CN212256638U - General flight simulation cabin structure - Google Patents

General flight simulation cabin structure Download PDF

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Publication number
CN212256638U
CN212256638U CN202021120481.7U CN202021120481U CN212256638U CN 212256638 U CN212256638 U CN 212256638U CN 202021120481 U CN202021120481 U CN 202021120481U CN 212256638 U CN212256638 U CN 212256638U
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China
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support
base
seat
vertical
seat base
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CN202021120481.7U
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Chinese (zh)
Inventor
胡进海
金泽芬芬
孙月
吕奇
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Weifei Technology Co ltd
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Xi'an Weifei Simulation Technology Co ltd
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Abstract

The utility model discloses a general flight simulation cabin structure conveniently realizes the flight simulator of multiple model under different scenes, different application demands fast. The simulation cabin structure comprises a front end base, a seat base, an underframe crossbeam, an adjustable central control rod support connected to the middle of the underframe crossbeam, a visual display support with adjustable height connected to the front end base, a central operating platform support connected to the front end base, a foot-steering pedal support with one end connected with the front end base and the other end connected with the underframe crossbeam, an adjustable keyboard support frame connected with the right side of the seat base, an adjustable left operating platform and an adjustable right operating platform connected to the seat base, and an adjustable seat mounted on the seat base. Through the design, the utility model discloses a possess free nimble characteristics, all kinds of operation panels all can carry out the regulation of multi-direction multi-angle according to actual need, make whole device can realize the aircraft simulation under different scenes, the different application demands.

Description

General flight simulation cabin structure
Technical Field
The utility model relates to a flight simulation cabin structure, specifically speaking relates to a general flight simulation cabin structure.
Background
With the rapid development of civil aviation industry in China, the opening of airspace in China and the relaxation of personal flight driving licenses, various flight experience devices and flight simulators become more concerned. However, for units such as aviation experience libraries, aviation science and technology libraries, and aviation education and training institutions, to meet the flight experience of visitors for different categories and different models, purchasing a flight simulator of a single model means greater investment and higher risk. Therefore, the research and development of a set of general flight simulation cabins has great practical significance.
The universal flight simulation cabin has high requirements on the flexibility of hardware structure design, can be adjusted according to different types of machines, and simultaneously needs to reserve flexible interfaces for related components, so that secondary developers can conveniently configure the universal flight simulation cabin. Meanwhile, the general flight simulation cabin should be compatible with common and common flight peripherals on the market, and an installation module of a related panel or an operating system is reserved.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a general flight simulation cabin structure conveniently realizes the flight simulator of multiple model under different scenes, different application demands fast.
In order to achieve the above object, the utility model adopts the following technical scheme:
the utility model provides a general flight simulation cabin structure, including the front end base, pass through the seat base that the adjusting connection spare links to each other with the front end base, the chassis crossbeam that links to each other with the adjusting connection spare, but connect the visual display support of height-adjusting on the front end base, install the multi-functional display support on visual display support, connect the central operation platform support on the front end base, one end is connected the rudder pedal support that the other end is connected with the chassis crossbeam with the front end base, the adjustable keyboard support frame of being connected on seat base right side, and install the adjustable seat on the seat base.
Further, the flight simulation cabin structure further comprises a central joystick bracket connected with the seat base; the central control rod support comprises a connecting support rod connected with the seat base, a first profile steel vertical shaft vertically connected with the connecting support rod, a second profile steel vertical shaft sleeved on the first profile steel vertical shaft and adjusted in height through two manual knobs, and a middle support table fixedly connected to the second profile steel vertical shaft.
Further, the visual display support comprises two first vertical rods vertically connected with the front end base, second vertical rods inserted into the first vertical rods and adjusted in height through a manual knob, a first support cross beam connected with the two second vertical rods through a screw lock catch, an extension support cross beam connected to two ends of the first support cross beam through an articulated piece, and a screen support arranged on the first support cross beam and the extension support cross beam.
The multifunctional display support comprises a second support cross beam which is connected with the two second vertical rods through screw lock catches and is positioned below the first support cross beam, and a screen support which is installed on the second support cross beam.
Furthermore, the central operating platform support comprises two third vertical rods vertically connected with the front end base, inclined supporting rods connected with each third vertical rod through elbow connecting pieces, first connecting rods connected with each inclined supporting rod through manual knobs, first horizontal supporting rods connected with the other ends of the first connecting rods through the elbow connecting pieces, first vertical sleeves fixedly connected with each first horizontal supporting rod, and an upper platen inserted into the first vertical sleeves and adjusted in height through the two manual knobs.
Further, the keyboard support frame includes the fourth montant that meets with the seat base is perpendicular, pegs graft in the fourth montant and through the second connecting rod of two manual knob height-adjusting, through the second horizontal branch that elbow connecting piece and second connecting rod link to each other, through the vertical sleeve pipe of second that elbow connecting piece and second horizontal branch link to each other, peg graft in the vertical sleeve pipe of second and through the keyboard mouse tray of manual knob height-adjusting.
