CN212256639U - Simulated flight support - Google Patents

Simulated flight support Download PDF

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Publication number
CN212256639U
CN212256639U CN202021290963.7U CN202021290963U CN212256639U CN 212256639 U CN212256639 U CN 212256639U CN 202021290963 U CN202021290963 U CN 202021290963U CN 212256639 U CN212256639 U CN 212256639U
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China
Prior art keywords
support
flight
mounting
supporting
section
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CN202021290963.7U
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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 simulated flight bracket, which comprises a supporting underframe, a pair of fixed connecting pieces arranged on the left and right frames of the supporting underframe, an installation front beam arranged at the front end of the supporting underframe, an installation rear beam arranged between the two fixed connecting pieces, a foot-steering pedal bracket connected between the installation front beam and the installation rear beam, and a supporting platform mounting plate arranged on the supporting platform bracket; and reserved mounting holes suitable for various flying peripherals are formed in the foot rudder pedal bracket, the operating platform mounting plate and the supporting platform mounting plate. The utility model discloses a simulation flight support makes things convenient for simulation flight training personnel to use flight simulation peripheral hardware. And, all be provided with the reservation mounting hole that adapts to multiple flight peripheral hardware on rudder pedal support, the operation panel mounting panel, the brace table mounting panel, be convenient for install the simulation flight peripheral hardware of different models, it is more convenient to use.

Description

Simulated flight support
Technical Field
The utility model belongs to the technical field of the simulation aircraft technique and specifically relates to a simulation flight support is related to.
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 simulated flight support is used as a main body of the flight simulation cabin, and the structure of the support is approximately determined, so that the research and development of the freely configured and flexibly assembled simulated flight support has great practical significance.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a simulation flight support, the configuration of simulation flight peripheral hardware is convenient, and the simulation flight training personnel of being convenient for use the simulation flight peripheral hardware.
In order to achieve the above object, the utility model adopts the following technical scheme:
a simulated flight support comprises a supporting underframe, a pair of fixed connecting pieces arranged on left and right frames of the supporting underframe, a mounting front beam arranged at the front end of the supporting underframe, a mounting rear beam arranged between the two fixed connecting pieces, a foot-steering pedal support with one end connected to the mounting front beam and the other end connected to the mounting rear beam, two operating platform supports correspondingly arranged on the two fixed connecting pieces respectively, operating platform mounting plates arranged on the two operating platform supports, a supporting platform support connected to each operating platform support, and a supporting platform mounting plate arranged on the supporting platform support; and reserved mounting holes suitable for various flying peripherals are formed in the foot rudder pedal bracket, the operating platform mounting plate and the supporting platform mounting plate.
Furthermore, a plurality of mounting holes with different heights are formed in the fixed connecting pieces, and the mounting rear beam is connected between the mounting holes with the same height of the two fixed connecting pieces.
Furthermore, the operating platform bracket comprises a first supporting square tube arranged on the fixed connecting piece, a second supporting square tube adjustably connected with the first supporting square tube through a manual knob, and a horizontal branch tube connected to the second supporting square tube; the operating platform mounting plate is mounted on the horizontal branch pipe, and the support table support is vertically connected to the middle of the second support square pipe.
Furthermore, the first supporting square tube comprises a vertical section connected with the fixed connecting piece, a bending section connected with the vertical section and bent towards one side of the simulation training personnel, and an inclined section connected with the bending section and inclined towards one side of the simulation training personnel; wherein, the second supports the square pipe and links to each other with the slope section of first support square pipe.
Furthermore, the support platform bracket comprises an inclined connecting section which is vertically connected with the second support square pipe through screw fixation, a transition section which is connected with the inclined connecting section and is used for the support platform bracket to transition to the horizontal direction, and a horizontal section which is connected with the other end of the transition section; wherein, the supporting table mounting plate is fixedly connected with the horizontal section through screws.
Furthermore, the fixed connecting piece is formed by sequentially connecting a large L-shaped guard plate and a small L-shaped guard plate, and the long edge of the large L-shaped guard plate is connected with the short edge of the small L-shaped guard plate; wherein, the vertical section of first support side's pipe is connected between big L type backplate and a little L type backplate, and the installation back beam is outwards extended by the breach department that big L type backplate and a little L type backplate enclose into formation.
Furthermore, support columns are further arranged at four corners of the bottom end of the support bottom frame.
Compared with the prior art, the utility model discloses following beneficial effect has:
(1) the utility model discloses a simulation flight support can freely dispose the visual ware support and the seat in flight simulation cabin, and convenient simulation flight training personnel use flight simulation peripheral hardware. And, all be provided with the reservation mounting hole that adapts to multiple flight peripheral hardware on rudder pedal support, the operation panel mounting panel, the brace table mounting panel, be convenient for install the simulation flight peripheral hardware of different models, it is more convenient to use.
(2) The utility model discloses a set up the mounting hole of co-altitude not on fixed connector, the height at the difference is installed to the easy to assemble crossbeam to be convenient for adjust the angle of the slope of rudder pedal support, be convenient for adapt to different flight training personnel's use custom.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention.
Fig. 2 is a schematic view of the overall structure of the present invention at another angle.
Fig. 3 is an enlarged schematic view of a local structure of the middle console bracket of the present invention.
Fig. 4 is the structural schematic diagram of the first square supporting tube of the present invention.
Fig. 5 is a schematic structural view of the support platform of the present invention.
Fig. 6 is an enlarged schematic view of a local structure of the middle fixing connector of the present invention.
Wherein, the names corresponding to the reference numbers are:
1-supporting underframe, 2-fixed connecting piece, 3-mounting front beam, 4-mounting rear beam, 5-rudder pedal support, 6-operating platform support, 7-operating platform mounting plate, 8-supporting platform support, 9-supporting platform mounting plate, 10-reserved mounting hole, 11-mounting hole, 12-first supporting square tube, 13-manual knob, 14-second supporting square tube, 15-horizontal branch tube, 16-vertical section, 17-bending section, 18-inclined section, 19-inclined connecting section, 20-transition section, 21-horizontal section, 22-large L-shaped guard plate, 23-small L-shaped guard plate and 24-supporting column.
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. 1-6, the utility model discloses a simulation flight support, including supporting chassis 1, install a pair of fixed connector 2 on supporting chassis 1's the left and right sides frame, set up in the installation front beam 3 that supports 1 front end of chassis, set up installation back beam 4 between two fixed connector 2, one end is connected on installation front beam 3 and the other end is connected in the rudder pedal support 5 of installation back beam, correspond two operation panel supports 6 of installing on two fixed connector 2 respectively, set up operation panel mounting panel 7 on two operation panel supports 6, connect brace table support 8 on every operation panel support 6, and install brace table mounting panel 9 on brace table support 8. And, support columns 24 are further arranged at four corners of the bottom end of the support chassis 1, so that abrasion of the support chassis during simulation use of the device is reduced. Wherein, the foot rudder pedal bracket 5 is fixedly connected with the mounting front beam 3 and the mounting rear beam 4.
The utility model discloses in, all be provided with the reservation mounting hole 10 that adapts to multiple flight peripheral hardware on rudder pedal support 5, operation panel mounting panel 7, the brace table mounting panel 9, the flight peripheral hardware of the different models of installation of being convenient for uses more conveniently. The foot rudder pedal bracket 5 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.
In this embodiment, the supporting platform bracket 8 includes an inclined connecting section 19 vertically connected to the second supporting square pipe 14 by screw fixation, a transition section 20 connected to the inclined connecting section 19 for the supporting platform bracket 8 to transition to the horizontal direction, and a horizontal section 21 connected to the other end of the transition section 20; wherein, the supporting platform mounting plate 9 is fixedly connected with the horizontal section 21 through screws. The support table mounting plate 9 is divided into a left support table mounting plate and a right support table mounting plate, and the left support table mounting plate 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. A Logitech X52 HOTAS rocker controller, a Logitech X56 HOTAS RGB rocker controller, a Thrustmaster A10C all-metal wart pig double-hand flight controller rocker and the like can be arranged on the right support platform mounting plate.
In this embodiment, the fixed connecting member 2 is formed by sequentially connecting a large L-shaped guard plate 22 and a small L-shaped guard plate 23, and the long side of the large L-shaped guard plate 22 is connected with the short side of the small L-shaped guard plate 23; wherein, the vertical section of the first square support tube 12 is connected between the large L-shaped guard plate 22 and a small L-shaped guard plate 23, and the gap formed by the large L-shaped guard plate 22 and the small L-shaped guard plate 23 in the surrounding manner of the rear mounting beam 4 extends outwards. The arrangement enables the vertical section of the first supporting square pipe 12 to be connected with the fixed connecting piece more stably. The fixed connecting pieces 2 are provided with a plurality of mounting holes 10 with different heights, and the mounting cross beam 3 is connected between the mounting holes 11 with the same height of the two fixed connecting pieces 2. Moreover, the mounting holes are arranged on the L-shaped guard plate 22 in an arc-shaped path, so that the inclination angle of the pedal bracket of the rudder is convenient to adjust, and the pedal bracket is convenient to adapt to the use habits of different flight training personnel.
In this embodiment, the console bracket 6 includes a first square supporting tube 12 mounted on the fixed connecting member, a second square supporting tube 14 adjustably connected to the first square supporting tube 12 by a manual knob 13, and a horizontal branch tube 15 connected to the second square supporting tube 14; the operation table mounting plate 7 is mounted on the horizontal branch pipe 15, and the support table bracket 8 is vertically connected to the middle of the second support square pipe 14. The first supporting square pipe 12 comprises a vertical section 16 connected with the fixed connecting piece 2, a bent section 17 connected with the vertical section 16 and bent towards one side of the simulation training personnel, and an inclined section 18 connected with the bent section 17 and inclined towards one side of the simulation training personnel; wherein the second square support tube 14 is connected to the inclined section 18 of the first square support tube 12. The structure of the first support square tube is more suitable for simulating training operation of a simulated flight support. 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.
In another embodiment, a steering column, such as a Honeycomb cellular alpha YOKE & switch panel Flight controller, is mounted to the left side of the center console, and a throttle, such as a Logitech Flight Yoke System throttle arc mount, is mounted to the right side of the center console.
Through the design, the utility model discloses a simulation flight support can freely dispose the visual ware support and the seat in flight simulation cabin, and the convenient simulation flight training personnel use flight simulation peripheral hardware. And, all be provided with the reservation mounting hole that adapts to multiple flight peripheral hardware on rudder pedal support, the operation panel mounting panel, the brace table mounting panel, be convenient for install the simulation flight peripheral hardware of different models, it is more convenient to use. 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 (7)

