CN207938219U - A kind of Helicopter Simulator emulation operating mechanism - Google Patents
A kind of Helicopter Simulator emulation operating mechanism Download PDFInfo
- Publication number
- CN207938219U CN207938219U CN201721274813.5U CN201721274813U CN207938219U CN 207938219 U CN207938219 U CN 207938219U CN 201721274813 U CN201721274813 U CN 201721274813U CN 207938219 U CN207938219 U CN 207938219U
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- rotary support
- shaft
- mounting plate
- operating mechanism
- control
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Abstract
The utility model discloses a kind of Helicopter Simulators to emulate operating mechanism, including fixed panel, control stick, pitch control mechanism and control of sideward roll mechanism；The pitch control mechanism includes rotary support and pitching shaft, and control of sideward roll mechanism includes the mounting plate being arranged at rotary support both ends, and the mounting plate is fixedly mounted on fixed panel；The control stick lower end is connected with driving support seat, and mounting hole is provided in driving support seat, and pitching shaft is fixedly connected across the mounting hole and driving support seat, and the mounting hole both ends end face is clearance fit with rotary support both sides inner wall.The operating mechanism topology layout connects reasonable, operational movement smoothness, and the control run of mechanism and the simulation of steering force can reach the requirement of fly simulation training；Manufacture, assembly technology are simple, connection, convenient disassembly between each part and assembly, are convenient for maintaining, have saved the expense needed for the maintaining in later stage.
Description
Technical field
The utility model is related to move simulation manipulation technology field, more particularly to a kind of Helicopter Simulator emulates manipulation machine
Structure.
Background technology
With the development of domestic General Aviation, the quantity of all purpose aircraft is growing, but lacks corresponding flight training
Equipment, and the expense for training of flying is higher by much than American-European countries training cost.Therefore reasonable employment flight simulator is to flying
Office staff carries out certain foundation training, can not only improve the efficiency of training, saves training cost, improves the safety of training,
The pollution etc. to environment can also be mitigated simultaneously.
The current virtual flight main control mechanism of civilian virtual flight in the market is using fixed-wing center control wheel and table
The center rod of face rank is come the pitching of aircraft when controlling simulated flight and roll posture.From domestic current introduced helicopter
From the point of view of type, majority is Robinson's R22/R44 helicopters, comparatively laborious for the relatively other helicopters of operating difficulty, because
This is badly in need of a kind of operating mechanism that can emulate helicopter flight operation.
Utility model content
The purpose of this utility model is to provide a kind of Helicopter Simulators to emulate operating mechanism, mechanism operational movement stream
Freely, the analog simulation requirement that can meet helicopter operation solves the problems, such as that flight training is of high cost, safety is bad.
In order to solve the above technical problems, the utility model uses following technical scheme：
A kind of Helicopter Simulator emulation operating mechanism, including fixed panel, control stick, pitch control mechanism and roll control
Mechanism processed；
The pitch control mechanism includes rotary support and pitching shaft, and the rotary support is hollow frame structure, rotation
Turn bearing both ends and be respectively arranged with roll shaft, pitching shaft is horizontally through rotary support and is arranged in rotary support, and pitching turns
Axis is arranged in a mutually vertical manner with roll shaft, and bearing is provided between pitching shaft both ends and rotary support；
The control of sideward roll mechanism includes the mounting plate being arranged at rotary support both ends, and the mounting plate is separately mounted to revolve
Turn in the roll shaft at bearing both ends, bearing is provided between mounting plate and roll shaft, the mounting plate is fixedly mounted on
Determine on panel；
The control stick lower end is connected with driving support seat, and the hollow frame structure in rotary support is arranged in the driving support seat
Interior, driving support seat, roll shaft and pitching shaft are arranged in a mutually vertical manner, and mounting hole is provided in driving support seat, and pitching shaft is worn
It crosses between the mounting hole and driving support seat and is fixedly connected, mounting hole both ends end face is gap with rotary support both sides inner wall
Cooperation.
In above-mentioned technical proposal, further, loading spring there are two settings between the rotary support and driving support seat,
The loading spring both ends are connected on rotary support and driving support seat, and two loading springs are symmetricly set on pitching shaft
Both sides.
In above-mentioned technical proposal, further, the rotary support side is respectively set in its underpart position there are two bullet
Spring bushing, driving support seat lower end reach one end outside rotary support and are provided with spring bushing, the loading spring both ends difference
It is connected on the spring bushing on rotary support and transmission bracket.
In above-mentioned technical proposal, further, there are two load bullet for setting between any mounting plate and rotary support
Spring, the loading spring both ends are separately connected on mounting plate and rotary support, and two loading springs are symmetricly set on roll shaft
Both sides.
In above-mentioned technical proposal, further, mounting plate lower end both sides are respectively arranged with spring bushing, rotary support
Upper that mounting plate one end lower part is provided with spring bushing, the loading spring both ends are connected to mounting plate and rotation branch
On spring bushing on seat.
In above-mentioned technical proposal, further, it is provided in the pitching shaft and/or roll shaft for measuring its turn
The sensor of dynamic angle.
In above-mentioned technical proposal, further, the sensor is mounted in a mounting bracket, and mounting bracket is fixed respectively
On mounting plate and rotary support, the shaft of sensor is fixedly connected with pitching shaft and roll shaft respectively.
In above-mentioned technical proposal, further, the pitching shaft and roll roller end are respectively arranged with along axis side
To centre bore, be fixedly connected between pitching shaft and roll shaft in the centrally disposed hole of shaft of the sensor.
In above-mentioned technical proposal, further, the control stick is T-shaped structure, including T shapes cross bar and T shape struts are described
It is connected by arm pivot post between T shapes cross bar and T shape struts, arm pivot post one end is fixedly connected with T shape cross bars, and the other end stretches into
In the connector sleeve being arranged to T shape strut ends, by the way that two axis at connector sleeve both ends are arranged between arm pivot post and connector sleeve
Hold connection.
In above-mentioned technical proposal, further, the T shapes cross bar both ends are respectively arranged with control crank.
Advantageous effect possessed by the utility model：
The utility model topology layout, connection are reasonable, and operational movement is smooth, the control run of mechanism and the mould of steering force
The quasi- requirement that can reach fly simulation training；Meanwhile this emulation operating mechanism uses generalization, modularization and standard
The design of change, manufacture, assembly technology are simple, connection, convenient disassembly between each part and assembly, are convenient for maintaining, section
Expense about needed for the maintaining in later stage.
Description of the drawings
Fig. 1 is the utility model dimensional structure diagram.
Fig. 2 is the utility model structural front view.
Fig. 3 is the utility model the structure left view.
Fig. 4 is the utility model structural blast schematic diagram.
In figure：1, fixed panel, 2, control stick, 201, T shape cross bars, 202, T shape struts, 203, arm pivot post, 204, even
Female connector, 205, control crank, 3, rotary support, 4, pitching shaft, 5, roll shaft, 6, bearing, 7, mounting plate, 8, transmission branch
Seat, 9, mounting hole, 10, loading spring, 11, spring bushing, 12, sensor, 13, mounting bracket.
Specific implementation mode
The utility model is further described in the following with reference to the drawings and specific embodiments.
Helicopter Simulator as shown in Figures 1 to 4 emulates operating mechanism, including fixed panel 1, control stick 2, pitch control
Mechanism and control of sideward roll mechanism；Pitch control mechanism includes rotary support 3 and pitching shaft 4, and rotary support 3 is hollow frame knot
Structure, 3 both ends of rotary support are respectively arranged with roll shaft 5, and pitching shaft 4 is horizontally through rotary support 3 and is arranged in rotary support 3
Interior, pitching shaft 4 is arranged in a mutually vertical manner with roll shaft 5, and bearing 6 is provided between 4 both ends of pitching shaft and rotary support 3.
Control of sideward roll mechanism includes the mounting plate 7 being arranged at 3 both ends of rotary support, and mounting plate 7 is separately mounted to rotary support both ends
In roll shaft 5, bearing 6 is provided between mounting plate 7 and roll shaft 5, mounting plate 7 is fixedly mounted on fixed panel 1.
2 lower end of control stick is connected with driving support seat 8, and driving support seat 8 is arranged in the hollow frame structure of rotary support 3,
Driving support seat 8, roll shaft 5 and pitching shaft 4 are arranged in a mutually vertical manner, and mounting hole 9, pitching shaft 4 are provided in driving support seat 8
It is fixedly connected across mounting hole 9 and driving support seat 8,9 both ends end face of mounting hole is matched with rotary support both sides inner wall for gap
It closes.
