CN215770140U - General fixed wing aircraft simulation flight equipment - Google Patents

General fixed wing aircraft simulation flight equipment Download PDF

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Publication number
CN215770140U
CN215770140U CN202122062232.8U CN202122062232U CN215770140U CN 215770140 U CN215770140 U CN 215770140U CN 202122062232 U CN202122062232 U CN 202122062232U CN 215770140 U CN215770140 U CN 215770140U
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CN
China
Prior art keywords
face
top end
seat
rod
bottom plate
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Expired - Fee Related
Application number
CN202122062232.8U
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Chinese (zh)
Inventor
苏彬
陈又军
黄欢
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Civil Aviation Flight University of China
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Civil Aviation Flight University of China
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Application filed by Civil Aviation Flight University of China filed Critical Civil Aviation Flight University of China
Priority to CN202122062232.8U priority Critical patent/CN215770140U/en
Application granted granted Critical
Publication of CN215770140U publication Critical patent/CN215770140U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a general fixed-wing aircraft simulated flight device which comprises a bottom plate, a simulated display screen, an operating platform, a button, a control rod, a pedal, an adjusting component, a base, a shaking component and a seat, wherein the simulated display screen is fixedly arranged at one end of the top end surface of the bottom plate, the operating platform is fixedly arranged outside one side of the simulated display screen, the button is fixedly arranged at one side of the top end surface of the operating platform, and the control rod is welded and arranged in the center of the top end surface of the bottom plate; the general fixed-wing aircraft simulated flight equipment is simple to operate and good in using effect; the adjusting component has the advantages that the adjusting component plays a role in adjusting the equipment seat, the seat is adjusted front and back and up and down, so that the equipment is suitable for more people, the compatibility of the equipment is improved, the usability of the equipment is guaranteed, the seat can be fixed by inserting the limiting rod into the limiting hole, the seat is prevented from moving in the experience process, and the experience feeling of an experience person is influenced.