Furthermore, the flight simulation cabin structure also comprises an adjustable left operating platform connected to the seat base; the left operating platform comprises a third steel vertical shaft fixedly connected to the seat base, a fourth steel vertical shaft connected to the third steel vertical shaft in a sleeved mode and adjusted in height through two manual knobs, a first horizontal connecting shaft vertically connected with the fourth steel vertical shaft, a second horizontal connecting shaft hinged to the other end of the horizontal connecting shaft through a locking adjusting nut, a fifth steel vertical shaft vertically connected with the second horizontal connecting shaft, and a left supporting platform connected to the fifth steel vertical shaft in a plugged mode and adjusted in height through the two manual knobs.
Further, flight simulation cabin structure still includes the right operation panel of adjustable of connecting on the seat base, right operation panel includes fixed connection in the support cylinder on the seat base, cup joints the regulation pipe on the support cylinder to and peg graft in the regulation pipe and through the right supporting bench of two manual knob height-adjusting.
Furthermore, the adjustable seat comprises a seat mounting plate arranged on the seat base, two slide rails arranged on the seat mounting plate, and a seat connected with the slide rails in a sliding manner.
Furthermore, the adjusting and connecting piece comprises a first sleeve sleeved on the front end base, a second sleeve sleeved on the seat base and an adjusting pipe, wherein one end of the adjusting pipe is inserted into the first sleeve, the other end of the adjusting pipe is inserted into the second sleeve, and the two ends of the adjusting pipe are adjusted in telescopic length through a manual knob.
Further, the screen support includes the hasp that is used for the joint, with the articulated horizontal rotation piece of hasp, with the articulated vertical rotation piece of horizontal rotation piece outer end to and the screen pre-installation frame of being connected with vertical rotation piece.
Compared with the prior art, the utility model discloses following beneficial effect has:
(1) the utility model discloses a simulation cabin structure can be set up aircraft simulation operation part according to concrete simulation aircraft's structure to each part bearing structure all adopts adjustable structure to set up, possesses the characteristics of freedom and flexibility, and all kinds of operation panels all can carry out the regulation of multi-direction multi-angle according to actual need, make whole device can realize the aircraft simulation under different scenes, the different application demands.
(2) The utility model discloses a screen support sets up horizontal rotation piece and vertical rotation piece through articulated, shows the installation and uses the back, can realize the multi-angle pivoted needs of display according to actual need, and the convenience is adjusted according to the visual angle custom of different simulators.
Drawings
Fig. 1 is a schematic view of the overall three-dimensional structure of the present invention.
Fig. 2 is a front view of the present invention.
Fig. 3 is a top view of the present invention.
Fig. 4 is a schematic structural view of the left operating table of the present invention.
Fig. 5 is a schematic structural view of the right console of the present invention.
Fig. 6 is a schematic view of the keyboard support frame of the present invention.
Fig. 7 is a schematic structural diagram of the adjusting connector of the present invention.
Fig. 8 is a schematic view of the screen support structure of the present invention.
Wherein, the names corresponding to the reference numbers are:
1-front base, 2-adjusting link, 21-first sleeve, 22-second sleeve, 23-adjusting tube, 3-seat base, 4-base frame beam, 5-central control lever support, 51-connecting strut, 52-first profile steel vertical shaft, 53-second profile steel vertical shaft, 54-middle support table, 6-visual display support, 61-first vertical rod, 62-second vertical rod, 63-screw lock, 64-first support beam, 65-second support beam, 66-hinge, 67-extension support beam, 68-screen support, 69-lock, 610-transverse rotating member, 611-vertical rotating member, 612-screen pre-mounting frame, 7-central console support, 71-third vertical rod, 72-inclined strut, 73-first connecting rod, 74-first horizontal strut, 75-first vertical sleeve, 76-upper deck, 8-rudder pedal support, 9-keyboard support, 91-fourth vertical rod, 92-second connecting rod, 93-second horizontal strut, 94-second vertical sleeve, 95-keyboard mouse tray, 10-left console, 101-third profile vertical shaft, 102-fourth profile vertical shaft, 103-first horizontal connecting shaft, 104-second horizontal connecting shaft, 105-fifth profile vertical shaft, 106-left support table, 107-locking adjusting nut, 11-right console, 111-support column, 112-adjusting circular tube, 113-right support table, 12-adjustable seat, 121-seat mounting plate, 122-slide rail, 123-seat, 13-manual knob, 14-elbow connector.
Detailed Description
The present invention will be further described with reference to the following description and examples, which include but are not limited to the following examples.
Examples
As shown in fig. 1 ~ 8, the utility model discloses a general flight simulation cabin structure, including front end base 1, seat base 3 that links to each other through adjusting connecting piece 2 with front end base 1, chassis crossbeam 4 that links to each other with adjusting connecting piece 2, but connect visual display support 6 of height-adjusting on front end base 1, install the multifunctional display support on visual display 6 support, connect central operation platform support 7 on front end base 1, one end is connected the rudder pedal support 8 that the other end is connected with chassis crossbeam 4 with front end base 1, adjustable keyboard support frame 9 of being connected on seat base 3 right side, and install adjustable seat 12 on seat base 3. Wherein, adjusting the connecting piece 2 including cup jointing in the first sleeve pipe 21 on front end base 1, cup jointing in the second sleeve pipe 22 on the seat base to and one end peg graft in first sleeve pipe 21 and the other end peg graft in the adjusting tube 23 of second sleeve pipe 22, adjusting tube 23 both ends are all through manual knob 13 regulation flexible length. In this way, the distance between the front end base and the seat base is made adjustable.
Wherein, the foot rudder pedal bracket 8 can be provided with foot rudders of the following types: the Logitech Flight rudders with toe brake simulation controller special Rudder pedal, Thrustmaster TPR professional grade Flight foot Rudder.
The utility model discloses in, view display support 6 includes and is connected two first montants 61 perpendicularly with front end base 1, pegs graft in first montant 61 and through the second montant 62 of manual knob 13 height-adjusting, through screw hasp 63 and two second montants 62 link to each other and parallel arrangement's first support crossbeam 64, connect in the extension support crossbeam 67 at first support crossbeam 64 both ends through articulated elements 66 to and set up in first support crossbeam 64, the screen support 68 on the extension support crossbeam 67. Still install the multifunctional display support on the visual display support, the multifunctional display support includes that it links to each other and is located the second support crossbeam 65 of first support crossbeam 64 below through screw hasp and two second montants to and install in the screen support of second support crossbeam 65.
And, the screen bracket 68 includes a latch 69 for latching, a transverse rotating member 610 hinged to the latch 69, a vertical rotating member 611 hinged to an outer end of the transverse rotating member 610, and a screen pre-mounting bracket 612 connected to the vertical rotating member 611. When the specific simulator is installed, the screen support is installed on the corresponding support beam through the lock catch, the extension support beam is additionally arranged for meeting the multi-screen requirements of the simulator, the extension support beam can also rotate by a certain angle by utilizing the hinge 66, and the left screen and the right screen can be bent towards the middle after the display is installed. The whole visual display support can adjust the height of the visual display through the relative height of the first vertical rod and the second vertical rod adjusted by a manual knob. The visual display support can be used for mounting 1 display below 65 inches or 3 displays of 24-32 inches.
The utility model discloses in, the analog compartment structure still includes central control rod support 5, central control rod support 5 includes the connecting rod 51 that links to each other with the seat base, with the first shaped steel vertical axis 52 that connecting rod 51 meets perpendicularly, cup joints on first shaped steel vertical axis 52 and through two manual knob 13 height-adjusting's second shaped steel vertical axis 53 to and well supporting bench 54 of fixed connection on second shaped steel vertical axis 53. The support platform serves as a central operating lever support. Such as including but not limited to a Thrustmaster A10C all-metal wart pig bimanual flight controller, etc.
The utility model discloses in, central console support 7 includes two third montants 71 that meet perpendicularly with front end base 1, connect in the slope branch 72 of every third montant 71 through elbow connecting piece 14, through the head rod 73 that manual knob 13 and every slope branch 72 link to each other, through the first horizontal branch 74 that elbow connecting piece 14 and every head rod 73 other end link to each other, with the first vertical sleeve pipe 75 of every first horizontal branch 74 fixed connection, peg graft in first vertical sleeve pipe 75 and through two upper platen 76 of manual knob 13 height-adjusting. The part of the support is used for installing the whole central operation console, a control system installing interface is reserved on the support, and a Roots Flight Switch cockpit analog Switch controller, a Roots Flight Multi Panel analog automatic navigation cockpit controller and a Roots Flight Radio Panel analog Radio controller can be installed on the support.
The utility model discloses in, keyboard support frame 9 includes the fourth montant 91 that meets perpendicularly with seat base 3, pegs graft in fourth montant 91 and through the second connecting rod 92 of two manual knobs 13 height-adjusting, through the second horizontal branch 93 that elbow connecting piece 14 and second connecting rod 92 link to each other, through the vertical sleeve pipe 94 of second that elbow connecting piece 14 and second horizontal branch 93 link to each other, peg graft in the vertical sleeve pipe 94 of second and through the keyboard mouse tray 95 of manual knob 94 height-adjusting. The partial bracket is used for mounting and placing a keyboard and a mouse.
