CN203325254U - Rotary wing type carrier operating system - Google Patents

Rotary wing type carrier operating system Download PDF

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Publication number
CN203325254U
CN203325254U CN2013203600535U CN201320360053U CN203325254U CN 203325254 U CN203325254 U CN 203325254U CN 2013203600535 U CN2013203600535 U CN 2013203600535U CN 201320360053 U CN201320360053 U CN 201320360053U CN 203325254 U CN203325254 U CN 203325254U
Authority
CN
China
Prior art keywords
type carrier
operating system
rotating speed
wind type
rotary wind
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
Application number
CN2013203600535U
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Chinese (zh)
Inventor
奥古斯托·乌德里克·西盖尔
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CICARE S.A.
Original Assignee
CICARE SA
AEROJONES AVIATION TECHNOLOGY Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by CICARE SA, AEROJONES AVIATION TECHNOLOGY Co Ltd filed Critical CICARE SA
Priority to CN2013203600535U priority Critical patent/CN203325254U/en
Application granted granted Critical
Publication of CN203325254U publication Critical patent/CN203325254U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model provides a rotary wing type carrier operating system. The rotary wing type carrier operating system includes an auxiliary device, a rotary wing type carrier, a driving device, and an automatic speed regulating device. The auxiliary device comprises a base, a cylinder, and a shipper rod which is connected to the cylinder in a manner that the shipper rod can be moved up and down. The rotary wing type carrier comprises a carrier body connected to the shipper rod, an engine provided with an accelerator, a main rotary wing, a pull rod, and a rolling handle. The automatic speed regulating device comprises a central processing unit which is electrically connected to the driving device and can be used to make the driving device to actuate. Thus, when a beginner learns how to operate the rotary wing type carrier, the driving device can be used to drive the accelerator timely through the control of the automatic speed regulating device, and the rotary wing type carrier can fly stability so as to improve the learning effects of the beginner.