Description

General fixed wing aircraft simulation flight equipment
Technical Field
The utility model relates to the technical field of simulated flight equipment, in particular to simulated flight equipment of a general fixed-wing aircraft.
Background
Flight simulation is a system that reproduces or simulates the driving feel of an aircraft as realistically as possible. Flight simulators range from electronic games to proportional simulated flight decks driven by hydraulic or electric motors and controlled by state-of-the-art computer technology. Flight simulators have been widely used in design and development by the aviation industry, as well as for pilot and crew training of civil and military aircraft.
In the prior art, the general fixed-wing aircraft simulated flight equipment has a small adjustable range for a seat in the use process, so that the equipment is not suitable for many people to use, and the usability of the equipment is influenced; the experience effect that equipment brought is not enough, can not let experience person have experience of being personally on the scene, therefore, it is very necessary to design a general fixed wing aircraft simulation flight equipment.
SUMMERY OF THE UTILITY MODEL
The utility model solves the problem of providing the general fixed-wing aircraft flight simulation equipment which is simple to operate and good in use effect; the adjusting assembly arranged on the equipment can effectively adjust the position of the seat, so that the seat is convenient for better people to use, and the using effect of the equipment is improved; the shaking assembly installed on the equipment can effectively bring flying experience to an experiencer, so that the simulated flight is more real.
In order to achieve the purpose, the utility model adopts the following technical scheme:
a general fixed-wing aircraft simulated flight device comprises a bottom plate, a simulated display screen, an operating platform, a button, a control rod, a pedal, an adjusting component, a base, a shaking component and a seat, wherein the simulated display screen is fixedly installed at one end of the top end face of the bottom plate, the operating platform is fixedly installed outside one side of the simulated display screen, the button is fixedly installed on one side of the top end face of the operating platform, the control rod is welded in the center of the top end face of the bottom plate, the pedals are fixedly installed outside two sides of the control rod, the adjusting component is arranged at the other end of the top end face of the bottom plate, the base is arranged on the top end face of the adjusting component, the shaking component is arranged on the top end face of the base, and the seat is fixedly installed on the top end face of the shaking component;
the adjusting component comprises straight chutes, sliding blocks, fixing rods, connecting rods, a first motor, a push rod, a lifting column and a pipe sleeve, wherein the straight chutes are formed in two sides of the center of the other end of the top end face of the bottom plate, the two sliding blocks are installed inside the straight chutes in an inserting mode, the fixing rods are installed between the two sliding blocks through welding, the lifting column is fixedly installed on the top end face of the sliding block, one end of the top of the lifting column is fixedly connected with the bottom end face of the base through welding, the connecting rods are arranged above the tops of the straight chutes, two ends of each connecting rod are fixedly connected with the outer walls of the sliding blocks on one side inside of the two straight chutes respectively, the first motor is arranged on one side of the outer portion of each connecting rod and fixedly connected with the top end face of the bottom plate through screws, the pipe sleeve is installed on the outer portion of the other end of the first motor in a welding mode, and the inner wall of the pipe sleeve is connected with the outer wall of the push rod in a laminating mode, the top end face of the sliding block is welded with a lifting column, and the top end face of the lifting column is fixedly connected with the bottom end face of the base.
As a further scheme of the utility model: the equal fixed mounting in inner wall both sides of operation panel has the stereo set, and the earphone hole has been seted up to the one end outer wall of operation panel.
As a further scheme of the utility model: the inner wall laminating of seat is installed the foam-rubber cushion, inner wall one side fixed mounting of seat has the safety belt.
As a further scheme of the utility model: a plurality of limiting holes are formed in one side of the outer portion of the straight sliding groove in one end of the top of the bottom plate, a limiting sleeve is fixedly installed on the outer wall of the sliding block on one side of the corner of the bottom of the base through welding, a limiting rod is installed in the center of the end face of the limiting sleeve in an inserted mode, and one end of the bottom of the limiting rod penetrates through the limiting sleeve and is located in the limiting holes.
