CN204406749U - A kind of spiraling simulator - Google Patents
A kind of spiraling simulator Download PDFInfo
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- CN204406749U CN204406749U CN201520060544.7U CN201520060544U CN204406749U CN 204406749 U CN204406749 U CN 204406749U CN 201520060544 U CN201520060544 U CN 201520060544U CN 204406749 U CN204406749 U CN 204406749U
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Abstract
The utility model relates to a kind of spiraling simulator, comprise and rotate passenger cabin, C type framework, support and base, rotated in C type framework by rotation passenger cabin and can realize simulation roll flight, can realize simulating pitching flying in cradle top rotation by C type framework, be rotated on base by support and can realize the change of simulated flight course.The utility model adopts Modular Structure Design cleverly, can realize the flare maneuver that rotates three axles and the emulation of load in conjunction with dynamo-electric automatic control technology and flight simulation software.The utility model can significantly improve training effect and the level of Aeronautics and Astronautics aircraft pilot, simultaneously also significant and extensive market in science popularization experience and amusement emulation.
Description
Technical field
The utility model relates to a kind of spiraling simulator, belong to Aeronautics and Astronautics training and science popularization experience, amusement flight simulation technology field.
Background technology
At present the domestic and international training patterns to pilot, spacefarer and extraordinary operating personnel and equipment varied, on the Training And Training Equipment of pilot, especially formed the world of specification and domestic standard.But existing training method and training cartridge be not for all meeting to pilot or driver the training in health, physical efficiency, psychology and agility completely, and the training of the ability of meeting an enemy attack fast especially under combat conditions and operation skill etc. is comparatively short of.
The flight simulator of act.std highlights the driver training to aircraft, but can't cover completely in the training of absolutely empty, air-to-ground engagement etc.Can not well train quality such as the health of pilot, physical efficiency, psychology and agilitys when such as doing the various stunts such as fast somersault at aircraft.Though this depends on that normal flight simulator can realize six degree of freedom simulation innervation and but omnidirectional can not infinitely provide action and load.Although some special simulators can reach omnidirectional in theory infinitely provide action and load, its cost is huge, and equipment manufacturing cost is extremely high, is difficult to universal and equipment, is more impossiblely generalized to science popularization experience and entertainment field.On the other hand, an existing class training aids also realizes the simulation to action and load by actions such as rotations, thus to the training of pilot's physical efficiency etc. on acquiring a certain degree, but its exercise equipment is simple, can not combine with flight simulation software, flight control technology etc., therefore training effect is general.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of spiraling simulator, this simulator is a system ensemble being integrated with the various technology such as machinery, electronics, automatically control, flight simulation, sound, light efficiency, solves deficiency of the prior art.
The technical scheme that the utility model solves the problems of the technologies described above is as follows: a kind of spiraling simulator, comprise and rotate passenger cabin, C type framework, support and base, flight simulation computing machine is provided with in described rotation passenger cabin, the two ends of described rotation passenger cabin and the two ends of described C type framework are rotationally connected, the described middle part of C type framework and the side, top of described support are rotationally connected, and the bottom of described support is arranged on described base; Also comprise two cover electric motor and controller assemblies, a set of described motor makes described rotation passenger cabin continuous multiple rotations between the two ends of described C type framework by its Control Component, another set of described motor makes described C type framework continuous multiple rotations on the side, top of described support by its Control Component, described rotation passenger cabin by two cover electric slip rings respectively with external power, flight simulation computer interactive, and control the operation of this two covers electric motor and controller assembly respectively.
On the basis of technique scheme, the utility model can also do following improvement.
Further, one end of described rotation passenger cabin and one end of described C type framework are rotationally connected by roll transmission component, and described motor controls roll transmission component by its Control Component, makes described rotation passenger cabin continuous multiple rotations between the two ends of described C type framework.
The beneficial effect of above-mentioned further scheme is adopted to be rotate passenger cabin continuous multiple rotations between the two ends of C type framework to form the roll motion of flight simulation.
Further, described roll transmission component is made up of pair of sprocket, chain, bearing, bearing seat and main shaft.
Adopt the beneficial effect of above-mentioned further scheme to be that rotation passenger cabin is arranged on C type framework by roll transmission component, and the support that can rotate is provided, by the power transmission of motor and the continuous multiple rotations of driven rotary passenger cabin.
Further, the described middle part of C type framework and the side, top of described support are rotationally connected by pitching transmission component, and described motor controls pitching transmission component by its Control Component, makes described C type framework continuous multiple rotations on the side, top of described support.
The beneficial effect of above-mentioned further scheme is adopted to be that C type framework continuous multiple rotations on the side, top of support forms the luffing of flight simulation.
Further, described pitching transmission component is made up of pair of sprocket, chain, bearing, bearing seat and main shaft.
Adopt the beneficial effect of above-mentioned further scheme be pitching transmission component by C type frame installation on the bracket, and provide the support that can rotate, the power transmission of motor driven the continuous multiple rotations of C type framework.
Further, the bottom of described support is installed on described base, is divided into fixed and rotary two kinds of forms.
Wherein, be fixedly: the bottom of described support is fixedly installed on described base.
Rotaryly be: described base is provided with rotatable course transmission component, and the bottom of described support is fixedly installed on the transmission component of described course.Also comprise extra a set of electric motor and controller assembly, this motor controls course transmission component by its Control Component and rotates on described base, thus drive described support to rotate, described rotation passenger cabin by extra a set of electric slip ring and external power, flight simulation computer interactive, and controls the operation of this electric motor and controller assembly.
Adopt revolving beneficial effect to be that course transmission component rotates on base, thus drive described support to rotate, form the course rotary motion of flight simulation.
Further, described course transmission component is made up of pair of sprocket, chain, bearing, bearing seat and main shaft.
Adopt the beneficial effect course transmission component of above-mentioned further scheme by described support installing on described base, and the support that can rotate is provided, the power transmission of motor is driven the continuous multiple rotations of described support.
Above-mentioned roll transmission component, pitching transmission component, course transmission component are all adopt transmission component the most conventional, bearing is provided with at bearing seat, main shaft is provided with in bearing, one end of main shaft connects power intake, the normally output terminal of motor, the other end of main shaft is provided with a sprocket wheel, and another is arranged on clutch end, namely need the parts that transmission rotates, between two sprocket wheels, pass through chain drive.
Further, described rotation passenger cabin comprises canopy frame, described canopy frame outer wrapping is by the shell with hatch door, be provided with display, pedal, jociey stick, throttle, seat, securing band, sound equipment and described flight simulation computing machine in described canopy frame, described flight simulation computing machine is electrically connected with display, pedal, jociey stick, throttle, sound equipment; Described seat is provided with at least two, and each described seat is equipped with securing band.
Adopt the beneficial effect of above-mentioned further scheme to be rotate passenger cabin to provide the interface of people at loop, each ingredient of its inside can simulate the control system under state of flight, reaches the object emulated for various aircraft flight.Rotate in passenger cabin and by widening, two or more seat can be installed, flight simulation can be carried out to many people simultaneously.
Described flight simulation computing machine provides the operation platform of flight simulation software, achieves the real-time control to motion, what comes into a driver's, audio and the real-time process to pilot control signal.
Described rotation passenger cabin, described motor and Control Component and the described power supply of flight simulation computing machine, the transmission of signal and realized by described electric slip ring alternately.
The beneficial effects of the utility model are: spiraling simulator of the present utility model adopts Modular Structure Design cleverly, flare maneuver that three axles are rotated and the emulation of load can be realized in conjunction with dynamo-electric automatic control technology, visual scene technology and flight simulation software, handle and drive response rapidly, precision is high; Fidelity is high, dynamic strong, is applicable to the flight simulation to various aircraft; Can meet pilot or driver in dispositional training such as health, physical efficiency, psychology and agilitys.Meanwhile, the utility model can significantly improve training effect and the level of Aeronautics and Astronautics aircraft pilot, simultaneously also significant and extensive market in science popularization experience and amusement emulation.
Accompanying drawing explanation
Fig. 1 is the utility model embodiment 1 front elevation;
Fig. 2 is the utility model embodiment 1 left view;
Fig. 3 is the utility model embodiment 1 structural representation;
Fig. 4 is that the utility model rotates passenger cabin cut-open view;
Fig. 5 is the structural representation that the utility model rotates that passenger cabin removes shell;
Fig. 6 is the structural representation that the utility model embodiment 1 removes shell;
Fig. 7 is the utility model embodiment 2 structural representation;
Fig. 8 is the structural representation that the utility model embodiment 2 removes shell;
In accompanying drawing, the list of parts representated by each label is as follows:
1, passenger cabin is rotated, 2, C type framework, 3, support, 4, base, 5, roll transmission component, 6, pitching transmission component, 7, course transmission component, 8, Control Component, 9, electric slip ring, 10, flight simulation computing machine, 11, display, 12, pedal, 13, jociey stick, 14, throttle, 15, seat, 16, securing band, 17, sound equipment, 18, shell, 19, canopy frame.
Embodiment
Be described principle of the present utility model and feature below in conjunction with accompanying drawing, example, only for explaining the utility model, is not intended to limit scope of the present utility model.
Embodiment 1
As shown in Figure 1 to Figure 3, a kind of spiraling simulator, comprise and rotate passenger cabin 1, C type framework 2, support 3 and base 4, flight simulation computing machine 10 is provided with in described rotation passenger cabin 1, the two ends of described rotation passenger cabin 1 and the two ends of described C type framework 2 are rotationally connected, the described middle part of C type framework 2 and the side, top of described support 3 are rotationally connected, and the bottom of described support 3 is arranged on described base 4; Also comprise two cover electric motor and controller assemblies 8, a set of described motor makes described rotation passenger cabin 1 continuous multiple rotations between the two ends of described C type framework 2 by its Control Component 8, another set of described motor makes described C type framework 2 continuous multiple rotations on the side, top of described support 3 by its Control Component 8, described rotation passenger cabin 1 is mutual with external power, flight simulation computing machine 10 respectively by two cover electric slip rings 9, and controls the operation of this two covers electric motor and controller assembly 8 respectively.
One end of described rotation passenger cabin 1 and one end of described C type framework 2 are rotationally connected by roll transmission component 5, and described motor controls roll transmission component 5 by its Control Component 8, make described rotation passenger cabin 1 continuous multiple rotations between the two ends of described C type framework 2.Described rotation passenger cabin 1 continuous multiple rotations between the two ends of C type framework 2 forms the roll motion of flight simulation.
Described roll transmission component 5 is made up of pair of sprocket, chain, bearing, bearing seat and main shaft.Rotation passenger cabin 1 is arranged on C type framework 2 by described roll transmission component 5, and provides the support that can rotate, by the power transmission of motor and driven rotary passenger cabin 1 continuously multiple rotations.
The described middle part of C type framework 2 and the side, top of described support 3 are rotationally connected by pitching transmission component 6, and described motor controls pitching transmission component 6 by its Control Component 8, make described C type framework 2 continuous multiple rotations on the side, top of described support 3.Described C type framework 2 continuous multiple rotations on the side, top of support 3 forms the luffing of flight simulation.
Described pitching transmission component 6 is made up of pair of sprocket, chain, bearing, bearing seat and main shaft.C type framework 2 is arranged on described support 3 by described pitching transmission component 6, and provides the support that can rotate, and the power transmission of motor is driven the continuous multiple rotations of C type framework 2.
The bottom of described support is installed on described base, is divided into fixed and rotary two kinds of forms.
Embodiment 1 is rotary, and described base 4 is provided with rotatable course transmission component 7, and the bottom of described support 3 is fixedly installed on described course transmission component 7.Also comprise extra a set of electric motor and controller assembly 8, this motor controls course transmission component 7 by its Control Component 8 and rotates on described base 4, thus drive described support 3 to rotate, described rotation passenger cabin 1 alternately, and controls the operation of this electric motor and controller assembly 8 by extra a set of electric slip ring 9 and external power, flight simulation computing machine 10.Described course transmission component 7 rotates on base 4, thus drives described support 3 to rotate, and forms the course rotary motion of flight simulation.
Described course transmission component 7 is made up of pair of sprocket, chain, bearing, bearing seat and main shaft.Described support 3 is arranged on described base 4 by described course transmission component 7, and provides the support that can rotate, and the power transmission of motor is driven described support 3 continuously multiple rotations.
As shown in Figures 4 to 6, described rotation passenger cabin 1 comprises canopy frame 19, described canopy frame 19 outer wrapping is by the shell 18 with hatch door, be provided with display 11, pedal 12, jociey stick 13, throttle 14, seat 15, securing band 16, sound equipment 17 and described flight simulation computing machine 10 in described canopy frame 19, described flight simulation computing machine 10 is electrically connected with display 11, pedal 12, jociey stick 13, throttle 14, sound equipment 17; Described seat 15 is provided with at least two, and each described seat 15 is equipped with securing band 16.
Described rotation passenger cabin 1 provides the interface of people at loop, and each ingredient of its inside can simulate the control system under state of flight, reaches the object emulated for various aircraft flight.By widening, two or more seat 15 can be installed in described rotation passenger cabin 1, flight simulation can be carried out to many people simultaneously.
Described flight simulation computing machine 10 provides the operation platform of flight simulation software, achieves the real-time control to motion, what comes into a driver's, audio and the real-time process to pilot control signal.
Described rotation passenger cabin 1, described motor and Control Component 8 and the described power supply of flight simulation computing machine 10, the transmission of signal and realized by described electric slip ring 9 alternately.
Embodiment 2
The bottom of described support is installed on described base, and be divided into fixed and rotary two kinds of forms, embodiment 1 is rotary, and as shown in Figure 7, Figure 8, embodiment 2 is fixed, and namely the bottom of described support 3 is fixedly installed on described base 4.Embodiment 2 is compared with embodiment 1, support 3 is fixed on base 4, do not need course transmission component 7 and supporting motor, Control Component 8 like this, although the course rotary motion of flight simulation cannot be carried out, but its structure is simpler, whole device firm stable more, is very applicable to the application of the aspect such as science popularization experience and amusement emulation, also has great importance and market widely.
The foregoing is only preferred embodiment of the present utility model, not in order to limit the utility model, all within spirit of the present utility model and principle, any amendment done, equivalent replacement, improvement etc., all should be included within protection domain of the present utility model.
Claims (10)
1. a spiraling simulator, it is characterized in that, comprise and rotate passenger cabin (1), C type framework (2), support (3) and base (4), flight simulation computing machine (10) is provided with in described rotation passenger cabin (1), the two ends of described rotation passenger cabin (1) and the two ends of described C type framework (2) are rotationally connected, the middle part of described C type framework (2) and the side, top of described support (3) are rotationally connected, and the bottom of described support (3) is arranged on described base (4);
Also comprise two cover electric motor and controller assemblies (8), a set of described motor makes described rotation passenger cabin (1) continuous multiple rotations between the two ends of described C type framework (2) by its Control Component (8), another set of described motor makes described C type framework (2) continuous multiple rotations on the side, top of described support (3) by its Control Component (8), described rotation passenger cabin (1) by two cover electric slip ring (9) respectively with external power, flight simulation computing machine (10) is mutual, and control the operation of this two cover electric motor and controller assembly (8) respectively.
2. a kind of spiraling simulator according to claim 1, it is characterized in that, one end of described rotation passenger cabin (1) and one end of described C type framework (2) are rotationally connected by roll transmission component (5), described motor controls roll transmission component (5) by its Control Component (8), makes described rotation passenger cabin (1) continuous multiple rotations between the two ends of described C type framework (2).
3. a kind of spiraling simulator according to claim 2, it is characterized in that, described roll transmission component (5) is made up of pair of sprocket, chain, bearing, bearing seat and main shaft.
4. a kind of spiraling simulator according to claim 1, it is characterized in that, the middle part of described C type framework (2) and the side, top of described support (3) are rotationally connected by pitching transmission component (6), described motor controls pitching transmission component (6) by its Control Component (8), makes described C type framework (2) continuous multiple rotations on the side, top of described support (3).
5. a kind of spiraling simulator according to claim 4, it is characterized in that, described pitching transmission component (6) is made up of pair of sprocket, chain, bearing, bearing seat and main shaft.
6. a kind of spiraling simulator according to claim 1, it is characterized in that, the bottom of described support (3) is fixedly installed on described base (4).
7. a kind of spiraling simulator according to claim 1, it is characterized in that, described base (4) is provided with rotatable course transmission component (7), and the bottom of described support (3) is fixedly installed on described course transmission component (7).
8. a kind of spiraling simulator according to claim 7, it is characterized in that, also comprise extra a set of electric motor and controller assembly (8), this motor controls course transmission component (7) in the upper rotation of described base (4) by its Control Component (8), thus drive described support (3) to rotate, described rotation passenger cabin (1) alternately, and controls the operation of this electric motor and controller assembly (8) by extra a set of electric slip ring (9) and external power, flight simulation computing machine (10).
9. a kind of spiraling simulator according to claim 7, it is characterized in that, described course transmission component (7) is made up of pair of sprocket, chain, bearing, bearing seat and main shaft.
10. a kind of spiraling simulator according to any one of claim 1 to 9, it is characterized in that, described rotation passenger cabin (1) comprises canopy frame (19), described canopy frame (19) outer wrapping is by the shell (18) with hatch door, display (11) is installed in described canopy frame (19), pedal (12), jociey stick (13), throttle (14), seat (15), securing band (16), sound equipment (17) and described flight simulation computing machine (10), described flight simulation computing machine (10) and display (11), pedal (12), jociey stick (13), throttle (14), sound equipment (17) is electrically connected, described seat (15) is provided with at least two, and each described seat (15) is equipped with securing band (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520060544.7U CN204406749U (en) | 2015-01-28 | 2015-01-28 | A kind of spiraling simulator |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520060544.7U CN204406749U (en) | 2015-01-28 | 2015-01-28 | A kind of spiraling simulator |
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| CN204406749U true CN204406749U (en) | 2015-06-17 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104637364A (en) * | 2015-01-28 | 2015-05-20 | 北京蓝天航空科技有限责任公司 | Rotating flight simulator |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104637364A (en) * | 2015-01-28 | 2015-05-20 | 北京蓝天航空科技有限责任公司 | Rotating flight simulator |
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