In the present embodiment, control stick 2 is T-shaped structure, including T shapes cross bar 201 and T shapes strut 202, T shapes cross bar 201 and T
It is connected by arm pivot post 203 between shape strut 202,203 one end of arm pivot post is fixedly connected with T shapes cross bar 201, and the other end is stretched
Enter into the connector sleeve 204 of 202 end set of T shapes strut, is being connected by setting between arm pivot post 203 and connector sleeve 204
Cover two bearings 6 connection at 204 both ends.201 both ends of T shapes cross bar are respectively arranged with control crank 205, are set on control crank 205
It is equipped with sponges cover.
There are two loading springs 10 for setting between rotary support 3 and driving support seat 8, and 10 both ends of loading spring are connected to
On rotary support 3 and driving support seat 8, two loading springs 10 are symmetricly set on 4 both sides of pitching shaft.Specifically, rotary support 3
Side is respectively set in its underpart position there are two spring bushing 11, and 8 lower end of driving support seat reaches one end outside rotary support 3
It is provided with spring bushing 11,10 both ends of loading spring are connected on the spring bushing 11 in rotary support 3 and transmission bracket.
Spring bushing 11 is fixedly mounted on by screw on rotary support 3 and driving support seat 8.
Similarly, there are two loading spring 10, loading springs for setting between any mounting plate 7 and rotary support 3 wherein
10 both ends are separately connected on mounting plate 7 and rotary support 3, and two loading springs 10 are symmetricly set on 5 both sides of roll shaft.Specifically
Ground, 7 lower end both sides of mounting plate are respectively arranged with spring bushing 11, are provided with positioned at 7 one end lower part of mounting plate on rotary support 3
Spring bushing 11,10 both ends of loading spring are connected on the spring bushing 11 on mounting plate and rotary support.
In the present embodiment, the sensor for measuring its rotational angle is provided in pitching shaft 4 and roll shaft 5
12.Sensor 12 is separately mounted in a mounting bracket 13, and mounting bracket 13 is respectively and fixedly installed to mounting plate 7 and rotary support
On 3, the shaft of sensor 12 is fixedly connected with pitching shaft 4 and roll shaft 5 respectively.Preferably, pitching shaft 4 and roll turn
5 end of axis is respectively arranged with centre bore in the axial direction, in the centrally disposed hole of shaft of sensor with pitching shaft 4 and cross
It is fixedly connected between wobble shaft 5.
When using the operating mechanism, trainer holds control crank, and when control control stick swings, control stick drives rotation
Turn bearing along roll shaft left-right rotation, roll shaft drives the sensor shaft rotation being connected thereto, by sensor telecommunications
It number is transported to simulated flight control box, realizes that the simulation to the roll posture of aircraft controls；When controlling control stick swing,
Control stick drives the rotation of pitching shaft, and pitching shaft drives the sensor shaft rotation being connected thereto, by sensor electric signal
It is transported to simulated flight control box, realizes that the simulation of the pitch attitude to aircraft controls.Loading spring is respectively that control stick provides
Restoring force makes control stick be returned to intermediate initial position.
The description and the appended drawings of the utility model are considered illustrative and not restrictive, on the utility model basis
On, for those skilled in the art according to disclosed technology contents, not needing performing creative labour can be to some of technology
Some replacements and deformation that feature is made, it is within the protection scope of the present utility model.
Claims (10)
1. a kind of Helicopter Simulator emulates operating mechanism, it is characterised in that：Including fixed panel, control stick, pitch control machine
Structure and control of sideward roll mechanism；
The pitch control mechanism includes rotary support and pitching shaft, and the rotary support is hollow frame structure, rotation branch
Seat both ends are respectively arranged with roll shaft, and pitching shaft is horizontally through rotary support and is arranged in rotary support, pitching shaft with
Roll shaft is arranged in a mutually vertical manner, and bearing is provided between pitching shaft both ends and rotary support；
The control of sideward roll mechanism includes the mounting plate being arranged at rotary support both ends, and the mounting plate is separately mounted to rotation branch
In the roll shaft at seat both ends, bearing is provided between mounting plate and roll shaft, the mounting plate is fixedly mounted on stationary plane
On plate；
The control stick lower end is connected with driving support seat, and the driving support seat is arranged in the hollow frame structure of rotary support,
Driving support seat, roll shaft and pitching shaft are arranged in a mutually vertical manner, and mounting hole is provided in driving support seat, and pitching shaft passes through institute
It states and is fixedly connected between mounting hole and driving support seat, mounting hole both ends end face is matched with rotary support both sides inner wall for gap
It closes.