As a further scheme of the utility model: rock the subassembly and include second motor, transmission shaft, backup pad, annular spout, bracing piece, cylinder and telescopic link, the top terminal surface central authorities fixed mounting of base has the second motor, and the top one end of second motor is pegged graft and is installed the transmission shaft, the top terminal surface welded mounting of transmission shaft has the backup pad, and the bottom terminal surface of backup pad has seted up annular spout, the top terminal surface of base all welded mounting all around has the bracing piece, and the one end of bracing piece is connected with the inner wall laminating of annular spout, the top terminal surface of backup pad all welded mounting all around has the cylinder, and the top one end of cylinder is pegged graft and is installed the telescopic link, the one end of telescopic link and the bottom terminal surface fixed connection of seat.
As a further scheme of the utility model: the spring is fixedly installed in the center of the top end face of the supporting plate, and one end of the spring is fixedly connected with the bottom end face of the seat.
The utility model has the beneficial effects that: the general fixed-wing aircraft simulated flight equipment is simple to operate and good in using effect; the adjusting assembly has the effect of adjusting the equipment seat, the seat is adjusted forwards and backwards and upwards, so that the equipment is suitable for more people, the compatibility of the equipment is improved, the usability of the equipment is guaranteed, the seat can be fixed by inserting the limiting rod into the limiting hole, and the situation that the seat moves in the experience process and the experience feeling of an experiencer is influenced is prevented; the seat can rock when the simulated flight is carried out by the rocking assembly, the sense of reality of the simulated flight is increased by slight rotation and rocking of the seat, the experience sense of the simulated flight of an experiencer is improved, and the using effect of the equipment is increased.
Drawings
FIG. 1 is an isometric overall view of the present invention;
FIG. 2 is an overall elevational view of the present invention;
FIG. 3 is a schematic view of the adjusting assembly of the present invention;
FIG. 4 is a schematic view of the wobble assembly of the present invention;
illustration of the drawings: 1. a base plate; 2. simulating a display screen; 3. an operation table; 4. a button; 5. a control lever; 6. a pedal; 7. an adjustment assembly; 8. a base; 9. shaking the assembly; 10. a seat; 71. a straight chute; 72. a slider; 73. fixing the rod; 74. a connecting rod; 75. a first motor; 76. a push rod; 77. a lifting column; 78. pipe sleeve; 91. a second motor; 92. a drive shaft; 93. a support plate; 94. an annular chute; 95. a support bar; 96. a cylinder; 97. a telescopic rod.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Specific examples are given below.
Referring to fig. 1-4, a general fixed wing aircraft flight simulation device comprises a bottom plate 1, a simulation display screen 2, an operation table 3, a button 4, a control rod 5, a pedal 6, an adjusting component 7, a base 8, a shaking component 9 and a seat 10, wherein the simulation display screen 2 is fixedly installed at one end of the top end surface of the bottom plate 1, the operation table 3 is fixedly installed outside one side of the simulation display screen 2, sound devices are fixedly installed on both sides of the inner wall of the operation table 3, an earphone hole is formed in the outer wall of one end of the operation table 3, sound generated in the simulation flight can be played through the sound devices, the reality of the simulation flight experience is enhanced, earphones can be inserted and installed through the earphone hole, the sound can be heard more clearly, the button 4 is fixedly installed on one side of the top end surface of the operation table 3, the control rod 5 is welded in the center of the top end surface of the bottom plate 1, and the pedals 6 are fixedly installed outside both sides of the control rod 5, the other end of the top end face of the bottom plate 1 is provided with an adjusting assembly 7, the top end face of the adjusting assembly 7 is provided with a base 8, the top end face of the base 8 is provided with a shaking assembly 9, a seat 10 is fixedly mounted on the top end face of the shaking assembly 9, a sponge cushion is mounted on the inner wall of the seat 10 in a fitting mode, a safety belt is fixedly mounted on one side of the inner wall of the seat 10, a more comfortable experience environment can be provided for an experiencer during simulated flight through mounting of the sponge cushion, the experiencer can be more firmly seated on the seat 10 when the safety belt is mounted, and the experiencer is prevented from falling off the seat 10 to generate danger when the seat 10 shakes;
