CN212084431U - Flight simulator cockpit frame structure - Google Patents
Flight simulator cockpit frame structure Download PDFInfo
- Publication number
- CN212084431U CN212084431U CN201922112531.0U CN201922112531U CN212084431U CN 212084431 U CN212084431 U CN 212084431U CN 201922112531 U CN201922112531 U CN 201922112531U CN 212084431 U CN212084431 U CN 212084431U
- Authority
- CN
- China
- Prior art keywords
- support connection
- plate
- rear end
- frame
- flight simulator
- 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.)
- Active
Links
Images
Landscapes
- Body Structure For Vehicles (AREA)
Abstract
The utility model discloses a flight simulator cockpit frame construction, including front end frame subassembly, many perpendicular honing strips, many long horizontal honing strips and rear end frame subassembly, form through first nut, first screw and angle aluminium combination between front end frame subassembly, many perpendicular honing strips, many long horizontal honing strips and the rear end frame subassembly. The utility model discloses the frame is not only structural strength reliable, dismantle with convenient assembling, be convenient for transport, and the cost is cheap moreover, and after the covering was laid to the frame simultaneously, cockpit size appearance and feel were very close with the fixed wing aircraft, and operating space is big, and the structure excellent performance can make the user possess good flight experience effect.
Description
Technical Field
The utility model relates to a flight simulator cockpit frame construction belongs to flight simulator structural design technical field, especially a flight simulator cockpit structure of fixed wing aircraft.
Background
Along with the continuous development and the popularization of science and technology, people also have higher and higher requirements on experience of flying products, wherein the cockpit is in the middle of the experience of the flight simulator, and the cockpit of the flight simulator in the current market is formed by opening the mold through composite materials.
However, the composite material is subjected to mold opening, so that the size and the appearance of the cockpit can be well guaranteed, the mold opening cost is very high, the size of the cockpit is large, and the cockpit is inconvenient to disassemble and transport. The whole manufacturing cost of the flight simulator is increased, so that a user needs to spend more price for experience, and the frame structure of the flight simulator cockpit is designed at present, so that the frame structure not only has excellent structural strength, but also has texture and size close to those of a real aircraft after being paved with a skin, and is low in manufacturing cost and convenient to detach and transport.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the defects of higher production cost, inconvenient disassembly and transportation in the prior art, thereby providing a flight simulator cockpit frame structure.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides a flight simulator cockpit frame construction, includes front end frame subassembly, many perpendicular honing strips, many long horizontal honing strips and rear end frame subassembly, form through first nut, first screw and angle aluminium combination between front end frame subassembly, many perpendicular honing strips, many long horizontal honing strips and the rear end frame subassembly.
Preferably, the front frame assembly comprises a front firewall, a front connecting frame plate, a supporting connecting sheet A, a supporting connecting sheet B, a supporting connecting sheet C, a supporting connecting sheet D, a supporting connecting sheet E and a supporting connecting sheet F, wherein the supporting connecting sheet A, the supporting connecting sheet B, the supporting connecting sheet C, the supporting connecting sheet D, the supporting connecting sheet E and the supporting connecting sheet F are all fixed with the front firewall through rivets.
Preferably, the rear end frame assembly comprises a rear end connecting flat plate, a rear end connecting frame plate, a supporting connecting piece H, a supporting connecting piece I, a supporting connecting piece J, a supporting connecting piece K, a supporting connecting piece L, a supporting connecting piece M and a supporting connecting piece N, and the supporting connecting piece H, the supporting connecting piece I, the supporting connecting piece J, the supporting connecting piece K, the supporting connecting piece L, the supporting connecting piece M and the supporting connecting piece N are all fixed with the rear end connecting flat plate through rivets.
Preferably, the vertical honing strip and the long and transverse honing strip are fixedly connected with the front end frame assembly and the rear end frame assembly through angle aluminum, a first nut and a first screw.
Preferably, the front-end firewall is of a D-type; the front end connecting frame plate is C-shaped.
Preferably, the rear end connection flat plate and the rear end connection frame plate are O-shaped.
The utility model has the advantages that: the flight simulator cockpit structure is formed by connecting the front frame assembly and the rear frame assembly through the honing strips and the angle aluminum, and is fixed by using the screws and the screws, the frame is reliable in structural strength, convenient to disassemble and assemble and transport, low in manufacturing cost, and after the frame is paved with the skin, the size and the appearance of the cockpit are very similar to those of a fixed-wing airplane, the operation space is large, the structural member performance is excellent, and a user can have a good flight experience effect.
Drawings
Fig. 1 is a schematic structural diagram of a flight simulator cockpit frame structure provided by the present invention;
fig. 2 is a schematic view of a front-end firewall structure of a flight simulator cockpit frame structure according to the present invention;
fig. 3 is a schematic diagram of a front-end connection frame plate structure of a flight simulator cockpit frame structure provided by the present invention;
fig. 4 is a schematic structural view of a rear connection plate of a flight simulator cockpit frame structure provided by the present invention;
fig. 5 is the utility model provides a flight simulator cockpit frame structure's rear end connection frame plate structure sketch map.
In the figure: 1. front end fire wall, 2 front end connecting frame plate, 3 long horizontal honing strip A, 4 vertical honing strip A, 5 vertical honing strip B, 6 vertical honing strip C, 7 vertical honing strip D, 8 vertical honing strip E, 9 vertical honing strip F, 10 vertical honing strip G, 11 rear end connecting frame plate, 12 long horizontal honing strip B,13 rear end connecting flat plate, 14 supporting connecting piece H,15 supporting connecting piece I,16 supporting connecting piece J,17 supporting connecting piece K,18 supporting connecting piece L,19 supporting connecting piece M,20 supporting connecting piece N,21 angle aluminum, 22 first screw, 23 first nut, 24 rivet, 25 supporting connecting piece F,26 supporting connecting piece E,27 supporting connecting piece D,28 supporting connecting piece C,29 supporting connecting piece B,30 supporting connecting piece A.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
Referring to fig. 1 to 5, the frame structure of the flight simulator cockpit is a bilateral symmetry structure, and is formed by combining the front frame assembly, the vertical honing strips A4 to G10, the long transverse honing strip A3, and the rear frame assembly through the angle aluminum 21, the first nut 23, and the first screw 22, wherein the front frame assembly is formed by connecting and fixing the front firewall 1, the front connecting frame plate 2, the supporting connecting piece a 30, the supporting connecting piece B29, the supporting connecting piece C28, the supporting connecting piece D27, the supporting connecting piece E26, and the supporting connecting piece F25 through the rivet 24; the rear end frame assembly is formed by fixedly connecting the rear end connecting frame plate 11, the rear end connecting flat plate 13, the supporting connecting piece H14, the supporting connecting piece I15, the supporting connecting piece J16, the supporting connecting piece K17, the supporting connecting piece L18, the supporting connecting piece M19 and the supporting connecting piece N20 through the rivet 24. The long transverse honing strips A3 and the long transverse honing strips B12 on the left side and the right side of the cockpit are fixedly connected with the vertical honing strips A4, the vertical honing strips B5, the vertical honing strips C6, the vertical honing strips D7, the vertical honing strips E8, the vertical honing strips F9 and the vertical honing strips G10 through the angle aluminum 21, the first nuts 23 and the first screws 22. Meanwhile, the long transverse honing strip A3 and the long transverse honing strip B12 are fixedly connected with the front end frame component and the rear end frame component through the angle aluminum 21, the first nut 23 and the first screw 22.
This flight simulator cockpit frame construction can not only have good structural strength, conveniently dismantles moreover and transports.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (6)
1. A flight simulator cockpit frame structure comprises a front end frame assembly, a plurality of vertical honing strips, a plurality of long transverse honing strips and a rear end frame assembly, and is characterized in that the front end frame assembly, the plurality of vertical honing strips, the plurality of long transverse honing strips and the rear end frame assembly are combined through a first nut (23), a first screw (22) and angle aluminum (21).
