Adjustable cockpit of VR spacecraft

Abstract

The utility model discloses a VR spacecraft adjustable cockpit which comprises a VR spacecraft, and a cockpit base is arranged in the VR spacecraft. The inner wall of the VR spacecraft is fixedly connected with a first L-shaped frame, the top of the cockpit seat is fixedly connected with a second L-shaped frame, the top of the second L-shaped frame is fixedly connected with a cylinder, the cylinder penetrates through the first L-shaped frame, and the outer wall of the cylinder is rotationally installed in the first L-shaped frame through a bearing. When a second L-shaped frame rotates, a connecting cylinder can control a travel switch to change the travel in an arc-shaped groove, so that a first electric push rod is controlled to drive a fixing pipe and a U-shaped surrounding rod to swing upwards, the U-shaped surrounding rod is made to be attached to the chest of the human body, and the stability of the human body taking the VR spacecraft is further improved; the U-shaped surrounding rod can be put down to reduce the constraint feeling of the upper body of the user, and the safety is improved while the immersion feeling is enhanced.

Description

Technical Field

[0001] The utility model relates to the technical field of VR aerospace simulators, in particular to an adjustable cockpit of a VR spacecraft. Background Art

[0002] A VR spacecraft is a simulated spaceship simulator, which looks similar to a real spacecraft or spacecraft, and has a cockpit inside. After wearing a VR headset, users can enter a realistic space environment and drive the spacecraft to perform various tasks. Through VR virtual reality technology, users can operate in a simulated space environment and feel the reality of complex tasks such as space station docking and satellite deployment. It is widely used in education and entertainment, allowing more people to experience space exploration.

[0003] However, in existing VR spacecraft, when the human body support and restraint mechanism on the cockpit seat is set to a fixed state, the user's upper body movement space in the virtual reality environment is easily limited, and the elastic human body support and restraint mechanism is easy to cause the user's body to suddenly tilt or get injured due to sudden movement or posture changes in the VR spacecraft, thereby affecting the user experience and the safety is insufficient. Utility Model Content

[0004] The utility model aims to solve at least one of the technical problems existing in the prior art.

[0005] To this end, one purpose of the utility model is to propose an adjustable cockpit for a VR spacecraft, which can provide upper body support for the human body through a U-shaped surround. When the second L-shaped frame rotates, the electric push rod can drive the U-shaped surround to fit the chest, thereby enhancing the stability and safety of the VR spacecraft and reducing the sense of restraint when there is no rotation.

[0006] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an adjustable cockpit of a VR spacecraft, comprising a VR spacecraft, wherein a cockpit seat is arranged inside the VR spacecraft; a first L-shaped frame is fixedly connected to the inner wall of the VR spacecraft, a second L-shaped frame is fixedly connected to the top of the cockpit seat, a cylinder is fixedly connected to the top of the second L-shaped frame, the cylinder passes through the first L-shaped frame, and the outer wall of the cylinder is rotatably mounted inside the first L-shaped frame through a bearing, two fixed tubes are symmetrically hinged on both sides of the cockpit seat, a U-shaped surrounding rod is slidably mounted inside the fixed tube, a first electric push rod is mounted on both sides of the cockpit seat, a piston rod of the first electric push rod is hinged to the outer wall of the fixed tube, an arc groove is arranged on the top of the second L-shaped frame, a slidable travel switch is mounted inside the arc groove, a connecting tube is mounted at the bottom of the first L-shaped frame, and one end of the top of the travel switch is clamped inside the connecting tube.

[0007] Preferably, a gear ring is installed on the top of the cylinder, a motor is installed on the top of the first L-shaped frame, the rotating shaft of the motor is meshed with the gear ring through a gear, and the travel switch is connected to the electrical control end of the motor.

[0008] Preferably, a touch-control integrated machine is installed inside the VR spacecraft, and the touch-control integrated machine has a built-in single-chip microcomputer.

[0009] Preferably, four connecting rods are symmetrically hinged at the bottom of the cockpit seat, and the ends of the four connecting rods are hinged to the soles of the feet, wherein a plate body is installed on one side of two of the connecting rods, and a second electric push rod is installed at the bottom of the cockpit seat, and a piston rod of the second electric push rod is hinged to one side of the plate body.

[0010] Preferably, a limit shell is installed on the bottom inner wall of the VR spacecraft.

[0011] Preferably, armrest pads are installed on both sides of the cockpit seat.

[0012] Compared with the prior art, the beneficial effects of the utility model are as follows: in the utility model, the U-shaped fence on the cockpit seat provides support and stability for the upper body of the human body, and when the second L-shaped frame rotates, the connecting tube can control the travel switch to change the travel in the arc groove, thereby controlling the first electric push rod to drive the fixed tube and the U-shaped fence to swing upward, so that the U-shaped fence fits the human chest, further improving the stability of the human body when riding in a VR spacecraft, and when the cockpit seat does not rotate, the U-shaped fence can be lowered to reduce the user's upper body restraint feeling, enhancing the immersion while improving safety. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 This is a structural schematic diagram of an adjustable cockpit of a VR spacecraft according to an embodiment of the utility model;

[0014] Figure 2 This is a structural schematic diagram of a cockpit seat in an adjustable cockpit of a VR spacecraft according to an embodiment of the utility model;

[0015] Figure 3 It is a partial cross-sectional structural diagram of a first L-shaped frame and a second L-shaped frame in an adjustable cockpit of a VR spacecraft according to an embodiment of the utility model;

[0016] Figure 4 It is a schematic structural diagram of the second L-shaped frame in the adjustable cockpit of a VR spacecraft according to an embodiment of the utility model.

[0017] In the figure: 1. VR spacecraft; 2. first L-shaped frame; 3. second L-shaped frame; 4. first electric push rod; 5. fixing tube; 6. cockpit seat; 7. U-shaped fence; 8. touch screen integrated machine; 9. connecting rod; 10. foot plate; 11. motor; 12. gear ring; 13. limit shell; 14. cylinder; 15. second electric push rod; 16. armrest pad; 17. arc groove; 18. travel switch; 19. connecting cylinder. DETAILED DESCRIPTION

[0018] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0019] See also Figure 1-Figure 2 An embodiment of the utility model provides an adjustable cockpit of a VR spacecraft, including: a VR spacecraft 1 and a cockpit seat 6.

[0020] Among them, Figure 1-Figure 3 As shown, the cockpit seat 6 is arranged inside the VR spacecraft 1, the inner wall of the VR spacecraft 1 is fixedly connected with the first L-shaped frame 2, the top of the cockpit seat 6 is fixedly connected with the second L-shaped frame 3, the top of the second L-shaped frame 3 is fixedly connected with the cylinder 14, the cylinder 14 passes through the first L-shaped frame 2, and the outer wall of the cylinder 14 is rotatably installed inside the first L-shaped frame 2 through a bearing, two fixed tubes 5 are symmetrically hinged on both sides of the cockpit seat 6, and a U-shaped enclosure rod 7 is slidably installed inside the fixed tube 5.

[0021] Furthermore, a gear ring 12 is installed on the top of the cylinder 14, and a motor 11 is installed on the top of the first L-shaped frame 2. The rotating shaft of the motor 11 is meshed with the gear ring 12 through a gear, and the travel switch 18 is connected to the electric control end of the motor 11. After the cylinder 14 passes through the first L-shaped frame 2 and is installed inside the first L-shaped frame 2 by a bearing, the second L-shaped frame 3 can rotate at the bottom of the first L-shaped frame 2, and at the same time, the first L-shaped frame 2 is prevented from rotating when the cylinder 14 rotates. By starting the motor 11, the gear ring 12 and the cylinder 14 can be driven to rotate, so that the second L-shaped frame 3 and the cockpit seat 6 can rotate, simulating the change of the seat direction. The U-shaped fence 7 on the cockpit seat 6 can provide additional support and stability for the upper body of the human body.

[0022] In this embodiment, Figure 1-Figure 4As shown, a first electric push rod 4 is installed on both sides of the cockpit seat 6, and the piston rod of the first electric push rod 4 is hinged to the outer wall of the fixed tube 5. An arc groove 17 is provided on the top of the second L-shaped frame 3, and a slidable travel switch 18 is installed inside the arc groove 17. A connecting tube 19 is installed at the bottom of the first L-shaped frame 2, and one end of the top of the travel switch 18 is clamped in the inside of the connecting tube 19.

[0023] When in use, by starting the first electric push rod 4, the two fixed tubes 5 can be driven to swing up and down to adjust their positions. In particular, when the second L-shaped frame 3 rotates to simulate the change in the direction of the seat, the travel switch 18 can be controlled by the connecting tube 19 to change the travel in the arc groove 17. When the travel changes, the first electric push rod 4 can be switched to drive the fixed tube 5 and the U-shaped surrounding rod 7 to swing upward, so that the U-shaped surrounding rod 7 can fit against the human chest.

[0024] like Figure 2 As shown, four connecting rods 9 are symmetrically hinged at the bottom of the cockpit seat 6, and footboards 10 are hinged at the ends of the four connecting rods 9, wherein a plate body 20 is installed on one side of two of the connecting rods 9, and a second electric push rod 15 is installed at the bottom of the cockpit seat 6, and the piston rod of the second electric push rod 15 is hinged to one side of the plate body 20. When the user sits in the cockpit seat 6, the feet can be placed on the top of the footboard 10, and the second electric push rod 15 can change the position of the footboard 10 to improve the comfort of the user's foot placement. In addition, armrest pads 16 are installed on both sides of the cockpit seat 6, so that the user's hands and limbs can be placed on the armrest pads 16.

[0025] Further, see Figure 1 A touch-control integrated machine 8 is installed inside the VR spacecraft 1. The touch-control integrated machine 8 has a built-in single-chip microcomputer. The single-chip microcomputer in the touch-control integrated machine 8 is electrically connected to the first electric push rod 4, the second electric push rod 15 and the motor 11 to realize electronic control operation.

[0026] Specifically, a limit shell 13 is installed on the bottom inner wall of the VR spacecraft 1. The limit shell 13 is located at the bottom of one side of the cockpit seat 6, and limits the rotatable angle and position of the cockpit seat 6. In addition.

[0027] According to the above technical scheme, the working steps of this scheme are summarized and sorted out: in the utility model, the top of the cockpit seat 6 is connected to the second L-shaped frame 3, and a cylinder 14 is fixed on the top of the second L-shaped frame 3. The cylinder 14 passes through the first L-shaped frame 2 and is installed inside the first L-shaped frame 2 using a bearing, so that the second L-shaped frame 3 can rotate at the bottom of the first L-shaped frame 2, and at the same time avoids the first L-shaped frame 2 from rotating when the cylinder 14 rotates. The U-shaped surrounding rod 7 on the cockpit seat 6 can provide additional support and stability for the upper body of the human body.

[0028] By starting the first electric push rod 4, the two fixed tubes 5 can be driven to swing up and down to adjust their positions. In particular, when the second L-shaped frame 3 rotates to simulate the change in the direction of the seat, the travel switch 18 can be controlled by the connecting tube 19 to change the travel in the arc groove 17. When the travel changes, the first electric push rod 4 can be switched to drive the fixed tube 5 and the U-shaped surrounding rod 7 to swing upward, so that the U-shaped surrounding rod 7 can be pressed against the human chest, further improving the stability of the human body when riding the VR spacecraft 1, enhancing the sense of immersion and improving safety.

[0029] Parts not involved in the present invention are the same as the prior art or can be implemented by the prior art. Although the embodiments of the present invention have been shown and described, it is understood by those skilled in the art that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of the present invention, and the scope of the present invention is defined by the attached claims and their equivalents.

Claims

1. An adjustable cockpit of a VR spacecraft, comprising a VR spacecraft (1), wherein a cockpit seat (6) is provided inside the VR spacecraft (1), and characterized in that: The inner wall of the VR spacecraft (1) is fixedly connected to a first L-shaped frame (2), the top of the cockpit seat (6) is fixedly connected to a second L-shaped frame (3), the top of the second L-shaped frame (3) is fixedly connected to a cylinder (14), the cylinder (14) passes through the first L-shaped frame (2), and the outer wall of the cylinder (14) is rotatably mounted inside the first L-shaped frame (2) through a bearing, and two fixed tubes (5) are symmetrically hinged on both sides of the cockpit seat (6), and the interior of the fixed tube (5) is slidable. A U-shaped guard bar (7) is installed, and first electric push rods (4) are installed on both sides of the cockpit seat (6), and the piston rod of the first electric push rod (4) is hinged to the outer wall of the fixed tube (5). The top of the second L-shaped frame (3) is provided with an arc groove (17), and a slidable travel switch (18) is installed inside the arc groove (17). A connecting tube (19) is installed at the bottom of the first L-shaped frame (2), and one end of the top of the travel switch (18) is clamped in the inside of the connecting tube (19).

2. The VR spacecraft adjustable cockpit according to claim 1, characterized in that: A gear ring (12) is installed on the top of the cylinder (14), a motor (11) is installed on the top of the first L-shaped frame (2), a rotating shaft of the motor (11) is meshed with the gear ring (12) via a gear, and the travel switch (18) is connected to the electrical control end of the motor (11).

3. The VR spacecraft adjustable cockpit according to claim 1, characterized in that: A touch-control integrated machine (8) is installed inside the VR spacecraft (1), and the touch-control integrated machine (8) has a built-in single-chip microcomputer.

4. The VR spacecraft adjustable cockpit according to claim 1, characterized in that: The bottom of the cockpit seat (6) is symmetrically hinged with four connecting rods (9), the ends of the four connecting rods (9) are hinged with foot plates (10), one side of two of the connecting rods (9) is installed with a plate body (20), and the bottom of the cockpit seat (6) is installed with a second electric push rod (15), and the piston rod of the second electric push rod (15) is hinged to one side of the plate body (20).

5. The VR spacecraft adjustable cockpit according to claim 1, characterized in that: A limit shell (13) is installed on the bottom inner wall of the VR spacecraft (1).

6. The VR spacecraft adjustable cockpit according to claim 1, characterized in that: Armrest pads (16) are installed on both sides of the cockpit seat (6).

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