the adjusting component 7 comprises a straight chute 71, a sliding block 72, a fixing rod 73, a connecting rod 74, a first motor 75, a push rod 76, a lifting column 77 and a pipe sleeve 78, wherein the straight chute 71 is respectively arranged at two sides of the center of the other end surface of the top part of the bottom plate 1, two sliding blocks 72 are inserted in the straight chute 71, the fixing rod 73 is fixedly arranged between the two sliding blocks 72 through welding, the lifting column 77 is fixedly arranged on the end surface of the top part of the sliding block 72, one end of the top part of the lifting column 77 is fixedly welded with the end surface of the bottom part of the base 8, the connecting rod 74 is arranged above the top part of the straight chute 71, two ends of the connecting rod 74 are respectively fixedly connected with the outer walls of the sliding blocks 72 at one side of the inner parts of the two straight chutes 71, the first motor 75 is arranged at one side of the outer part of the connecting rod 74, the first motor 75 is fixedly connected with the end surface of the top part of the bottom plate 1 through a screw, the pipe sleeve 78 is welded at the other end part of the first motor 75, the inner wall of the pipe sleeve 78 is connected with the outer wall of the push rod 76 in a fitting manner, the top end face of the sliding block 72 is welded with a lifting column 77, the top end face of the lifting column 77 is fixedly connected with the bottom end face of the base 8, one side of the outer portion of the straight sliding groove 71 at one end of the top of the bottom plate 1 is provided with a plurality of limiting holes, the outer wall of the sliding block 72 at one side of the corner of the bottom of the base 8 is fixedly provided with a limiting sleeve in a welding manner, a limiting rod is inserted and installed in the center of the end face of the limiting sleeve, one end of the bottom of the limiting rod penetrates through the limiting sleeve and is located in the limiting hole, and the limiting rod is inserted and installed in the limiting hole, so that the seat 10 can be fixed, the seat 10 is prevented from moving in the experience process, and the experience feeling of an experiencer is influenced;
the shaking assembly 9 comprises a second motor 91, a transmission shaft 92, a support plate 93, an annular chute 94, a support rod 95, a cylinder 96 and a telescopic rod 97, the second motor 91 is fixedly installed in the center of the top end face of the base 8, the transmission shaft 92 is installed at one end of the top of the second motor 91 in an inserted manner, the support plate 93 is installed on the top end face of the transmission shaft 92 in a welded manner, a spring is fixedly installed in the center of the top end face of the support plate 93, one end of the spring is fixedly connected with the bottom end face of the seat 10, the connection performance between the spring and the seat 10 can be improved through the spring, after the seat 10 shakes, the spring can help the seat 10 to rapidly reset, meanwhile, the spring provides a damping effect, the influence of shaking on equipment is reduced, the annular chute 94 is formed in the bottom end face of the support plate 93, the support rods 95 are welded around the top end face of the base 8, and one end of each support rod 95 is connected with the inner wall of the annular chute 94 in an attached manner, all welded mounting has cylinder 96 all around the top end face of backup pad 93, and the telescopic link 97 is installed in the grafting of the top one end of cylinder 96, the one end of telescopic link 97 and the bottom terminal surface fixed connection of seat 10.
The working principle of the utility model is as follows: when the simulation device is used, an experiencer sits on the seat 10 firstly, the push rod 76 is driven by the first motor 75 to move forwards and backwards, the position of the seat 10 is adjusted, acting force is transmitted to the connecting rod 74 through the push rod 76, the sliding block 72 moves in the straight sliding groove 71, the sliding block 72 of the same straight sliding groove 71 is connected by the fixing rod 73, the stability during moving is improved, the moving push rod 76 is limited through the pipe sleeve 78, the push rod 76 can push and pull a specified point, the height of the base 8 is changed through the lifting of the lifting column 77, the experiencer sits more comfortably, the experiencer starts equipment by pressing the button 4 on the operating platform 3, simulated flight is performed by pulling the control rod 5 and stepping the pedal 6, a flying picture is displayed through the simulation display screen 2, and in the process of simulated flight, the transmission shaft 92 is driven by the second motor 91 to rotate, make backup pad 93 can drive seat 10 redirecting, when backup pad 93 rotated, bracing piece 95 supported in annular chute 94 for backup pad 93 is more stable, pushes up through cylinder 96 and moves telescopic link 97, lets seat 10 can possess the sensation of rocking about, increases the authenticity of simulation nature of flying.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and equivalent alternatives or modifications according to the technical solution of the present invention and the inventive concept thereof should be covered by the scope of the present invention.

