CN204857033U - Flexible passenger cabin of simulator flight - Google Patents
Flexible passenger cabin of simulator flight Download PDFInfo
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- CN204857033U CN204857033U CN201520626863.XU CN201520626863U CN204857033U CN 204857033 U CN204857033 U CN 204857033U CN 201520626863 U CN201520626863 U CN 201520626863U CN 204857033 U CN204857033 U CN 204857033U
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Abstract
The utility model relates to an aircraft simulation engineering technical field, concretely relates to flexible passenger cabin of simulator flight, including well accuse platform, well accuse platform is including well accuse platform skeleton, well accuse platform skeleton is including a plurality of mutual parallel arrangement's well accuse platform stand, be connected with a plurality of well accuse platform horizontal poles between the well accuse platform stand, be provided with panel and/or instrument and/or avionics on the well accuse platform skeleton, well accuse platform horizontal pole divide into the first horizontal pole and vertical first vertical pole that sets up of horizontal setting according to its orientation, first horizontal pole is extending structure, makes well accuse platform skeleton is being followed the ascending length in first horizontal pole side can be adjusted. In the above -mentioned scheme of this application, regulation that can be through to first horizontal pole length is controlled the size of whole storehouse seat, and then is makeed the flexible passenger cabin of simulator flight of this application can be applicable to different models, simulator flight passenger cabin that convenient man -machine engineering was verified.
Description
Technical field
The utility model relates to plane simulation field of engineering technology, is specifically related to the flexible passenger cabin of a kind of simulator flight.
Background technology
Aircraft engineering simulator is a kind of professional flight system emulation platform, it mainly comprises the analog capsule cabin of flight simulator, boiler-plate seat inside is provided with operating control, instrument, signal apparatus etc., these devices are identical with the structure in real aircraft passenger cabin with instrument, and work is also identical with real aircraft with instruction situation.
Pilot in analog capsule cabin, among the passenger cabin of the true aircraft that coexists.When the various maneuvering device jociey stick of pilot guidance, throttle, switch etc., not only various instrument, the relevant work of signal lamp energy, and the sound that relevant device sends can also be heard, and the sound of external environment.Meanwhile, the hand of pilot and pin can also there is the power sense produced because of operating aircraft.
Above-mentioned aircraft engineering analog machine is used for the research of course of new aircraft, experiment and the improvement to existing aircraft, its cockpit configuration is consistent with aircraft, control platform before being generally divided into, console, side control platform, although the simulation actual operating condition that the analog capsule cabin of said structure can be good, it still also exists deficiency, imbody in the following areas:
Traditional project analog machine passenger cabin is only customized for a certain or a certain class type, can not be applicable to the testing research of other types; And need in the research process of course of new aircraft to verify human factor engineering, traditional cockpit design is fixed, and is not easy to further improvement; Studying course of new aircraft, to test and in process that existing aircraft improves, can frequently change or increase and decrease panel, but traditional passenger cabin due to its configuration fixing, so in Renewal process, traditional passenger cabin is difficult to meet instrument, avionics and panel size change requirement.
Based on above-mentioned, need one at present badly and can be applicable to different type of machines, the plane simulation passenger cabin facilitating human factor engineering to verify.
Utility model content
The purpose of this utility model is: the problems referred to above existed for current plane simulation passenger cabin, provide one to be applicable to different type of machines, the simulator flight passenger cabin facilitating human factor engineering to verify.
To achieve these goals, the technical solution adopted in the utility model is:
The flexible passenger cabin of a kind of simulator flight, comprise console, described console includes console skeleton, described console skeleton includes some console columns arranged in parallel, some console cross bars are connected with between described console column, described console skeleton is provided with panel and/or instrument and/or avionics, the first vertical pole that described console cross bar is arranged towards the first cross bar and longitudinal direction that are divided into horizontally set according to it, described first cross bar is stretching structure, and described console skeleton can be conditioned along the length on described first cross bar direction.
In the such scheme of the application, because the first cross bar is stretching structure, so make console skeleton can be conditioned along the length on described first cross bar direction, when panel and/or instrument and/or avionics are when changing along the size on the first cross bar direction, can by the length of adjustment first cross bar, with the change in size enabling console skeleton be adapted to panel and/or instrument and/or avionics, and, can by the adjustment to the first cross bar length, control the size of whole storehouse seat, and then make the flexible passenger cabin of the simulator flight of the application to be applicable to different type of machines, the simulator flight passenger cabin facilitating human factor engineering to verify.
