1 It is a three-dimensional structural schematic diagram of the utility model;
[0019] Figure 2 This is a three-dimensional diagram of the operating lever assembly of the utility model from a first perspective;
[0020] Figure 3 This is a stereoscopic diagram of the operating lever assembly from a second viewing angle of the present utility model;
[0021] Figure 4 It is a three-dimensional diagram of the universal joint bracket of the utility model;
[0022] Figure 5 It is a three-dimensional diagram of the rudder foot assembly of the utility model;
[0023] Figure 6 It is a three-dimensional diagram of the throttle lever assembly of the utility model.
[0024] In the figure: 1, horizontal support rod; 2, first vertical support rod; 3, seat cushion; 4, mesh plate; 5, operating rod bottom plate; 6, operating rod base bracket; 601, first fulcrum; 602, eighth fulcrum; 7, universal joint bracket; 8, joystick body; 9, damping assembly; 901, damping cylinder; 902, piston rod; 903, second fulcrum; 904, third fulcrum; 10, rudder assembly; 1001, rudder bottom plate; 1002, rudder base; 1003, fourth fulcrum ; 1004, first swing arm; 1005, fifth fulcrum; 1006, rotating shaft; 1007, second swing arm; 1008, first connecting rod; 1009, pedal rod; 11, second vertical support rod; 12, throttle lever assembly; 1201, throttle lever base plate; 1202, throttle lever base bracket; 1203, sixth fulcrum; 1204, third swing arm; 1205, throttle lever body; 1206, seventh fulcrum; 1207, fourth swing arm; 1208, second connecting rod. DETAILED DESCRIPTION
[0025] The preferred embodiments of the present invention are described in detail below in conjunction with the accompanying drawings so that the advantages and features of the present invention can be more easily understood by those skilled in the art, thereby making a clearer and more definite definition of the protection scope of the present invention.
[0026] See also Figure 1-Figure 6A new type of simulated flight rocker includes a horizontal support rod 1, a first vertical support rod 2 is fixedly connected to one end of the Y-axis of the top of the horizontal support rod 1, a cushion 3 is fixedly connected to the top of the first vertical support rod 2, a mesh plate 4 is fixedly connected to both sides of the X-axis of the horizontal support rod 1, an operating rod bottom plate 5 is fixedly connected to the middle end of the top of the horizontal support rod 1, an operating rod base bracket 6 is installed on the top of the operating rod bottom plate 5, a universal joint bracket 7 is movably connected to the top of the operating rod base bracket 6, a joystick body 8 is movably connected to the top of the operating rod base bracket 6, and two A damping assembly 9, the damping assembly 9 includes a damping cylinder 901, the output end of the damping cylinder 901 is fixedly connected to a piston rod 902, the outer wall of the damping cylinder 901 is fixedly connected to a second fulcrum 903, and the bottom of the damping cylinder 901 is fixedly connected to a third fulcrum 904, wherein the second fulcrum 903 of one group of damping assemblies 9 is internally connected to the universal joint bracket 7 for rotation, and the third fulcrum 904 is connected to the operating rod base plate 5 for rotation, and the second fulcrum 903 of another group of damping assemblies 9 is internally connected to the operating rod body 8 for rotation, and the third fulcrum 904 is connected to the universal joint bracket 7 through a connecting block. The operating rod base bracket 6 includes a first fulcrum 601, and the other end of the universal joint bracket 7Y axis is provided with an eighth fulcrum 602. The first fulcrum 601 is internally connected to the universal joint bracket 7 for rotation. When in use, the operating rod has two axial rotations in XY. The two axial directions of X are provided with hydraulic damping rods to provide damping force. The hydraulic damping rod is composed of a damping cylinder 901 and a piston rod 902. The piston rod 902 moves linearly along the cylinder. The cylinder body and the piston rod 902 of the damping rod are provided with joint bearings. The first fulcrum 601, the second fulcrum 903 and the third fulcrum 904 are three fulcrums. The third fulcrum 904 and the eighth fulcrum 602 form a triangular geometric structure. When the x-axis rotates, the first fulcrum 601 is rotated around the first fulcrum 601. At this time, the distance between the second fulcrum 903 and the third fulcrum 904 changes, and a damping force is generated between the piston rod 902 and the damping cylinder 901, so that a damping force is generated in the x-axis direction. When the y-axis rotates, the eighth fulcrum 602 is rotated around the eighth fulcrum 602. At this time, the distance between the second fulcrum 903 and the third fulcrum 904 changes, so that a damping force is generated in the y-axis direction.