2. The flight simulator cockpit frame structure of claim 1, wherein the front frame assembly comprises a front firewall (1), a front connection frame plate (2), a support connection sheet a (30), a support connection sheet B (29), a support connection sheet C (28), a support connection sheet D (27), a support connection sheet E (26), and a support connection sheet F (25), and the support connection sheet a (30), the support connection sheet B (29), the support connection sheet C (28), the support connection sheet D (27), the support connection sheet E (26), and the support connection sheet F (25) are all fixed to the front firewall (1) by rivets.
3. The flight simulator cockpit frame structure of claim 1, wherein the rear end frame assembly comprises a rear end connection flat plate (13), a rear end connection frame plate (11), a support connection plate H (14), a support connection plate I (15), a support connection plate J (16), a support connection plate K (17), a support connection plate L (18), a support connection plate M (19), and a support connection plate N (20), and the support connection plate H (14), the support connection plate I (15), the support connection plate J (16), the support connection plate K (17), the support connection plate L (18), the support connection plate M (19), and the support connection plate N (20) are all fixed with the rear end connection flat plate (13) through rivets.
4. A flight simulator cockpit frame structure according to claim 1 where the vertical and horizontal honing bars are fixed to the front and rear frame members by means of angle aluminum (21) and first nuts (23) and first screws (22).
5. A flight simulator cockpit frame structure according to claim 2, characterized in that said front firewall (1) is D-shaped; the front end connecting frame plate (2) is C-shaped.
6. A flight simulator cockpit frame structure according to claim 3, characterised in that the rear end connection plate (13) and the rear end connection frame plate (11) are O-shaped.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922112531.0U CN212084431U (en) | 2019-12-01 | 2019-12-01 | Flight simulator cockpit frame structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922112531.0U CN212084431U (en) | 2019-12-01 | 2019-12-01 | Flight simulator cockpit frame structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212084431U true CN212084431U (en) | 2020-12-04 |
Family
ID=73556775
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922112531.0U Active CN212084431U (en) | 2019-12-01 | 2019-12-01 | Flight simulator cockpit frame structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212084431U (en) |
-
2019
- 2019-12-01 CN CN201922112531.0U patent/CN212084431U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105416565A (en) | Solar powered aircraft | |
| CN212084431U (en) | Flight simulator cockpit frame structure | |
| CN103204236B (en) | Multi-purpose plug-in device for helicopter | |
| CN205574265U (en) | Rotor unmanned aerial vehicle | |
| CN208530832U (en) | Built-in steering engine formula composite material unmanned plane wing | |
| CN113306699B (en) | Connecting structure and method for horizontal tail and vertical tail of T-tail layout aircraft | |
| US4148450A (en) | Model aircraft construction | |
| CN207631472U (en) | Honeycomb structure wing and aircraft | |
| CN205216194U (en) | But fixed -wing aircraft of VTOL | |
| CN203666969U (en) | Bonded aerofoil architecture | |
| CN210681125U (en) | Control surface skin for small aircraft | |
| USRE21850E (en) | Airplane structural element | |
| CN203612194U (en) | Concentrated-load force-transferring diffusion piece in box section of wing box | |
| CN206231451U (en) | A kind of stressed-skin construction of fast assembling-disassembling skin | |
| CN219225719U (en) | Low-speed simulated aircraft | |
| CN207045673U (en) | A kind of airstair | |
| CN114715376B (en) | Maintenance flap suitable for flexible skin wing | |
| CN209194736U (en) | It is a kind of can rapid build simple construction component | |
| CN206318017U (en) | A kind of strut dome structure | |
| CN203354001U (en) | Dismountable bookshelf component | |
| CN207607631U (en) | Three axis connecting rod unmanned planes non-stop layer plate framework fuselage | |
| CN201597522U (en) | Automobile top luggage rack capable of being disassembled freely | |
| CN109720570A (en) | A kind of floating drum connection structure of large size amphibious aircraft | |
| CN212980534U (en) | Fixed wing unmanned aerial vehicle capable of being transformed into stretcher and water boiling device | |
| CN210395895U (en) | Assembled detachable antique component |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |