CN203366576U - A top platform body structure of a flight simulator six-degree-of-freedom platform - Google Patents
A top platform body structure of a flight simulator six-degree-of-freedom platform Download PDFInfo
- Publication number
- CN203366576U CN203366576U CN 201320390613 CN201320390613U CN203366576U CN 203366576 U CN203366576 U CN 203366576U CN 201320390613 CN201320390613 CN 201320390613 CN 201320390613 U CN201320390613 U CN 201320390613U CN 203366576 U CN203366576 U CN 203366576U
- Authority
- CN
- China
- Prior art keywords
- main frame
- flight simulator
- body structure
- platform body
- degree
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Landscapes
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
Abstract
The utility model relates to a top platform body structure of a flight simulator six-degree-of-freedom platform. The top platform body structure is a discrete structure and comprises a main frame, a left frame, a right frame, front ball curtain supports, and a rear tail cabin frame, a supporting rack, a seat cabin supporting rack, apron boards, and a bottom cover. The left frame, the right frame, the front ball curtain supports, and the rear tail cabin frame are connected with the four sides of the main frame. The supporting rack and the seat cabin supporting rack are connected in the main frame in a supporting manner. The apron boards and the bottom cover are connected with the outer side and the bottom of the main frame. Compared with a product in the prior art, the top platform body structure is produced by using a light alloy split producing method. An original large-size top platform body difficult to transport, assemble, and maintain is divided into a plurality of modules. Each module has a relatively small size and is easy to transport, assemble, and maintain. In addition, because light alloy material is used, the weight of the top platform body is decreased and the moving quality of the flight simulator is increased.
Description
Technical field
The utility model relates to and is applicable to various large-scale flight simulator six-freedom motion system upper platform bodies, especially relates to a kind of flight simulator six degree of freedom platform upper platform body structure.
Background technology
At present, the six degree of freedom platform is widely used in the flight simulator kinematic system, it for flight simulator provide lifting, side direction, vertically, motion in pitching, roll, driftage six-freedom degree.It by motion upper mounting plate, fixed base and an end by ball pivot, an end by universal six motions that ACTUATOR forms that are hinged.Simulator is arranged on motion platform, along with the motion of motion platform, moves.Upper platform body should realize the motion of six degree of freedom platform, is again the pedestal of carrying flight simulator.The upper platform body of existing domestic and international large-scale flight simulator adopts structural shapes or the welding of rectangular tube grid structure to manufacture more, adopt the upper mounting plate of structural shapes welding exist from great, be difficult for the problem such as transportation, and there is the problem that complex structure, manufacturing process are loaded down with trivial details, can utilize space parallax in the upper mounting plate of employing rectangular tube grid structure.
The utility model content
The purpose of this utility model is exactly to provide a kind of in order to overcome the defect that above-mentioned prior art exists.
The purpose of this utility model can be achieved through the following technical solutions:
A kind of flight simulator six degree of freedom platform upper platform body structure, be separated structure, comprises
Main frame,
Left border, Right Border, the forecourt curtain that is connected to the main frame surrounding supports, rear deck store framework,
Bracing frame and the passenger cabin bracing frame of support and connection in main frame,
Be connected to skirtboard and the bottom of the main frame outside and bottom.
Described main frame is comprised of anterior framework and rear portion framework two parts, and described rear portion framework is inserted in anterior framework and through bolted.
Described left border and Right Border respectively have four, are separately positioned on the left and right sides of main frame, and correspondence is arranged on the fixed position of the structural flight simulator of stage body.
Described rear deck store framework is comprised of six installing plates, all with the rear portion framework that forms main frame, is connected fastening.
Place the work chamber of flight simulator on described rear deck store framework.
Described passenger cabin bracing frame is fixedly connected in the anterior framework that forms main frame.
Described skirtboard supports through being bolted to left border, Right Border, forecourt curtain, after the deck store frame form the motion platform upper platform body.
Compared with prior art, the utility model adopts the split type manufacture method manufacture of light-duty alloy, make originally bulky, transportation, assembling, safeguard that all very difficult upper platform body is broken down into some, modules volume less, be convenient to transportation, assembling and safeguard.Owing to adopting light-duty alloy material, alleviate the weight of upper platform body in addition, improved the motion quality of flight simulator.
The accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is decomposition texture schematic diagram of the present utility model;
The mounting structure schematic diagram that Fig. 3 is main frame.
In figure, 1 be main frame, 11 for anterior framework, 12 for the rear portion framework, 2 for Right Border, 3 for left border, 4 for bracing frame, 5 for the forecourt curtain support, 6 for rear deck store framework, 7 for passenger cabin bracing frame, 8 be skirtboard.
Embodiment
Below in conjunction with the drawings and specific embodiments, the utility model is elaborated.
Embodiment
A kind of flight simulator six degree of freedom platform upper platform body structure, its structure as shown in Figure 1-2, this upper platform body structure is separated structure, comprise main frame 1, be connected to left border 3, Right Border 2, forecourt curtain support 5, the rear deck store framework 6 of main frame 1 surrounding, bracing frame 4 and the passenger cabin bracing frame 7 of support and connection in main frame 1, be connected to skirtboard 8 and the bottom of main frame 1 outside and bottom in addition.
The structure of main frame 1 as shown in Figure 3, is comprised of anterior framework 11 and rear portion framework 12 two parts, and rear portion framework 12 is inserted in anterior framework 11 and connects fastening through the hexagon head hinged bolts of 2 groups of M24.For making anterior framework 11 and rear portion framework 12 not produce deformation, can also install gusset additional around the corner.Anterior framework 11 center sections are reserved with the space of 2100mm * 2000mm, and passenger cabin bracing frame 7 is fixed in this space, and passenger cabin bracing frame 7 is mainly used in laying the passenger cabin of flight simulator.Bracing frame 4 one ends are fixed on anterior framework 11 with hinged bolts, and an end is fixed on rear portion framework 12.
Claims (7)
1. a flight simulator six degree of freedom platform upper platform body structure, is characterized in that, this stage body structure is separated structure, comprises
Main frame,
Left border, Right Border, the forecourt curtain that is connected to the main frame surrounding supports, rear deck store framework,
Bracing frame and the passenger cabin bracing frame of support and connection in main frame,
Be connected to skirtboard and the bottom of the main frame outside and bottom.
2. a kind of flight simulator six degree of freedom platform upper platform body structure according to claim 1, is characterized in that, described main frame is comprised of anterior framework and rear portion framework two parts, and described rear portion framework is inserted in anterior framework and through bolted.
3. a kind of flight simulator six degree of freedom platform upper platform body structure according to claim 1, it is characterized in that, described left border and Right Border respectively have four, are separately positioned on the left and right sides of main frame, and correspondence is arranged on the fixed position of the structural flight simulator of stage body.
4. a kind of flight simulator six degree of freedom platform upper platform body structure according to claim 2, is characterized in that, described rear deck store framework is comprised of six installing plates, all with the rear portion framework that forms main frame, is connected fastening.
5. according to the described a kind of flight simulator six degree of freedom platform upper platform body structure of claim 1 or 4, it is characterized in that, place the work chamber of flight simulator on described rear deck store framework.
6. a kind of flight simulator six degree of freedom platform upper platform body structure according to claim 2, is characterized in that, described passenger cabin bracing frame is fixedly connected in the anterior framework that forms main frame.
7. a kind of flight simulator six degree of freedom platform upper platform body structure according to claim 1, is characterized in that, described skirtboard supports through being bolted to left border, Right Border, forecourt curtain, after the deck store frame form the motion platform upper platform body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320390613 CN203366576U (en) | 2013-07-02 | 2013-07-02 | A top platform body structure of a flight simulator six-degree-of-freedom platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320390613 CN203366576U (en) | 2013-07-02 | 2013-07-02 | A top platform body structure of a flight simulator six-degree-of-freedom platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203366576U true CN203366576U (en) | 2013-12-25 |
Family
ID=49814309
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320390613 Expired - Fee Related CN203366576U (en) | 2013-07-02 | 2013-07-02 | A top platform body structure of a flight simulator six-degree-of-freedom platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203366576U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106365041A (en) * | 2015-07-20 | 2017-02-01 | 北京卫星环境工程研究所 | Space mechanical arm lifting transferring apparatus having high-precision pose maintaining function |
| CN106530895A (en) * | 2017-01-12 | 2017-03-22 | 北京航宇荣康科技股份有限公司 | High-intensity large field-of-view dome screen real image display system |
| CN112885188A (en) * | 2021-04-09 | 2021-06-01 | 北京摩诘创新科技股份有限公司 | Upper platform applied to flight simulator |
-
2013
- 2013-07-02 CN CN 201320390613 patent/CN203366576U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106365041A (en) * | 2015-07-20 | 2017-02-01 | 北京卫星环境工程研究所 | Space mechanical arm lifting transferring apparatus having high-precision pose maintaining function |
| CN106530895A (en) * | 2017-01-12 | 2017-03-22 | 北京航宇荣康科技股份有限公司 | High-intensity large field-of-view dome screen real image display system |
| CN112885188A (en) * | 2021-04-09 | 2021-06-01 | 北京摩诘创新科技股份有限公司 | Upper platform applied to flight simulator |
| CN112885188B (en) * | 2021-04-09 | 2023-07-25 | 北京摩诘创新科技股份有限公司 | Upper platform applied to flight simulator |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203366576U (en) | A top platform body structure of a flight simulator six-degree-of-freedom platform | |
| CN102581615B (en) | Flexible tool set platform for rear section of integral wing-body structure | |
| CN202152007U (en) | Supporting device for various engines | |
| CN103192882B (en) | Framework type frame structure and concrete pump truck | |
| CN202367734U (en) | Engine lifting device | |
| CN203583959U (en) | Tray anti-swing device for traversing frame of stereo garage | |
| CN203267707U (en) | Automobile front leaf spring rear bracket | |
| CN202684401U (en) | Monocoque bus body skeleton assembling equipment | |
| CN211968884U (en) | UV flatbed printer | |
| CN202726424U (en) | Large-size shell assembling mould base | |
| CN203867238U (en) | Photovoltaic power generating device mounted on top of double-layer parking platform and capable of tracking sunlight | |
| CN103406888B (en) | Holder for automobile cabin stringer | |
| CN204968914U (en) | Hatching of hatch machine goes out young convertible car | |
| CN203739625U (en) | Passenger car and cooling device of engine of passenger car | |
| CN203358647U (en) | Revolving frame for finished automobile fairing | |
| CN206925833U (en) | A kind of apparatus for placing for the fastener for assembling vehicle frame | |
| CN202345417U (en) | Instrument table assembly | |
| CN105882787A (en) | Multi-purpose transportation trailer | |
| CN201321739Y (en) | Liftable stereo garage with double supporting plates | |
| CN204039002U (en) | A kind of folded form aerial platform | |
| CN219747952U (en) | Side wall storage rack of passenger car | |
| CN211192670U (en) | Rail transit locomotive top skeleton welding strutting arrangement | |
| CN203793645U (en) | Body supporting structure of four-axis aircraft | |
| CN203078613U (en) | Carriage top portion corner section bar of aluminium alloy carriage type transport semitrailer | |
| CN103863549B (en) | A kind of four axle unmanned vehicle supporting fuselage assemblies |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20131225 Termination date: 20170702 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |