Simulation flight simulator cabin
By using multiple electric cylinder support structures and flexible covering layers in the flight simulator cockpit, the roof can be changed at multiple angles, solving the problem of insufficient degrees of freedom in existing simulators and improving the realism of the flight experience.
Patent Information
- Application Number
- CN202520538183.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-03-26
- Publication Date
- 2026-02-27
- Estimated Expiration
- 2035-03-26
AI Technical Summary
Existing flight simulators have limited simulation support platforms, making it difficult to effectively simulate turbulence and weightlessness during flight.
The cockpit uses a flight simulator and is supported between a fixed plate and a top plate by a first, second, third, fourth, fifth, and sixth electric cylinder, which allows for multi-angle changes in the top plate. Combined with a flexible covering layer and a flight simulation control system, it simulates a more realistic flight experience.
It increases the freedom of flight simulators, enhances the simulation of turbulence and weightlessness during flight, and improves the realism and effectiveness of training.
Smart Images
Figure CN223956185U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to flight simulator field, especially involves simulation flight simulator cockpit. BACKGROUND
[0002] Flight simulator, from the broad sense, is the device that is used to simulate the flight of aircraft, missile, satellite, spaceship and other flights, can be called flight simulator. It is the simulation device that can reproduce the aircraft and the aerial environment and can operate. From the narrow sense, it is the device that is used to simulate the flight of aircraft and has relatively complex structure and relatively complete function. In the flight simulator, the important one is whether the jolt and weightlessness in the flight process can be simulated through the transformation of multiple degrees of freedom,
[0003] Flight simulator adopts real-time simulation technology to reproduce the cockpit and the aerial flight environment on the ground, is used to carry out the initial, modification, retraining of take-off, climbing, turning, landing, maneuvering and other of the pilot, is not limited by the weather condition and the site, makes the flight personnel familiar with the driving technology of the machine type in the relatively short time, so the feeling of simulating jolt is very important, the freedom degree of simulation support platform in the prior art is not high, needs optimization improvement. CONTENT OF UTILITY MODEL
[0004] The utility model aims at providing simulation flight simulator cockpit to solve the above-mentioned prior art problem.
[0005] The above technical purpose of the utility model is realized through the following technical scheme:
[0006] The cockpit of the simulation flight simulator comprises a base and a cockpit fixedly installed on the top of the base, the base comprises a fixed plate, a first mounting plate, a second mounting plate, a third mounting plate and a top plate, the first mounting plate, the second mounting plate and the third mounting plate are in a triangular shape and arranged on the top of the fixed plate, the top of the first mounting plate is provided with a first rotating shaft and a second rotating shaft arranged vertically and spaced apart, the top of the second mounting plate is provided with a third rotating shaft and a fourth rotating shaft arranged vertically and spaced apart, the top of the third mounting plate is provided with a fifth rotating shaft and a sixth rotating shaft arranged vertically and spaced apart, one end of the first electric cylinder is hingedly connected to the top end of the first rotating shaft, one end of the second electric cylinder is hingedly connected to the top end of the second rotating shaft, one end of the third electric cylinder is hingedly connected to the top end of the third rotating shaft, one end of the fourth electric cylinder is hingedly connected to the top end of the fourth rotating shaft, one end of the fifth electric cylinder is hingedly connected to the top end of the fifth rotating shaft, and one end of the sixth electric cylinder is hingedly connected to the top end of the sixth rotating shaft, the other end of the first electric cylinder, the second electric cylinder, the third electric cylinder, the fourth electric cylinder, the fifth electric cylinder and the sixth electric cylinder are hingedly connected to the bottom of the bottom plate, the connecting points of the first electric cylinder, the second electric cylinder, the third electric cylinder, the fourth electric cylinder, the fifth electric cylinder and the sixth electric cylinder and the bottom of the top plate are arranged in sequence in the circumferential direction, and the cockpit is fixedly installed on the top of the top plate.
[0007] By adopting the above technical scheme, the first electric cylinder, the second electric cylinder, the third electric cylinder, the fourth electric cylinder, the fifth electric cylinder and the sixth electric cylinder are supported between the fixed plate and the top plate, and the free extension of the first electric cylinder, the second electric cylinder, the third electric cylinder, the fourth electric cylinder, the fifth electric cylinder and the sixth electric cylinder can realize the angle change of the top plate, so that better simulation effect is achieved.
[0008] In further embodiments, one end of the first electric cylinder, the second electric cylinder, the third electric cylinder, the fourth electric cylinder, the fifth electric cylinder and the sixth electric cylinder connected to the top plate is hingedly connected to a round rod, the other end of the round rod is rotatably installed on the bottom of the top plate, and the axis of the round rod is vertically arranged.
[0009] In further embodiments, the periphery of the fixed plate is provided with a cover, and one side of the cover is provided with a step.
[0010] By adopting the above technical scheme, it is convenient for the user to enter the cockpit through the step.
[0011] In further embodiments, a flight simulation control system is arranged in the cockpit, a control cabinet is arranged at the center of the top of the fixed plate, the control cabinet is connected to the flight simulation control system through a wire harness, and the control cabinet is used to control the extension of the first electric cylinder, the second electric cylinder, the third electric cylinder, the fourth electric cylinder, the fifth electric cylinder and the sixth electric cylinder through the data of the flight simulation control system.
[0012] In a further embodiment, a plurality of handles are provided on one side of the cockpit.
[0013] In a further embodiment, the interior of the cabin is provided with a flexible covering layer.
[0014] In summary, this utility model has the following beneficial effects:
[0015] 1. Supported between the fixed plate and the top plate by the first, second, third, fourth, fifth, and sixth electric cylinders, the top plate can be adjusted to multiple angles by the free extension and retraction of the first, second, third, fourth, fifth, and sixth electric cylinders, thus achieving a better simulation effect. Attached Figure Description
[0016] Figure 1 This is a schematic diagram of the overall structure of this utility model;
[0017] Figure 2 This is a structural schematic diagram of the base used to illustrate this utility model.
[0018] In the diagram, 1 is the base; 11 is the fixing plate; 12 is the first mounting plate; 13 is the second mounting plate; 14 is the third mounting plate; 15 is the top plate; 2 is the cockpit; 3 is the first rotating shaft; 31 is the first electric cylinder; 4 is the second rotating shaft; 41 is the second electric cylinder; 5 is the third rotating shaft; 51 is the third electric cylinder; 6 is the fourth rotating shaft; 61 is the fourth electric cylinder; 7 is the fifth rotating shaft; 71 is the fifth electric cylinder; 8 is the sixth rotating shaft; 81 is the sixth electric cylinder. Detailed Implementation
[0019] The present invention will be further described in detail below with reference to the accompanying drawings.
[0020] Identical parts are indicated by the same reference numerals. It should be noted that the terms "front," "rear," "left," "right," "upper," and "lower" used in the following description refer to the attached figures. Figure 1 In this specification, the terms "bottom surface" and "top surface," "inner" and "outer" refer to the direction toward or away from the geometry of a specific component. Furthermore, the terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of this specification, "a plurality of" means two or more, unless otherwise explicitly and specifically defined by the direction of the center.
[0021] Example 1:
[0022] like Figures 1-2As shown, the flight simulator cockpit, including the base 1 and the cockpit 2, the cockpit 2 is fixedly installed on the top of the base 1, the base 1 includes a fixed plate 11, a first mounting plate 12, a second mounting plate 13, a third mounting plate 14 and a top plate 15, the first mounting plate 12, the second mounting plate 13 and the third mounting plate 14 are distributed in the shape of a triangle on the top of the fixed plate 11, the top of the first mounting plate 12 is provided with a first rotating shaft 3 and a second rotating shaft 4 installed vertically, the top of the second mounting plate 13 is provided with a third rotating shaft 5 and a fourth rotating shaft 6 installed vertically, the top of the third mounting plate 14 is provided with a fifth rotating shaft 7 and a sixth rotating shaft 8 installed vertically, one end of the first electric cylinder 31 is hingedly connected to the top end of the first rotating shaft 3, one end of the second electric cylinder 41 is hingedly connected to the top end of the second rotating shaft 4, one end of the third electric cylinder 51 is hingedly connected to the top end of the third rotating shaft 5, one end of the fourth electric cylinder 61 is hingedly connected to the top end of the fourth rotating shaft 6, one end of the fifth electric cylinder 71 is hingedly connected to the top end of the fifth rotating shaft 7, and one end of the sixth electric cylinder 81 is hingedly connected to the top end of the sixth rotating shaft 8, the other end of the first electric cylinder 31, the second electric cylinder 41, the third electric cylinder 51, the fourth electric cylinder 61, the fifth electric cylinder 71 and the sixth electric cylinder 81 are hingedly installed on the bottom of the bottom plate, and the connection points of the first electric cylinder 31, the second electric cylinder 41, the third electric cylinder 51, the fourth electric cylinder 61, the fifth electric cylinder 71 and the sixth electric cylinder 81 and the top plate 15 are arranged in sequence around the top plate 15, the cockpit 2 is fixedly installed on the top of the top plate 15, the periphery of the fixed plate 11 is provided with a cover, one side of the cover is provided with a step, the cockpit 2 is provided with a flight simulation control system, a control cabinet is arranged at the center of the top of the fixed plate 11, the control cabinet is connected to the flight simulation control system through a wire harness, and the control cabinet is used for controlling the extension and contraction of the first electric cylinder 31, the second electric cylinder 41, the third electric cylinder 51, the fourth electric cylinder 61, the fifth electric cylinder 71 and the sixth electric cylinder 81 through the data of the flight simulation control system, one side of the cockpit 2 is provided with a plurality of handles, and the inside of the cockpit 2 is provided with a flexible cladding layer.
[0023] Specific implementation process: the first electric cylinder, the second electric cylinder, the third electric cylinder, the fourth electric cylinder, the fifth electric cylinder and the sixth electric cylinder are all linear drive electric cylinders, the first electric cylinder, the second electric cylinder, the third electric cylinder, the fourth electric cylinder, the fifth electric cylinder and the sixth electric cylinder are supported between the fixed plate and the top plate, and the free extension of the first electric cylinder, the second electric cylinder, the third electric cylinder, the fourth electric cylinder, the fifth electric cylinder and the sixth electric cylinder can realize the change of multiple angles of the top plate, so that better simulation effect is achieved.
[0024] Embodiment 2:
[0025] The first electric cylinder 31, the second electric cylinder 41, the third electric cylinder 51, the fourth electric cylinder 61, the fifth electric cylinder 71 and the sixth electric cylinder 81 are hingedly connected with one end of the top plate 15, and the other end of the round rod is rotatably installed at the bottom of the top plate 15, and the axis of the round rod is vertically arranged.
[0026] In the embodiments disclosed in the present application, the terms "mounting", "connecting", "connecting", "fixing" and the like should be understood in a broad sense. For example, "connecting" can be fixed connection, detachable connection or integral connection; "connecting" can be direct connection or indirect connection through an intermediate medium. For those skilled in the art, the specific meanings of the above terms in the embodiments disclosed in the present application can be understood according to the specific circumstances.
[0027] The specific embodiments are merely an explanation of the present application, and are not a limitation of the present application. Those skilled in the art can make modifications to the embodiments without creative contribution after reading the present application, as long as the modifications are within the scope of the claims of the present application.
Claims
1. A flight simulator cockpit, characterized in that: The utility model provides a flight simulator, including base (1) and cockpit (2), cockpit (2) is fixedly installed on the top of base (1), base (1) includes fixed plate (11), first mounting plate (12), second mounting plate (13), third mounting plate (14) and top plate (15), first mounting plate (12), second mounting plate (13), third mounting plate (14) are in the shape of a triangle and are distributed on the top of fixed plate (11), the top of first mounting plate (12) is provided with the vertical installation first rotating shaft (3), second rotating shaft (4) at interval, the top of second mounting plate (13) is provided with the vertical installation third rotating shaft (5), fourth rotating shaft (6) at interval, the top of third mounting plate (14) is provided with the vertical installation fifth rotating shaft (7), sixth rotating shaft (8) at interval, the top of first rotating shaft (3) is hingedly connected with one end of first electric cylinder (31), the top of second rotating shaft (4) is hingedly connected with one end of second electric cylinder (41), the top of third rotating shaft (5) is hingedly connected with one end of third electric cylinder (51), the top of fourth rotating shaft (6) is hingedly connected with one end of fourth electric cylinder (61), the top of fifth rotating shaft (7) is hingedly connected with one end of fifth electric cylinder (71), the top of sixth rotating shaft (8) is hingedly connected with one end of sixth electric cylinder (81), the end of first electric cylinder (31), second electric cylinder (41), third electric cylinder (51), fourth electric cylinder (61), fifth electric cylinder (71), sixth electric cylinder (81) is not connected with first rotating shaft (3), second rotating shaft (4), third rotating shaft (5), fourth rotating shaft (6), fifth rotating shaft (7), sixth rotating shaft (8) is hingedly installed on the bottom of bottom plate, and the connecting point of first electric cylinder (31), second electric cylinder (41), third electric cylinder (51), fourth electric cylinder (61), fifth electric cylinder (71), sixth electric cylinder (81) and top plate (15) bottom is sequentially arranged circumferentially, cockpit (2) is fixedly installed on the top of top plate (15).
2. The flight simulator cockpit according to claim 1, characterized in that: The end of first electric cylinder (31), second electric cylinder (41), third electric cylinder (51), fourth electric cylinder (61), fifth electric cylinder (71), sixth electric cylinder (81) and top plate (15) is hingedly connected with round bar, the other end of round bar is rotatably installed on the bottom of top plate (15), and the axis of round bar is vertically arranged.
3. The flight simulator cockpit of claim 1, wherein: The periphery of fixed plate (11) is provided with a shell, and one side of the shell is provided with a step.
4. The flight simulator cockpit of claim 1, wherein: A flight simulation control system is arranged in the cockpit (2), a control cabinet is arranged at the top center of the fixed plate (11), the control cabinet is connected with the flight simulation control system through a wire harness, and the control cabinet is used for controlling the extension and retraction of the first electric cylinder (31), the second electric cylinder (41), the third electric cylinder (51), the fourth electric cylinder (61), the fifth electric cylinder (71) and the sixth electric cylinder (81) through the data of the flight simulation control system.
5. The flight simulator cockpit of claim 1, wherein: A plurality of handles are arranged on one side of the cockpit (2).
6. The flight simulator cockpit of claim 1, wherein: A flexible cladding layer is arranged in the cockpit (2).