As the preferred version of the application, first cross bar described in each root all includes at least two first cross bar sections, dismountablely between adjacent two first cross bar sections be connected with the first cross bar extension element, different by described first cross bar sections and described first cross bar extension element link position, control described console skeleton along the length on described first cross bar direction.
As the preferred version of the application, described first cross bar sections is the fit depressions of tool reeded C shape section bar, described first cross bar extension element and described first cross bar sections.
In the such scheme of the application, the first cross bar extension element is arranged in the groove of the first cross bar sections, facilitates the adjustment of the first cross bar length, avoids in adjustment process, and the first cross bar extension element is from landing the first cross bar.
As the preferred version of the application, first vertical pole described in each root all includes at least two first vertical pole sections, dismountablely between adjacent two first vertical pole sections be connected with the first vertical pole extension element, different by described first vertical pole sections and described first vertical pole extension element link position, control described console skeleton along the length on described first vertical pole direction.
In the such scheme of the application, first vertical pole is also set to stretching structure, the console skeleton of the application can be conditioned along the length on the first vertical pole direction, when panel and/or instrument and/or the size of avionics on the first vertical pole direction change, can by the length of adjustment first vertical pole, with the change in size enabling console skeleton be adapted to panel and/or instrument and/or avionics, so, further improve the adaptability of the flexible passenger cabin of simulator flight of the application.
As the preferred version of the application, described first vertical pole sections is the fit depressions of tool reeded C shape section bar, described first vertical pole extension element and described first vertical pole sections.
As the preferred version of the application, control platform before the flexible passenger cabin of described simulator flight also includes, before described, platform is rotating is arranged on described console in control, and the central axis that before described, control platform rotates parallels with described first cross bar.
In the such scheme of the application, front control platform can rotate relative to console, front control platform can be adjusted to according to causing the operating position of personnel the position being most suited to operating personnel and using, further facilitate the flexible passenger cabin engineering simulation test of the application's simulator flight to verify with ergonomic.
As the preferred version of the application, before described, control platform controls platform skeleton and at least two support rails before including, before described, control platform skeleton is provided with panel and/or instrument and/or avionics, one end of described support rail is hinged on described console skeleton, the other end is dismountable is connected with vertical supporting rod, and described vertical supporting rod is vertically arranged on described console skeleton.
In the such scheme of the application, one end of support rail is hinged on described console skeleton, the other end is dismountable is connected with vertical supporting rod, vertical supporting rod is vertically arranged on console skeleton, when removing the connection between support rail and vertical supporting rod, support rail can rotate around hinged end, when support rail turns to desired location, again support rail is fixedly connected with vertical supporting rod, realize the adjustment to support rail, and then the rotation realized by controlling support rail, the rotation of control platform before controlling.
As the preferred version of the application, before described, control platform skeleton comprises some front control platform columns arranged in parallel, some front control platform cross bars are connected with between control platform column before described, platform cross bar is controlled according to it towards the second vertical pole being divided into the second cross bar of horizontally set and longitudinally arrange before described, described second cross bar is stretching structure, and described front control platform skeleton can be conditioned along the length on described second cross bar direction.
In this application, by the second cross bar is set to stretching structure, before making, control platform skeleton also can be conditioned along the length on the second cross bar direction, and then the adaptability of the flexible passenger cabin of the simulator flight that further improve the application.
As the preferred version of the application, second cross bar described in each root all includes at least two second cross bar sections, dismountablely between adjacent two second cross bar sections be connected with the second cross bar extension element, different by described second cross bar sections and described second cross bar extension element link position, control described before control platform skeleton along the length on described second cross bar direction.
As the preferred version of the application, the flexible passenger cabin of described simulator flight also includes shading platform, and described shading platform is arranged on described front control platform.
In this application, before being arranged on by shading platform on control platform, because front control platform is rotatable, and then shading platform also can be rotated with front control platform, further improve the controllability of the flexible passenger cabin of the application's simulator flight.
As the preferred version of the application, described shading platform is provided with shading platform fixture, correspondingly with described shading platform fixture on described support rail is provided with chute, described shading platform fixture is slidably arranged in described chute.
In sum, owing to have employed technique scheme, the beneficial effect of the application is:
Because the first cross bar is stretching structure, so make console skeleton can be conditioned along the length on described first cross bar direction, when panel and/or instrument and/or avionics are when changing along the size on the first cross bar direction, can by the length of adjustment first cross bar, with the change in size enabling console skeleton be adapted to panel and/or instrument and/or avionics, and, can by the adjustment to the first cross bar length, control the size of whole storehouse seat, and then make the flexible passenger cabin of the simulator flight of the application to be applicable to different type of machines, the simulator flight passenger cabin facilitating human factor engineering to verify.
Accompanying drawing explanation
Fig. 1 is the structural representation of the application;
Fig. 2 is the structural representation of the application's console skeleton and front control platform skeleton;
Fig. 3 is the structural representation before removing in Fig. 2 after control platform skeleton;
Fig. 4 is the partial enlarged drawing at A place in Fig. 2;
Fig. 5 is the partial enlarged drawing at B place in Fig. 2,
Mark in figure: 1-console, 2-console skeleton, 3-console column, 4-console cross bar, 5-first cross bar, 6-first vertical pole, 7-first cross bar extension element, 8-first cross bar sections, 9-first vertical pole sections, control platform before 10-, 11-support rail, control platform skeleton before 12-, 13-vertical supporting rod, control platform column before 14-, control platform cross bar before 15-, 16-second cross bar, 17-second vertical pole, 18-second cross bar sections, 19-second cross bar extension element, 20-shading platform, 21-shading platform fixture, 22-chute, 23-panel, 24-instrument, 25-avionics, 26-first vertical pole extension element.
Embodiment
Below in conjunction with accompanying drawing, the utility model is described in detail.
In order to make the purpose of this utility model, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the utility model is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
Embodiment 1:
As Figure 1-5, the flexible passenger cabin of a kind of simulator flight, comprise console 1, described console 1 includes console skeleton 2, described console skeleton 2 includes some console columns 3 arranged in parallel, some console cross bars 4 are connected with between described console column 3, described console skeleton 2 is provided with panel 23 and/or instrument 24 and/or avionics 25, the first vertical pole 6 that described console cross bar 4 is arranged towards the first cross bar 5 and longitudinal direction that are divided into horizontally set according to it, described first cross bar 5 is stretching structure, described console skeleton 2 can be conditioned along the length on described first cross bar 5 direction.
In the such scheme of the present embodiment, because the first cross bar 5 is stretching structure, so make console skeleton 2 can be conditioned along the length on described first cross bar 5 direction, when panel 23 and/or instrument 24 and/or avionics 25 are when changing along the size on the first cross bar 5 direction, can by the length of adjustment first cross bar 5, with the change in size making console skeleton 2 can be adapted to panel 23 and/or instrument 24 and/or avionics 25, and, can by the adjustment to the first cross bar 5 length, control the size of whole storehouse seat, and then make the flexible passenger cabin of the simulator flight of the present embodiment to be applicable to different type of machines, the simulator flight passenger cabin facilitating human factor engineering to verify.
Embodiment 2:
As Figure 1-5, passenger cabin as described in Example 1, first cross bar 5 described in each root all includes at least two first cross bar sections 8, dismountablely between adjacent two first cross bar sections 8 be connected with the first cross bar extension element 7, different by described first cross bar sections 8 and described first cross bar extension element 7 link position, control described console skeleton 2 along the length on described first cross bar 5 direction, described first cross bar sections 8 is tool reeded C shape section bar, the fit depressions of described first cross bar extension element 7 and described first cross bar sections 8.
In the such scheme of the present embodiment, the first cross bar extension element 7 is arranged in the groove of the first cross bar sections 8, facilitates the adjustment of the first cross bar 5 length, avoids in adjustment process, and the first cross bar extension element 7 is from landing the first cross bar 5.
Embodiment 3:
As Figure 1-5, passenger cabin as described in Example 1, first vertical pole 6 described in each root all includes at least two first vertical pole sections 9, dismountablely between adjacent two first vertical pole sections 9 be connected with the first vertical pole extension element 26, different by described first vertical pole sections 9 and described first vertical pole extension element 26 link position, control described console skeleton 2 along the length on described first vertical pole 6 direction, described first vertical pole sections 9 is tool reeded C shape section bar, the fit depressions of described first vertical pole extension element 26 and described first vertical pole sections 9.
In the such scheme of the present embodiment, first vertical pole 6 is also set to stretching structure, the console skeleton 2 of the present embodiment can be conditioned along the length on the first vertical pole 6 direction, when panel 23 and/or instrument 24 and/or the size of avionics 25 on the first vertical pole 6 direction change, can by the length of adjustment first vertical pole 6, with the change in size making console skeleton 2 can be adapted to panel 23 and/or instrument 24 and/or avionics 25, so, further improve the adaptability of the flexible passenger cabin of simulator flight of the present embodiment.
Embodiment 4:
As Figure 1-5, passenger cabin as described in Example 1, control platform 10 before the flexible passenger cabin of described simulator flight also includes, before described, platform 10 is rotating is arranged on described console 1 in control, the central axis that before described, control platform 10 rotates parallels with described first cross bar 5, before described, control platform 10 controls platform skeleton 12 and at least two support rails 11 before including, before described, control platform skeleton 12 is provided with panel 23 and/or instrument 24 and/or avionics 25, one end of described support rail 11 is hinged on described console skeleton 2, the other end is dismountable is connected with vertical supporting rod 13, described vertical supporting rod 13 is vertically arranged on described console skeleton 2, before described, control platform skeleton 12 comprises some front control platform columns 14 arranged in parallel, some front control platform cross bars 15 are connected with between control platform column 14 before described, platform cross bar 15 is controlled according to it towards the second cross bar 16 being divided into horizontally set and the second vertical pole 17 longitudinally arranged before described, described second cross bar 16 is stretching structure, described front control platform skeleton 12 can be conditioned along the length on described second cross bar 16 direction, second cross bar 16 described in each root all includes at least two second cross bar sections 18, dismountablely between adjacent two second cross bar sections 18 be connected with the second cross bar extension element 19, different by described second cross bar sections 18 and described second cross bar extension element 19 link position, control described before control platform skeleton 12 along the length on described second cross bar 16 direction, the flexible passenger cabin of described simulator flight also includes shading platform 20, described shading platform 20 is arranged on described front control platform 10, described shading platform 20 is provided with shading platform fixture 21, correspondingly with described shading platform fixture 21 on described support rail 11 be provided with chute 22, described shading platform fixture 21 is slidably arranged in described chute 22.
In the such scheme of the present embodiment, front control platform 10 can rotate relative to console 1, front control platform 10 can be adjusted to according to causing the operating position of personnel the position being most suited to operating personnel and using, the flexible passenger cabin engineering simulation test of the present embodiment simulator flight is further facilitated to verify with ergonomic, in the present embodiment, one end of support rail 11 is hinged on described console skeleton 2, the other end is dismountable is connected with vertical supporting rod 13, vertical supporting rod 13 is vertically arranged on console skeleton 2, when removing the connection between support rail 11 and vertical supporting rod 13, support rail 11 can rotate around hinged end, when support rail 11 turns to desired location, again support rail 11 is fixedly connected with vertical supporting rod 13, realize the adjustment to support rail 11, by controlling the rotation of support rail 11, and then before controlling, control the rotation of platform 10, by the second cross bar 16 is set to stretching structure, before making, control platform skeleton 12 also can be conditioned along the length on the second cross bar 16 direction, and then the adaptability of the flexible passenger cabin of the simulator flight that further improve the present embodiment, before shading platform 20 is arranged on control platform 10, because front control platform 10 is rotatable, and then shading platform 20 also can be rotated with front control platform 10, further improve the controllability of the flexible passenger cabin of the present embodiment simulator flight.
All do within spirit of the present utility model and principle any amendment, equivalent to replace and improvement etc., all should be included within protection domain of the present utility model.
Claims (10)
1. the flexible passenger cabin of simulator flight, comprise console, described console includes console skeleton, described console skeleton includes some console columns arranged in parallel, some console cross bars are connected with between described console column, described console skeleton is provided with panel and/or instrument and/or avionics, it is characterized in that: the first vertical pole that described console cross bar is arranged towards the first cross bar and longitudinal direction that are divided into horizontally set according to it, described first cross bar is stretching structure, described console skeleton can be conditioned along the length on described first cross bar direction.
2. the flexible passenger cabin of simulator flight according to claim 1, it is characterized in that: the first cross bar described in each root all includes at least two first cross bar sections, dismountablely between adjacent two first cross bar sections be connected with the first cross bar extension element, different by described first cross bar sections and described first cross bar extension element link position, control described console skeleton along the length on described first cross bar direction.
3. the flexible passenger cabin of simulator flight according to claim 2, is characterized in that: described first cross bar sections is the fit depressions of tool reeded C shape section bar, described first cross bar extension element and described first cross bar sections.
4. the flexible passenger cabin of simulator flight according to claim 1, it is characterized in that: the first vertical pole described in each root all includes at least two first vertical pole sections, dismountablely between adjacent two first vertical pole sections be connected with the first vertical pole extension element, different by described first vertical pole sections and described first vertical pole extension element link position, control described console skeleton along the length on described first vertical pole direction.
5. the flexible passenger cabin of simulator flight according to claim 4, is characterized in that: described first vertical pole sections is the fit depressions of tool reeded C shape section bar, described first vertical pole extension element and described first vertical pole sections.
6. the flexible passenger cabin of the simulator flight according to claim 1-5 any one, it is characterized in that: control platform before the flexible passenger cabin of described simulator flight also includes, before described, platform is rotating is arranged on described console in control, and the central axis that before described, control platform rotates parallels with described first cross bar.
7. the flexible passenger cabin of simulator flight according to claim 6, it is characterized in that: before described, control platform controls platform skeleton and at least two support rails before including, before described, control platform skeleton is provided with panel and/or instrument and/or avionics, one end of described support rail is hinged on described console skeleton, the other end is dismountable is connected with vertical supporting rod, and described vertical supporting rod is vertically arranged on described console skeleton.
8. the flexible passenger cabin of simulator flight according to claim 7, it is characterized in that: before described, control platform skeleton comprises some front control platform columns arranged in parallel, some front control platform cross bars are connected with between control platform column before described, platform cross bar is controlled according to it towards the second vertical pole being divided into the second cross bar of horizontally set and longitudinally arrange before described, described second cross bar is stretching structure, and described front control platform skeleton can be conditioned along the length on described second cross bar direction.
9. the flexible passenger cabin of simulator flight according to claim 8, it is characterized in that: the second cross bar described in each root all includes at least two second cross bar sections, dismountablely between adjacent two second cross bar sections be connected with the second cross bar extension element, different by described second cross bar sections and described second cross bar extension element link position, control described before control platform skeleton along the length on described second cross bar direction.
10. the flexible passenger cabin of simulator flight according to claim 6, is characterized in that: the flexible passenger cabin of described simulator flight also includes shading platform, and described shading platform is arranged on described front control platform.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520626863.XU CN204857033U (en) | 2015-08-19 | 2015-08-19 | Flexible passenger cabin of simulator flight |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520626863.XU CN204857033U (en) | 2015-08-19 | 2015-08-19 | Flexible passenger cabin of simulator flight |
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| CN204857033U true CN204857033U (en) | 2015-12-09 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112598958A (en) * | 2020-12-17 | 2021-04-02 | 中国航空综合技术研究所 | Flexible simulation cabin man-machine work efficiency test system and evaluation method thereof |
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2015
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112598958A (en) * | 2020-12-17 | 2021-04-02 | 中国航空综合技术研究所 | Flexible simulation cabin man-machine work efficiency test system and evaluation method thereof |
| CN112598958B (en) * | 2020-12-17 | 2022-08-05 | 中国航空综合技术研究所 | Flexible simulation cabin man-machine work efficiency test system and evaluation method thereof |
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Address after: 610042 No. 846, south section, Tianfu Road, Huayang street, Tianfu New District, Sichuan, Chengdu Patentee after: Chengdu Hermes Polytron Technologies Inc Address before: 610200 No. 846, south section, Tianfu Road, Huayang street, Tianfu New District, Sichuan, Chengdu Patentee before: CHENGDU HERMES TECHNOLOGY CO., LTD. |