2. Helicopter Simulator according to claim 1 emulates operating mechanism, it is characterised in that：The rotary support and biography
There are two loading springs, the loading spring both ends to be connected on rotary support and driving support seat for setting between dynamic bearing,
Two loading springs are symmetricly set on pitching shaft both sides.
3. Helicopter Simulator according to claim 2 emulates operating mechanism, it is characterised in that：The rotary support side
Spring bushing there are two being respectively set in its underpart position, driving support seat lower end reaches one end outside rotary support and is provided with bullet
Spring bushing, the loading spring both ends are connected on the spring bushing on rotary support and transmission bracket.
4. Helicopter Simulator according to claim 1 emulates operating mechanism, it is characterised in that：Any mounting plate and
There are two loading springs, the loading spring both ends to be separately connected on mounting plate and rotary support for setting between rotary support, and two
A loading spring is symmetricly set on roll shaft both sides.
5. Helicopter Simulator according to claim 4 emulates operating mechanism, it is characterised in that：The mounting plate lower end two
Side is respectively arranged with spring bushing, and mounting plate one end lower part is provided with spring bushing, the load bullet on rotary support
Spring both ends are connected on the spring bushing on mounting plate and rotary support.
6. Helicopter Simulator according to any one of claim 1 to 5 emulates operating mechanism, it is characterised in that：It is described
The sensor for measuring its rotational angle is provided in pitching shaft and/or roll shaft.
7. Helicopter Simulator according to claim 6 emulates operating mechanism, it is characterised in that：The sensor is mounted on
In one mounting bracket, mounting bracket is respectively and fixedly installed on mounting plate and rotary support, the shaft of sensor respectively with pitching
Shaft is fixedly connected with roll shaft.
8. Helicopter Simulator according to claim 7 emulates operating mechanism, it is characterised in that：The pitching shaft and cross
Rolling axial end portion is not provided with centre bore in the axial direction, turns with pitching in the centrally disposed hole of shaft of the sensor
It is fixedly connected between axis and roll shaft.
9. Helicopter Simulator according to claim 1 emulates operating mechanism, it is characterised in that：The control stick is T shapes
Structure, including T shapes cross bar and T shape struts, are connected between the T shapes cross bar and T shape struts by arm pivot post, arm pivot post one
End is fixedly connected with T shape cross bars, and the other end is extend into the connector sleeve of T shape strut ends setting, arm pivot post and connector sleeve it
Between by be arranged connector sleeve both ends two bearings connection.
10. Helicopter Simulator according to claim 9 emulates operating mechanism, it is characterised in that：The T shapes cross bar both ends
It is respectively arranged with control crank.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721274813.5U CN207938219U (en) | 2017-09-29 | 2017-09-29 | A kind of Helicopter Simulator emulation operating mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721274813.5U CN207938219U (en) | 2017-09-29 | 2017-09-29 | A kind of Helicopter Simulator emulation operating mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207938219U true CN207938219U (en) | 2018-10-02 |
Family
ID=63645302
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721274813.5U Expired - Fee Related CN207938219U (en) | 2017-09-29 | 2017-09-29 | A kind of Helicopter Simulator emulation operating mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207938219U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109147466A (en) * | 2018-10-24 | 2019-01-04 | 吉林大学 | Helicopter driving simulator steerable system |
| CN113557488A (en) * | 2019-01-03 | 2021-10-26 | M-R·格纳特 | Control device for controlling real or virtual airborne objects |
| CN114999268A (en) * | 2022-05-07 | 2022-09-02 | 北京领为军融科技有限公司 | Universal operating rod base for air combat confrontation simulation training system |
-
2017
- 2017-09-29 CN CN201721274813.5U patent/CN207938219U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109147466A (en) * | 2018-10-24 | 2019-01-04 | 吉林大学 | Helicopter driving simulator steerable system |
| CN113557488A (en) * | 2019-01-03 | 2021-10-26 | M-R·格纳特 | Control device for controlling real or virtual airborne objects |
| CN114999268A (en) * | 2022-05-07 | 2022-09-02 | 北京领为军融科技有限公司 | Universal operating rod base for air combat confrontation simulation training system |
| CN114999268B (en) * | 2022-05-07 | 2023-03-21 | 北京领为军融科技有限公司 | Universal operating rod base for air combat confrontation simulation training system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181002 Termination date: 20190929 |