1. A simulated flight support is characterized by comprising a supporting chassis (1), a pair of fixed connecting pieces (2) arranged on left and right frames of the supporting chassis (1), a mounting front beam (3) arranged at the front end of the supporting chassis (1), a mounting rear beam (4) arranged between the two fixed connecting pieces (2), a foot-steering pedal support (5) with one end connected to the mounting front beam (3) and the other end connected to the mounting rear beam, two operating platform supports (6) respectively corresponding to the two fixed connecting pieces (2), operating platform mounting plates (7) arranged on the two operating platform supports (6), a support platform support (8) connected to each operating platform support (6) and a support platform (9) arranged on the support platform supports (8); the novel flight control device is characterized in that reserved mounting holes (10) suitable for various flight peripherals are formed in the foot rudder pedal support (5), the operating platform mounting plate (7) and the supporting platform mounting plate (9).
2. A simulated flight support according to claim 1, wherein the fixed connectors (2) are provided with a plurality of mounting holes (11) of different heights, and the mounting back beams (4) are connected between the mounting holes (11) of two fixed connectors (2) of equal height.
3. A simulated flight support according to claim 2, wherein the console support (6) comprises a first square support tube (12) mounted on a fixed connecting piece, a second square support tube (14) adjustably connected with the first square support tube (12) by a manual knob (13), and a horizontal branch tube (15) connected to the second square support tube (14); the operating platform mounting plate (7) is mounted on the horizontal branch pipe (15), and the support platform support (8) is vertically connected to the middle of the second support square pipe (14).
4. A simulated flight support according to claim 3, wherein the first square support tube (12) comprises a vertical section (16) connected with the fixed connecting piece (2), a bent section (17) connected with the vertical section (16) and bent to one side of the simulated trainee, and an inclined section (18) connected with the bent section (17) and inclined to one side of the simulated trainee; wherein, the second square supporting tube (14) is connected with the inclined section (18) of the first square supporting tube (12).
5. A simulated flight support according to claim 4, wherein the support platform support (8) comprises an inclined connecting section (19) vertically connected with the second support square pipe (14) through screw fixation, a transition section (20) connected with the inclined connecting section (19) and used for the support platform support (8) to transition to the horizontal direction, and a horizontal section (21) connected with the other end of the transition section (20); wherein, the supporting table mounting plate (9) is fixedly connected with the horizontal section (21) through screws.
6. A simulated flight support as claimed in claim 5, wherein the fixed connection member (2) is formed by a large L-shaped guard (22) and a small L-shaped guard (23) which are connected in series, and the long side of the large L-shaped guard (22) is connected with the short side of the small L-shaped guard (23); the vertical section of the first supporting square pipe (12) is connected between the large L-shaped guard plate (22) and the small L-shaped guard plate (23), and the gap formed by the large L-shaped guard plate (22) and the small L-shaped guard plate (23) in a surrounding mode of the mounting back beam (4) extends outwards.
7. A simulated flight support according to claim 6, characterised in that support posts (24) are also provided at the four corners of the bottom end of the support chassis (1).
CN202021290963.7U 2020-07-03 2020-07-03 Simulated flight support Active CN212256639U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202021290963.7U CN212256639U (en) 2020-07-03 2020-07-03 Simulated flight support

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202021290963.7U CN212256639U (en) 2020-07-03 2020-07-03 Simulated flight support

Publications (1)

Publication Number Publication Date
CN212256639U true CN212256639U (en) 2020-12-29

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ID=73980519

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CN202021290963.7U Active CN212256639U (en) 2020-07-03 2020-07-03 Simulated flight support

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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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TR01 Transfer of patent right

Effective date of registration: 20240602

Address after: Room 608, block B, 35 Changjiang South Road, Xinwu District, Wuxi City, Jiangsu Province

Patentee after: Weifei Technology Co.,Ltd.

Country or region after: China

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

Patentee before: Xi'an Weifei Simulation Technology Co.,Ltd.

Country or region before: China