In the present invention, the adjustable seat 12 includes a seat mounting plate 121 installed on the seat base 3, two slide rails 122 disposed on the seat mounting plate 121, and a seat 123 slidably connected to the slide rails 122. The seat can be adjusted in a pitching mode, and the front-back distance of the seat can be adjusted through the sliding rail.
In another embodiment, the simulated cabin structure further comprises an adjustable left console 10 connected to the seat base 3; the left operating platform 10 comprises a third steel vertical shaft 101 fixedly connected to the seat base 3, a fourth steel vertical shaft 102 connected to the third steel vertical shaft 101 in a sleeved mode and adjusted in height through two manual knobs 13, a first horizontal connecting shaft 103 vertically connected with the fourth steel vertical shaft 102, a second horizontal connecting shaft 104 hinged to the other end of the horizontal connecting shaft 103 through a locking adjusting nut 107, a fifth steel vertical shaft 105 vertically connected with the second horizontal connecting shaft 104, and a left supporting platform 106 connected to the fifth steel vertical shaft 105 in an inserted mode and adjusted in height through the two manual knobs 13. During the use, can unscrew locking adjusting nut 107 through special handle, and then rotate the position of second horizontal connecting axle, conveniently simulate navigating mate and take a seat. The left operating platform can be provided with a Logitech X52 HOTAS accelerator, a Logitech X56 HOTAS RGB accelerator, a Thrustmaster A10C all-metal wart pig two-hand flight controller accelerator and the like.
In another embodiment, the simulation cabin structure further includes an adjustable right operation platform 11 connected to the seat base 3, and the right operation platform 11 includes a support cylinder 111 fixedly connected to the seat base 3, an adjusting circular tube 112 sleeved on the support cylinder 111, and a right support platform 113 inserted into the adjusting circular tube 112 and having a height adjusted by two manual knobs 13. The right console can be provided with Logitech X52 HOTAS rocker controller, Logitech X56 HOTAS RGB rocker controller, Thrustmaster A10C all-metal wart pig double-hand flight controller rocker, etc.
For example, for a model simulation, the left operation table is provided with an accelerator corresponding to the model, such as a Logitech X56 HOTAS RGB accelerator, the right operation table is provided with a steering column corresponding to the model, such as a Logitech X56 HOTAS RGB rocker controller, and a foot Rudder corresponding to the model, such as a special Rudder pedal with a toe brake simulation controller, is arranged on a foot Rudder pedal bracket.
For another specific model simulation, the left console may be equipped with a throttle, such as a Thrustmaster A10C all-metal throttle, the central control lever bracket is equipped with a steering column, such as a Thrustmaster A10C all-metal two-hand flight controller, and the foot rudder pedal bracket is equipped with a foot rudder, such as a Thrustmaster TPR professional grade flight foot rudder.
Or another machine type, the left side of the central operation platform can be provided with a steering column, such as a Honeycomb cellular alpha YOKE & switch panel Flight controller, the right side of the central operation platform is provided with an accelerator, such as a Logitech Flight Yoke System accelerator arc seat, and a foot Rudder is arranged on a foot Rudder pedal bracket, such as a special Rudder pedal with a toe brake simulation controller.
Through the design, the simulation cabin structure of the utility model can be used for setting up aircraft simulation operation parts according to the structure of a specific simulation aircraft, and each part supporting structure adopts an adjustable structure, so that the simulation cabin structure has the characteristics of freedom and flexibility, and various operation platforms can be adjusted in multiple directions and multiple angles according to actual needs, so that the whole device can realize aircraft simulation under different scenes and different application requirements, and the application scenes can be simulated flight exercises of an aeronautical and scientific center and an experience shop; simulating a flight classroom for primary and middle schools; simulating flight practice of flight enthusiasts; the research of simulated flight subjects of aviation scientific research institutes, and the like. Therefore, compared with the prior art, the utility model has the substantive characteristics and progress.
The above embodiment is only one of the preferred embodiments of the present invention, and should not be used to limit the protection scope of the present invention, but all the insubstantial changes or modifications made in the spirit and the idea of the main design of the present invention, the technical problems solved by the embodiment are still consistent with the present invention, and all should be included in the protection scope of the present invention.

