CN209441617U - A kind of rudder control system of light-duty sport plane - Google Patents
A kind of rudder control system of light-duty sport plane Download PDFInfo
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- CN209441617U CN209441617U CN201822253173.0U CN201822253173U CN209441617U CN 209441617 U CN209441617 U CN 209441617U CN 201822253173 U CN201822253173 U CN 201822253173U CN 209441617 U CN209441617 U CN 209441617U
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- rudder
- pedal
- control system
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- cable wire
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Abstract
A kind of rudder control system of light-duty sport plane, pedal component, transmission rope and the rudder skeleton adjusted the angle including the control rudder that is linked in sequence；The pedal component includes two groups of left pedal groups and right pedal group being articulated in rack, and pulling force can be transmitted by the transmission rope and the rudder skeleton is driven to deflect or deflect to the right to the left by stepping on the left pedal group or the right pedal group.The rudder control system of the light-duty sport plane of the utility model is manipulated using pedal component, by transmission rope to the transmitting of power come manipulation direction rudder skeleton, structure is simple, reaction is quick, and entire rudder control system is made of mechanical structure completely, guarantees to manipulate in flight course safe and reliable；In addition, pedal component links in two cockpits, guarantee two drivers can manipulation direction rudder, further strengthen safety.
Description
Technical field
The utility model relates to the control system field of baby plane state of flight, more specifically to a kind of light-duty fortune
The rudder control system of dynamic aircraft.
Background technique
Flight control system refers to the control command of transmitting driver or automatic pilot, driving rudder face and other mechanisms
With the system for controlling aircraft flight attitude.According to control command source, artificial manipulation can be divided into and automatically controlled.Artificial manipulation is again
Primary control circuit and secondary control system can be divided into, primary control circuit is by control stick and pedal, i.e. central control mechanism comes
The operating mechanism of the elevator of aircraft, aileron and rudder is controlled to control aircraft flight path and posture.Secondary control system
Including trimmer, wing flap, flap, adjustable stabilizer and wing sweep control mechanism etc., for controlling the movement of aircraft
State.
Primary control circuit includes rudder control system, Aileron control system and rudder control system, controls aircraft liter
It drops rudder, aileron and rudder kick and generates the torque around three spatial axes of aircraft, aircraft is made to carry out phase by the intention of driver
Pitching, inclination and the yawing rotation answered.Secondary control system is rudder control system, and control wing flap deflection increases lift.
The effect of rudder of aircraft is to control the deflection of rudder by trampling pedals, so that it is inclined to generate aircraft
The athletic posture of boat, plays a crucial role in aircraft flight, and pedals control the transmission of rudder
Mode decides the service performance and reliability of rudder, all plays decisive role to the performance and safety of aircraft.
Utility model content
The utility model provides a kind of rudder control system of light-duty sport plane in view of the deficiencies of the prior art,
The rudder control system of the light-duty sport plane of the utility model is manipulated using pedal component, by transmission rope to power
Transmitting carry out manipulation direction rudder skeleton, structure is simple, reaction is quick, and entire rudder control system is completely by mechanical structure
Composition guarantees to manipulate in flight course safe and reliable；In addition, pedal component links in two cockpits, guarantees two and drive
The person of sailing can manipulation direction rudder, further strengthen safety.
The specific technical solution of the utility model is as follows, a kind of rudder control system of light-duty sport plane, including suitable
Pedal component, transmission rope and the rudder skeleton that sequence connection control rudder adjusts the angle；
The pedal component includes two groups of left pedal groups and right pedal group being articulated in rack, steps on the left pedal group
Or the right pedal group can be transmitted pulling force by the transmission rope and drive the rudder skeleton deflect to the left or to right avertence
Turn.
Deflection, structure is adjusted by transmission rope described in the pedal component handles in the rudder skeleton as a result,
Simple and stable, securely and reliably；In addition, the pedal component links in two cockpits, guarantee that two drivers can grasp
Longitudinal direction rudder, further strengthens safety.
As the preferred of the utility model, the left pedal group is connected the left pedal of the twoth operator seat by left articulated shaft
It connects, the right pedal group is connected the right pedal of two operator seats by right articulated shaft, is connected with left swing on the left articulated shaft
Lever is connected with right oscillating rod on the right articulated shaft.
The left pedal of two cockpits is connected by the left pedal group by the left articulated shaft as a result, realizes connection
Dynamic, the right pedal of two cockpits is connected by the right pedal group by the right articulated shaft realizes linkage, and described
Left swing lever and the left articulated shaft are affixed, and the right oscillating rod and the right articulated shaft are affixed, two drivers any one
Stepping on the left pedal or the right pedal can be such that the left swing lever or the right oscillating rod swings forward, realize to described
The pulling of transmission rope.
As the preferred of the utility model, the rudder skeleton includes the left connection sheet and right connection for driving deflection
Piece, the transmission rope include left connection cable wire and right connection cable wire, the left connection cable wire be connected to the left swing lever and
Between the left connection sheet, the right connection cable wire is connected between the right oscillating rod and the right connection sheet.
The left swing lever pulls the left connection cable wire to drive the left connection sheet to make the rudder bone as a result,
Frame deflection, the right oscillating rod pull the right connection cable wire to drive the right connection sheet to keep the rudder skeleton inclined
Turn.
As the preferred of the utility model, left reset branch is separately installed with below the left pedal group and the right pedal group
Strut and right reset support rod.
The left reset support rod and the right reset support rod use spring, air pressure or hydraulic reset mode as a result, step on
Pass through the left reset support rod after moving the left pedal group or the right pedal group or the right reset support rod can be rapid
It resets.
As the preferred of the utility model, at least there is one section of bullet in the left connection cable wire and the right connection cable wire respectively
Property section.
It is capable of forming buffering when pulling the left connection cable wire or the right connection cable wire as a result, guarantees the rudder
Skeleton is more steady to be deflected.
As the preferred of the utility model, the range that the rudder skeleton is deflected from middle position to two sides is in 30 °.
Safety is influenced in order to avoid rudder kick is excessive, the inclined of the rudder skeleton is limited in mechanical structure
Gyration is effective means in a certain range, and rudder control surfaces stroke limits institute generally within the scope of 30 ° accordingly
It states rudder skeleton and deflects 30 ° from the most multidirectional two sides of initial position.
In conclusion the utility model has the following beneficial effects:
The rudder control system of the light-duty sport plane of the utility model is manipulated using pedal component, passes through transmission
Cable wire carrys out manipulation direction rudder skeleton to the transmitting of power, and structure is simple, reaction is quick, and entire rudder control system completely by
Mechanical structure composition guarantees to manipulate in flight course safe and reliable；In addition, pedal component links in two cockpits, protect
Demonstrate,prove two drivers can manipulation direction rudder, further strengthen safety.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the rudder control system of the light-duty sport plane of the utility model；
Fig. 2 is the structural schematic diagram of the rudder control system pedal component of the light-duty sport plane of the utility model；
Fig. 3 is rudder control drive system cable wire and the pedal component junction of the light-duty sport plane of the utility model
Structural schematic diagram；
Fig. 4 is rudder control drive system cable wire and the rudder skeleton junction of the light-duty sport plane of the utility model
Structural schematic diagram；
In figure, 1- pedal component, 11- left pedal group, the left articulated shaft of 111-, 112- left pedal, 113- left swing lever, 114-
The right reset support of left reset support rod, 12- right pedal group, the right articulated shaft of 121-, 122- right pedal, the right oscillating rod of 123-, 124-
The left connection cable wire of bar, 2- transmission rope, 21-, the right connection cable wire of 22-, 3- rudder skeleton, the left connection sheet of 31-, the right connection of 32-
Piece.
Specific embodiment
Below in conjunction with attached drawing, by specific embodiment, the utility model is described in further detail.
As shown in Figure 1, Figure 2, Fig. 3, Fig. 4, a kind of rudder control system of light-duty sport plane, including sequential connection controlling party
Pedal component 1, transmission rope 2 and the rudder skeleton 3 adjusted the angle to rudder；
Pedal component 1 includes two groups of left pedal groups 11 and right pedal group 12 being articulated in rack, steps on left pedal group 11
Or right pedal group 12 can be transmitted pulling force by transmission rope 2 and rudder skeleton 3 is driven to deflect or deflect to the right to the left.
Rudder skeleton 3 manipulates transmission rope 2 by pedal component 1 and is adjusted deflection as a result, simple and stable structure,
Securely and reliably；In addition, pedal component 1 links in two cockpits, guarantee two drivers can manipulation direction rudder, into one
Step reinforces safety.
Such as Fig. 2, left pedal group 11 is connected the left pedal 112 of the twoth operator seat by left articulated shaft 111, right pedal group
12 are connected the right pedal 122 of two operator seats by right articulated shaft 121, are connected with left swing lever 113 on left articulated shaft 111,
Right oscillating rod 123 is connected on right articulated shaft 121.
The left pedal 112 of two cockpits is connected by left pedal group 11 by left articulated shaft 111 as a result, realizes linkage, right
The right pedal 122 of two cockpits is connected by pedal group 12 by right articulated shaft 121 realizes linkage, and 113 He of left swing lever
Left articulated shaft 111 is affixed, and right oscillating rod 123 and right articulated shaft 121 are affixed, two drivers any one step on left pedal 112
Or right pedal 122 can be such that left swing lever 113 or right oscillating rod 123 swings forward, realize the pulling to transmission rope 2.
As shown in Figure 1, Figure 2, Fig. 3, Fig. 4, rudder skeleton 3 include the left connection sheet 31 and right connection sheet for driving deflection
32, transmission rope 2 includes left connection cable wire 21 and right connection cable wire 22, and left connection cable wire 21 is connected to left swing lever 113 and a left side
Between connection sheet 31, right connection cable wire 22 is connected between right oscillating rod 123 and right connection sheet 32.
Left swing lever 113 pulls left connection cable wire 21 to drive left connection sheet 31 to deflect rudder skeleton 3 as a result,
Right oscillating rod 123 pulls right connection cable wire 22 to drive right connection sheet 32 to deflect rudder skeleton 3.
Such as Fig. 2, left reset support rod 114 and right reset support are separately installed with below left pedal group 11 and right pedal group 12
Bar 124.
Left reset support rod 114 and right reset support rod 124 are stepped on using spring, air pressure or hydraulic reset mode as a result,
It can be resetted rapidly after left pedal group 11 or right pedal group 12 by left 114 or right reset support rod 124 of reset support rod.
At least there is one section of stretch section respectively in left connection cable wire 21 and right connection cable wire 22.
It is capable of forming buffering when pulling left 21 or right connection cable wire 22 of connection cable wire as a result, guarantees rudder skeleton 3 more
It is steady to deflect.
The range that rudder skeleton 3 is deflected from middle position to two sides is in 30 °.
Safety is influenced in order to avoid rudder kick is excessive, the deflection of rudder skeleton 3 is limited in mechanical structure
Angle is effective means in a certain range, and rudder control surfaces stroke limits direction generally within the scope of 30 ° accordingly
Rudder skeleton 3 deflects 30 ° from the most multidirectional two sides of initial position.
Embodiment described above is only that preferred embodiments of the present invention are described, not practical new to this
The conception and scope of type is defined.Without departing from the design concept of the present utility model, ordinary people in the field is to this
The all variations and modifications that the technical solution of utility model is made, should fall within the protection scope of the present utility model, this is practical
Novel claimed technology contents, are all described in the claims.