[0027] like Figure 5As shown, a rudder assembly 10 is installed at the other end of the top Y-axis of the horizontal support rod 1, and the rudder assembly 10 includes a rudder base plate 1001 fixedly connected to the other end of the top Y-axis of the horizontal support rod 1, a rudder base 1002 is fixedly connected to the top of the rudder base plate 1001, and fourth fulcrums 1003 are arranged at both ends of the Y-axis of the rudder base 1002, and the first swing arm 1004 is rotatably connected inside the two fourth fulcrums 1003, and two fifth fulcrums 1005 are fixedly connected to the top of the rudder base 1002, and the two fifth fulcrums 1005 are rotatably connected inside the two fifth fulcrums 1005, and two second swing arms 1007 are fixedly connected to the outer wall of the rotating shaft 1006, and the two second swing arms 1007 are rotatably connected to the first connecting rod 1008 at both ends of the Y-axis of the two second swing arms 1007, and pedal rods 1009 are fixedly connected on both sides of the X-axis of the rotating shaft 1006, and a damping assembly 9 is installed between the rudder base 1002 and the first swing arm 1004, and the second fulcrum 903 is connected inside by The connecting shaft is rotatably connected to the rudder base 1002, and the third fulcrum 904 is internally rotatably connected to the first swing arm 1004. When in use, when the pedal rod 1009 is subjected to force, it drives the rotating shaft 1006 to make a circular motion around the two fifth fulcrums 1005. The two second swing arms 1007 are placed on the rotating shaft 1006. The rotational motion of the rotating shaft 1006 drives the two second swing arms 1007 to move up and down. The two second swing arms 1007 drive the first swing arm 1004 to move up and down through the first connecting rod 1008. The other end of the first swing arm 1004 is connected to the third fulcrum 904. The fourth fulcrum 1003, the third fulcrum 904 and the second fulcrum 903 form a triangular geometric shape. When the pedal rod 1009 is pushed to move forward and backward, the distance between the third fulcrum 904 and the second fulcrum 903 changes, and a damping force is generated between the damping cylinder 901 and the piston rod 902, so that the rudder has a damping force, so that the user has a sufficient realistic feeling.
[0028] like Figure 6As shown, one of the mesh plates 4 is fixedly connected to the second vertical support rod 11 on one side of the X-axis, and a throttle rod assembly 12 is installed on the top of the second vertical support rod 11. The throttle rod assembly 12 includes a throttle rod bottom plate 1201 fixedly connected to the top of the second vertical support rod 11, and a throttle rod base bracket 1202 is fixedly connected to the other end of the top Y-axis of the throttle rod bottom plate 1201, and a sixth fulcrum 1203 is provided inside the throttle rod base bracket 1202, and the third swing arm 1204 is rotatably connected inside the sixth fulcrum 1203, and the third swing arm 1204 is rotatably connected to the throttle rod body 1205 on one side of the X-axis, and a seventh fulcrum 1206 is fixedly connected to one end of the top Y-axis of the throttle rod bottom plate 1201, and the outer wall of the seventh fulcrum 1206 is rotatably connected to the fourth swing arm 1207, and the fourth swing arm 1207 is rotatably connected to the second connecting rod 1208 on the other side of the X-axis. A damping assembly 9 is installed on one side of the X-axis of the top of the throttle lever base plate 1201, and one side of the X-axis of the seventh fulcrum 1206 is rotatably connected to the second fulcrum 903, and the inside of the third fulcrum 904 is rotatably connected to the throttle lever base plate 1201. When in use, the throttle lever drives the third swing arm 1204 to make a circular motion around the sixth fulcrum 1203 after being subjected to force, and the third swing arm 1204 drives the third swing arm 1204 to make a circular motion around the seventh fulcrum 1206 through the second connecting rod 1208. The other end of the third swing arm 1204 is connected to the third fulcrum 904 of the piston rod 902. The second fulcrum 903 and the seventh fulcrum 1206 form a triangular geometric shape. When the throttle lever is pushed forward and backward, when the distance between the second fulcrum 903 and the third fulcrum 904 changes, a damping force is generated between the piston rod 902 and the cylinder body, so that the throttle lever has a damping force.
[0029] When the utility model is in use, after the user sits on the cushion 3, the control lever rotates in two axes X and Y. The hydraulic damping rods in both axes X provide damping force. When the x-axis rotates, it rotates around the first fulcrum 601 as the center. At this time, the distance between the second fulcrum 903 and the third fulcrum 904 changes. When the y-axis rotates, it rotates around the eighth fulcrum 602 as the center. At this time, the distance between another set of second fulcrums 903 and the third fulcrum 904 changes to generate damping force in the y-axis direction. When the pedal rod 1009 is subjected to force, it drives the rotating shaft 1006. It makes circular motion around the two fifth fulcrums 1005, and the two second swing arms 1007 are placed on the rotating shaft 1006. The rotational motion of the rotating shaft 1006 drives the two second swing arms 1007 to make up and down motion. The two second swing arms 1007 drive the first swing arm 1004 to make up and down motion through the first connecting rod 1008. After the throttle lever is subjected to force, it drives the third swing arm 1204 to make circular motion around the sixth fulcrum 1203. The third swing arm 1204 drives the third swing arm 1204 to make circular motion around the seventh fulcrum 1206 through the second connecting rod 1208.
[0030] The above description is only an embodiment of the present invention, and does not limit the patent scope of the present invention. Any equivalent structure or equivalent process transformation made by using the contents of the specification and drawings of the present invention, or directly or indirectly applied in other related technical fields, are also included in the patent protection scope of the present invention.