Claims (10)

1. The utility model provides a general flight simulation cabin structure, a serial communication port, including front end base (1), seat base (3) that link to each other through adjusting connecting piece (2) with front end base (1), chassis crossbeam (4) that link to each other with adjusting connecting piece (2), but connect visual display support (6) of height-adjusting on front end base (1), install the multi-functional display support on visual display support (6), connect central operation platform support (7) on front end base (1), one end is connected foot rudder footboard support (8) that the other end is connected with chassis crossbeam (4) with front end base (1), adjustable keyboard support frame (9) of being connected on seat base (3) right side, and install adjustable seat (12) on seat base (3).
2. A generic flight simulator cabin structure according to claim 1, characterized in that it further comprises a central joystick bracket (5) connected to the seat base; the central control rod support (5) comprises a connecting support rod (51) connected with the seat base, a first profile steel vertical shaft (52) vertically connected with the connecting support rod (51), a second profile steel vertical shaft (53) sleeved on the first profile steel vertical shaft (52) and adjusted in height through two manual knobs (13), and a middle support table (54) fixedly connected to the second profile steel vertical shaft (53).
3. A generic flight simulator cabin structure according to claim 2, characterized in that the view display support (6) comprises two first vertical bars (61) vertically connected to the front end base (1), a second vertical bar (62) inserted into the first vertical bar (61) and adjusted in height by means of a manual knob (13), a first support beam (64) connected to the two second vertical bars (62) by means of screw fasteners (63), an extension support beam (67) connected to both ends of the first support beam (64) by means of an articulation (66), and a screen support (68) arranged on the first support beam (64) and the extension support beam (67).
4. A generic flight simulator cabin structure according to claim 3, characterized in that the central console support (7) comprises two third vertical bars (71) connected perpendicularly to the front base (1), an inclined strut (72) connected to each third vertical bar (71) by means of an elbow connection (14), a first connection bar (73) connected to each inclined strut (72) by means of a manual knob (13), a first horizontal strut (74) connected to the other end of each first connection bar (73) by means of an elbow connection (14), a first vertical sleeve (75) fixedly connected to each first horizontal strut (74), an upper platen (76) inserted in the first vertical sleeve (75) and adjusted in height by means of two manual knobs (13).
5. A generic flight simulator cabin structure according to claim 4, characterized in that the keyboard support frame (9) comprises a fourth vertical bar (91) connected vertically to the seat base (3), a second connecting bar (92) inserted in the fourth vertical bar (91) and adjusted in height by means of two manual knobs (13), a second horizontal strut (93) connected to the second connecting bar (92) by means of an elbow connector (14), a second vertical sleeve (94) connected to the second horizontal strut (93) by means of an elbow connector (14), and a keyboard and mouse tray (95) inserted in the second vertical sleeve (94) and adjusted in height by means of a manual knob (13).
6. A generic flight simulator cabin structure according to claim 1, characterized in that it further comprises an adjustable left console (10) connected to the seat base (3); left side operation panel (10) are including third shaped steel vertical axis (101) of fixed connection on seat base (3), cup joint on third shaped steel vertical axis (101) and through two manual knob (13) height-adjusting's fourth shaped steel vertical axis (102), first horizontal connecting axle (103) that meet perpendicularly with fourth shaped steel vertical axis (102), pass through locking adjusting nut (107) articulated second horizontal connecting axle (104) with horizontal connecting axle (103) other end, fifth shaped steel vertical axis (105) that meet perpendicularly with second horizontal connecting axle (104), and peg graft in fifth shaped steel vertical axis (105) and through two manual knob (13) height-adjusting's left brace table (106).
7. A general flight simulation cabin structure according to claim 1, further comprising an adjustable right console (11) connected to the seat base (3), wherein the right console (11) comprises a support cylinder (111) fixedly connected to the seat base (3), an adjusting circular tube (112) sleeved on the support cylinder (111), and a right support platform (113) inserted into the adjusting circular tube (112) and having a height adjusted by two manual knobs (13).
8. A generic flight simulator cabin structure according to claim 1, characterized in that the adjustable seat (12) comprises a seat mounting plate (121) mounted on the seat base (3), two slide rails (122) arranged on the seat mounting plate (121), and a seat (123) slidably connected to the slide rails (122).
9. The general flight simulation cabin structure according to claim 1, wherein the adjusting connector (2) comprises a first sleeve (21) sleeved on the front end base (1), a second sleeve (22) sleeved on the seat base (3), and an adjusting pipe (23) with one end inserted in the first sleeve (21) and the other end inserted in the second sleeve (22), and the two ends of the adjusting pipe (23) are adjusted in telescopic length by a manual knob (13).
10. A generic flight simulator cabin structure according to claim 3, characterized in that the screen support (68) comprises a latch (69) for snap-fitting, a lateral turning member (610) hinged to the latch (69), a vertical turning member (611) hinged to the outer end of the lateral turning member (610), and a screen pre-mount bracket (612) connected to the vertical turning member (611).
CN202021120481.7U 2020-06-17 2020-06-17 General flight simulation cabin structure Active CN212256638U (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116092350A (en) * 2022-12-02 2023-05-09 通航未来(北京)航空技术发展集团有限公司 Double-seat teaching flight simulation equipment and flight simulation cabin

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116092350A (en) * 2022-12-02 2023-05-09 通航未来(北京)航空技术发展集团有限公司 Double-seat teaching flight simulation equipment and flight simulation cabin

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Effective date of registration: 20240602

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Address before: G41, 7th floor, angel building, 9 Gaoxin 2nd Road, Zhangba Street office, high tech Zone, Xi'an City, Shaanxi Province, 710000

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