Claims (6)

1. A general fixed wing aircraft simulated flight device is characterized by comprising a bottom plate (1), a simulated display screen (2), an operating platform (3), a button (4), a control rod (5), a pedal (6), an adjusting component (7), a base (8), a shaking component (9) and a seat (10), wherein the simulated display screen (2) is fixedly installed at one end of the top end face of the bottom plate (1), the operating platform (3) is fixedly installed outside one side of the simulated display screen (2), the button (4) is fixedly installed at one side of the top end face of the operating platform (3), the control rod (5) is welded and installed in the center of the top end face of the bottom plate (1), the pedals (6) are fixedly installed outside two sides of the control rod (5), the adjusting component (7) is arranged at the other end face of the top of the bottom plate (1), and the base (8) is arranged on the top end face of the adjusting component (7), a shaking assembly (9) is arranged on the top end face of the base (8), and a seat (10) is fixedly mounted on the top end face of the shaking assembly (9);
the adjusting component (7) comprises straight sliding grooves (71), sliding blocks (72), fixing rods (73), connecting rods (74), a first motor (75), a push rod (76), lifting columns (77) and pipe sleeves (78), the straight sliding grooves (71) are formed in two sides of the center of the other end of the top end face of the bottom plate (1), the two sliding blocks (72) are installed in the straight sliding grooves (71) in an inserting mode, the fixing rods (73) are fixedly installed between the two sliding blocks (72) through welding, the lifting columns (77) are fixedly installed on the top end faces of the sliding blocks (72), one ends of the tops of the lifting columns (77) are fixedly welded with the bottom end face of the base (8), the connecting rods (74) are arranged above the tops of the straight sliding grooves (71), and two ends of the connecting rods (74) are fixedly connected with the outer walls of the sliding blocks (72) on one side of the inner portions of the two straight sliding grooves (71) respectively, outside one side of connecting rod (74) is provided with first motor (75), and first motor (75) pass through the top terminal surface fixed connection of screw and bottom plate (1), pipe box (78) are installed to the other end external welding of first motor (75), and the inner wall of pipe box (78) is connected with the outer wall laminating of push rod (76), the top terminal surface welding of slider (72) installs lift post (77), and the top terminal surface of lift post (77) and the bottom terminal surface fixed connection of base (8).
2. The general fixed-wing aircraft simulated flight device as claimed in claim 1, wherein sound equipment is fixedly mounted on both sides of the inner wall of the operating platform (3), and an earphone hole is formed in the outer wall of one end of the operating platform (3).
3. The general fixed-wing aircraft simulated flight device as claimed in claim 1, wherein a sponge cushion is attached to the inner wall of the seat (10), and a safety belt is fixedly mounted on one side of the inner wall of the seat (10).
4. The universal fixed wing aircraft simulated flight device according to claim 1, characterized in that a plurality of limiting holes are formed in one side of the outer portion of the straight sliding groove (71) at one end of the top of the bottom plate (1), a limiting sleeve is fixedly installed on the outer wall of the sliding block (72) on one side of the corner of the bottom of the base (8) through welding, a limiting rod is installed in the center of the end face of the limiting sleeve in an inserted mode, and one end of the bottom of the limiting rod penetrates through the limiting sleeve and is located in the limiting hole.
5. The general fixed-wing aircraft simulated flight device according to claim 1, wherein the shaking assembly (9) comprises a second motor (91), a transmission shaft (92), a support plate (93), an annular chute (94), a support rod (95), a cylinder (96) and a telescopic rod (97), the second motor (91) is fixedly installed in the center of the top end face of the base (8), the transmission shaft (92) is installed at one end of the top of the second motor (91) in an inserted manner, the support plate (93) is installed on the top end face of the transmission shaft (92) in a welded manner, the annular chute (94) is formed in the bottom end face of the support plate (93), the support rods (95) are installed around the top end face of the base (8) in a welded manner, one end of the support rod (95) is connected with the inner wall of the annular chute (94) in an attached manner, the cylinders (96) are installed around the top end face of the support plate (93) in a welded manner, and the top one end of cylinder (96) is pegged graft and is installed telescopic link (97), the one end of telescopic link (97) and the bottom terminal surface fixed connection of seat (10).
6. The generic fixed-wing aircraft simulated flight device of claim 5, characterized in that a spring is fixedly mounted centrally on the top end face of the support plate (93) and one end of the spring is fixedly connected to the bottom end face of the seat (10).
CN202122062232.8U 2021-08-30 2021-08-30 General fixed wing aircraft simulation flight equipment Expired - Fee Related CN215770140U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202122062232.8U CN215770140U (en) 2021-08-30 2021-08-30 General fixed wing aircraft simulation flight equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202122062232.8U CN215770140U (en) 2021-08-30 2021-08-30 General fixed wing aircraft simulation flight equipment

Publications (1)

Publication Number Publication Date
CN215770140U true CN215770140U (en) 2022-02-08

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Application Number Title Priority Date Filing Date
CN202122062232.8U Expired - Fee Related CN215770140U (en) 2021-08-30 2021-08-30 General fixed wing aircraft simulation flight equipment

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114822142A (en) * 2022-04-13 2022-07-29 滨州学院 Flight simulation training device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114822142A (en) * 2022-04-13 2022-07-29 滨州学院 Flight simulation training device

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Granted publication date: 20220208