Claims
1. A novel simulated flight rocker, comprising a horizontal support rod (1), characterized in that: A first vertical support rod (2) is fixedly connected to one end of the top Y-axis of the horizontal support rod (1), and a seat cushion (3) is fixedly connected to the top of the first vertical support rod (2); The horizontal support rod (1) is fixedly connected with mesh plates (4) on both sides of the X-axis, the middle end of the top of the horizontal support rod (1) is fixedly connected with an operating rod base plate (5), the top of the operating rod base plate (5) is installed with an operating rod base bracket (6), the top of the operating rod base bracket (6) is movably connected with a universal joint bracket (7), the top of the operating rod base bracket (6) is movably connected with a joystick body (8), and the top of the operating rod base bracket (6) is installed with two damping components (9); A rudder foot assembly (10) is mounted on the other end of the top of the horizontal support rod (1) in the Y-axis direction, and a second vertical support rod (11) is fixedly connected to one side of one of the mesh plates (4) in the X-axis direction, and a throttle lever assembly (12) is mounted on the top of the second vertical support rod (11).
2. A novel simulated flight rocker according to claim 1, characterized in that: The operating rod base bracket (6) comprises a first fulcrum (601), and an eighth fulcrum (602) is provided on the other end of the Y-axis of the universal joint bracket (7), and the first fulcrum (601) is internally rotatably connected to the universal joint bracket (7).
3. The novel simulated flight rocker according to claim 1, characterized in that: The damping assembly (9) comprises a damping cylinder (901), the output end of the damping cylinder (901) is fixedly connected to a piston rod (902), the outer wall of the damping cylinder (901) is fixedly connected to a second fulcrum (903), and the bottom of the damping cylinder (901) is fixedly connected to a third fulcrum (904).
4. A novel simulated flight rocker according to claim 3, characterized in that: The second fulcrum (903) of one group of the damping assemblies (9) is internally connected to the universal joint bracket (7) for rotation, and the third fulcrum (904) is connected to the operating rod base plate (5) for rotation; the second fulcrum (903) of another group of the damping assemblies (9) is internally connected to the operating rod body (8) for rotation, and the third fulcrum (904) is connected to the universal joint bracket (7) through a connecting block for rotation.
5. The novel simulated flight rocker according to claim 3, characterized in that: The rudder foot assembly (10) comprises a rudder foot base plate (1001) fixedly connected to the other end of the top of the horizontal support rod (1) in the Y-axis direction, the top of the rudder foot base plate (1001) is fixedly connected to a rudder foot base (1002), the rudder foot base (1002) is provided with fourth fulcrums (1003) at both ends in the Y-axis direction, the two fourth fulcrums (1003) are both rotatably connected to the first swing arm (1004), the top of the rudder foot base (1002) is fixedly connected to two fifth fulcrums (1003), and the first swing arm (1004) is rotatably connected to the first swing arm (1004). 05), the two fifth fulcrums (1005) are both rotatably connected with a rotating shaft (1006) inside, the outer wall of the rotating shaft (1006) is fixedly connected with two second swing arms (1007), the two second swing arms (1007) are rotatably connected with a first connecting rod (1008) at both ends of the Y axis, the rotating shaft (1006) is fixedly connected with a pedal rod (1009) at both sides of the X axis, and a damping component (9) is installed between the rudder base (1002) and the first swing arm (1004).
6. A novel simulated flight rocker according to claim 5, characterized in that: The second fulcrum (903) is rotatably connected to the rudder base (1002) via a connecting shaft, and the third fulcrum (904) is rotatably connected to the first swing arm (1004).
7. The novel simulated flight rocker according to claim 3, characterized in that: The throttle lever assembly (12) comprises a throttle lever base plate (1201) fixedly connected to the top of the second vertical support rod (11); a throttle lever base bracket (1202) is fixedly connected to the other end of the top Y-axis of the throttle lever base plate (1201); a sixth fulcrum (1203) is provided inside the throttle lever base bracket (1202); a third swing arm (1204) is rotatably connected inside the sixth fulcrum (1203); the third swing arm (1204) is rotatably connected to the inside of the throttle lever base bracket (1202); 4) A throttle lever body (1205) is rotatably connected to one side of the X-axis, a seventh fulcrum (1206) is fixedly connected to one end of the top Y-axis of the throttle lever base plate (1201), a fourth swing arm (1207) is rotatably connected to the outer wall of the seventh fulcrum (1206), the fourth swing arm (1207) is rotatably connected to the other side of the X-axis with a second connecting rod (1208), and a damping assembly (9) is installed on one side of the top X-axis of the throttle lever base plate (1201).
8. The novel simulated flight rocker according to claim 7, characterized in that: The seventh fulcrum (1206) is rotatably connected to the second fulcrum (903) on one side of the X-axis, and the third fulcrum (904) is rotatably connected to the throttle lever base plate (1201) inside.