Claims (6)
1. a kind of rudder control system of light-duty sport plane, it is characterised in that: including the control rudder adjustment that is linked in sequence
Pedal component (1), transmission rope (2) and the rudder skeleton (3) of angle；
The pedal component (1) includes two groups of left pedal groups (11) and right pedal group (12) being articulated in rack, is stepped on described
Left pedal group (11) or the right pedal group (12) can transmit pulling force by the transmission rope (2) and drive the rudder bone
Frame (3) is deflected to the left or is deflected to the right.
2. a kind of rudder control system of light-duty sport plane according to claim 1, it is characterised in that: the left foot
It pedals group (11) and is connected the left pedal (112) of the twoth operator seat by left articulated shaft (111), the right pedal group (12) passes through
Right articulated shaft (121) connects the right pedal (122) of two operator seats, is connected with left swing lever on the left articulated shaft (111)
(113), right oscillating rod (123) are connected on the right articulated shaft (121).
3. a kind of rudder control system of light-duty sport plane according to claim 2, it is characterised in that: the direction
Rudder skeleton (3) includes the left connection sheet (31) and right connection sheet (32) for driving deflection, and the transmission rope (2) includes left company
Cable wire (21) and right connection cable wire (22) are connect, the left connection cable wire (21) is connected to the left swing lever (113) and the left side
Between connection sheet (31), the right connection cable wire (22) be connected to the right oscillating rod (123) and the right connection sheet (32) it
Between.
4. a kind of rudder control system of light-duty sport plane according to claim 2, it is characterised in that: the left foot
It pedals and is separately installed with left reset support rod (114) and right reset support rod (124) below group (11) and the right pedal group (12).
5. a kind of rudder control system of light-duty sport plane according to claim 3, it is characterised in that: the left company
It connects cable wire (21) and the right connection cable wire (22) at least has one section of stretch section respectively.
6. a kind of rudder control system of light-duty sport plane described in any bar claim according to claim 1 ~ 5,
Be characterized in that: the range that the rudder skeleton (3) deflects from middle position to two sides is in 30 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822253173.0U CN209441617U (en) | 2018-12-29 | 2018-12-29 | A kind of rudder control system of light-duty sport plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822253173.0U CN209441617U (en) | 2018-12-29 | 2018-12-29 | A kind of rudder control system of light-duty sport plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209441617U true CN209441617U (en) | 2019-09-27 |
Family
ID=68016836
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822253173.0U Active CN209441617U (en) | 2018-12-29 | 2018-12-29 | A kind of rudder control system of light-duty sport plane |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112885187A (en) * | 2021-03-26 | 2021-06-01 | 陕西东弘机电设备有限公司 | Flight simulator control system |
| CN113184168A (en) * | 2021-05-14 | 2021-07-30 | 陕西飞机工业有限责任公司 | Elevator adjustment sheet control system |
| CN114056550A (en) * | 2021-11-03 | 2022-02-18 | 哈尔滨哈飞航空工业有限责任公司 | Dustproof device for airplane pedal |
| CN114180030A (en) * | 2021-12-29 | 2022-03-15 | 浙江万丰飞机制造有限公司 | Light airplane rudder control device |
-
2018
- 2018-12-29 CN CN201822253173.0U patent/CN209441617U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112885187A (en) * | 2021-03-26 | 2021-06-01 | 陕西东弘机电设备有限公司 | Flight simulator control system |
| CN113184168A (en) * | 2021-05-14 | 2021-07-30 | 陕西飞机工业有限责任公司 | Elevator adjustment sheet control system |
| CN114056550A (en) * | 2021-11-03 | 2022-02-18 | 哈尔滨哈飞航空工业有限责任公司 | Dustproof device for airplane pedal |
| CN114180030A (en) * | 2021-12-29 | 2022-03-15 | 浙江万丰飞机制造有限公司 | Light airplane rudder control device |
| CN114180030B (en) * | 2021-12-29 | 2024-02-13 | 浙江万丰飞机制造有限公司 | Steering device for light aircraft rudder |
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