Description

Rotary wind type carrier operating system
Technical field
The utility model relates to a kind of operating system of training rotary wind type carrier beginner to operate the rotary wind type carrier, refers to especially a kind of rotary wind type carrier operating system.
Background technology
As U.S. Patent Bulletin number No. US5678999 disclosed a kind of rotary wind type training carrier, this carrier is gently navigate helicopter and connect an auxiliary unit of a kind of traditional one-seater, this auxiliary unit is through a fuselage by ㄇ font gate arch, below connect a base, this base below also arranges several wheels again.In when operation, rotating speed and the variation of two fin angles by a main rotor produce lift, make whereby this fuselage fly away from ground, and now this auxiliary unit atmospheric pressure pole can extend, but is unlikely to make this base built on stilts.
This case, owing to thering is this auxiliary merit unit, therefore if, when beginner's careless misoperation when using carrier, this carrier can be because there be the buffering effect of this atmospheric pressure pole of this auxiliary unit, and can avoids this carrier directly to fall ground and cause that the student is injured and carrier is impaired.But the operation of this carrier, still need to grope voluntarily and comprehension by the new person, its operate learning effect is limited.
The utility model content
The purpose of this utility model is to provide a kind of rotary wind type carrier operating system that can promote rotary wind type carrier beginner's operate learning effect.
The utility model rotary wind type carrier operating system, comprise a servicing unit, a rotary wind type carrier, a drive unit, and an automatic speed governing device.
This servicing unit comprises a base, a cylinder body that is arranged at this base, and a carriage release lever that can be connected in up or down this cylinder body.
This rotary wind type carrier comprises a carrier body that is connected in this carriage release lever, an engine that is arranged at this carrier body and there is a throttle, one is arranged at this carrier body and driven by this engine and the main rotor of rotation, be arranged at this carrier body to control the pull bar of this main rotor angle an energy pivot pendulum, one be arranged at this carrier body and be connected in this pull bar and this main rotor between the first coupling assembling, one can be arranged at rotationally this pull bar with this throttle of interlock and then control the handle of the rotating speed of this main rotor, and second coupling assembling be connected between this handle and this throttle.
This drive unit is arranged on this carrier body and can controls this throttle.
This automatic speed governing device comprises a CPU (central processing unit) that is electrically connected on this drive unit and can controls this drive unit start.
Rotary wind type carrier operating system of the present utility model, this servicing unit also comprises several wheels that are arranged at respectively this base.
Rotary wind type carrier operating system of the present utility model, also comprise a stop means that is arranged at this servicing unit, and can not move horizontally by spacing this servicing unit that makes.
Rotary wind type carrier operating system of the present utility model, this drive unit is the servo motor that is connected in this second coupling assembling.
Rotary wind type carrier operating system of the present utility model, this automatic speed governing device also comprises first sensor that is electrically connected on this CPU (central processing unit) and can detects the rotating speed of this main rotor.
Rotary wind type carrier operating system of the present utility model, this automatic speed governing device also comprises a starting switch that is arranged at this carrier body and is electrically connected on this CPU (central processing unit), when this starting switch is opened, this CPU (central processing unit) can be accepted the rotating speed of this main rotor of this first sensor detecting, and control this throttle via this drive unit, with so control the rotating speed of this main rotor.
Rotary wind type carrier operating system of the present utility model, this automatic speed governing device also comprises second sensor that is electrically connected on this CPU (central processing unit) and can detects the rotating speed of this engine.
Rotary wind type carrier operating system of the present utility model, this automatic speed governing device also comprises a rotating speed control change-over switch that is arranged at this carrier body and is electrically connected on this CPU (central processing unit).
Rotary wind type carrier operating system of the present utility model, this rotating speed control change-over switch can be controlled this main rotor and export with 100% rotating speed, or exports with 90% rotating speed.
Rotary wind type carrier operating system of the present utility model, also comprise a far-end control device, and this far-end control device comprises a controller that is connected in this CPU (central processing unit) in the wireless network mode.
Rotary wind type carrier operating system of the present utility model, this controller has a display interface, can show rotating speed, the rotating speed of this engine, the water temperature of this main rotor, and oil temperature.
Rotary wind type carrier operating system of the present utility model, this controller has an automatic speed regulation interface button, when starting this automatic speed regulation interface button, after this CPU (central processing unit) can receive the rotating speed of this main rotor, to drive this drive unit, control this throttle to adjust the rotating speed of this main rotor.
Rotary wind type carrier operating system of the present utility model, the container that the base of this servicing unit is an energy filling liquid.
The beneficial effects of the utility model are: utilize this servicing unit, this drive unit to coordinate with this automatic speed governing device, as the beginner during at this rotary wind type carrier of learning manipulation, allow control that this drive unit can be by this automatic speed governing device and in good time this throttle of driving, and allow this rotary wind type carrier fly safely and steadly, to promote beginner's results of learning.
The accompanying drawing explanation
Fig. 1 is the stereographic map of a preferred embodiment of the utility model rotary wind type carrier operating system;
Fig. 2 is a side view of this preferred embodiment;
Fig. 3 is a system block diagrams of this preferred embodiment;
Fig. 4 is a schematic diagram of this preferred embodiment, and a far-end control device is described;
Fig. 5 is an action schematic diagram of this preferred embodiment, and limited state of flight is described;
Fig. 6 is an action schematic diagram of this preferred embodiment, and not limited state of flight is described;
Fig. 7 is the process flow diagram of a preferred embodiment of the method for operating of the utility model rotary wind type carrier operating system.
Embodiment
Below in conjunction with drawings and Examples, the utility model is elaborated.
Consult Fig. 1, Fig. 2, and Fig. 3, a preferred embodiment of the utility model rotary wind type carrier operating system, comprise a servicing unit 2, stop means 3, rotary wind type carrier 4, drive unit 5, an automatic speed governing device 6, and a far-end control device 7.
This servicing unit 2 comprises that a base 21, one can be hubbed at the cylinder body 22 of this base 21, a carriage release lever 23 that can be connected in up or down this cylinder body 22 and be the ㄇ font rotationally, and several wheels 24 that are arranged at respectively this base 21.Wherein, this cylinder body 22 has an air valve 221, utilize this air valve 221 can be in order to the action this cylinder body 22 carried out pneumatic compression with disappointing step-down, thus, when inflating pressure, this carriage release lever 23 can have preferably stability and more not be vulnerable to the external force impact and move up and down, and when losing heart step-down, 23 of this carriage release levers are be vulnerable to the external force impact and move up and down.In this preferred embodiment, but the plastic bottle aspect that this base 21 is filling liquid, and this base 21 can lower the center of gravity to promote its stablizing effect at dress after water, if can weight reduction after water is released and be easy to mobile.
This stop means 3 is arranged at this servicing unit 2, and can spacing this servicing unit 2 can't move horizontally, and comprises several difference to rotate and adjust the support foot rest 31 of vertical height.While supportting overhead when adjusting the length of growing the aforementioned support foot rest 31 that is positioned at these base 21 belows by aforementioned wheel 24, this base 21 can be limited and can't be moved horizontally, as shown in Figure 5, and when adjusting the length of the short aforementioned support foot rest 31 that is positioned at these base 21 belows, and allow aforementioned support foot rest 31 break away from ground, and while allowing aforementioned wheel 24 contact with ground, this base 21 is not limited and can move horizontally, as shown in Figure 6.
This rotary wind type carrier 4 comprises that one connects and through in this carriage release lever 23 and have the carrier body 41 of a driving cabin 411, one is arranged at this carrier body 41 and has a throttle 421 and be positioned at the engine 42 at these driving cabin 411 rears, one is arranged at this carrier body 41 and is positioned at top and driven and the main rotor 43 of rotation by this engine 42, an empennage 44 that is arranged at this carrier body 41 and is positioned at rear, one can swingingly be arranged at this carrier body 41 and be positioned at this driving cabin 411 to control this main rotor 43 angles, with the pull bar 45 that produces raising force and then this carrier body 41 is moved up and down, one is arranged at this carrier body 41 and is connected in this pull bar 45 and the first coupling assembling 46 of 43 of this main rotors, one can be arranged at rotationally this pull bar 45 with this throttle 421 of interlock and then control the handle 47 of the rotating speed of this main rotor 43, second coupling assembling 48 that is connected in 421, this handle 47 and this throttle, one is arranged at this carrier body 41 and is positioned at this driving cabin 411 to control the steering yoke 49 at these main rotor 43 angles of inclination, an and instrument panel 40 that is arranged at this carrier body 41 and is positioned at this driving cabin 411.
This pull bar 45 is connected to main rotor 43 by this first coupling assembling 46, and can adjust the angle of two fins on this main rotor 43, when this pull bar 45 more up draws, the angle of the aforementioned fin of aforementioned main rotor 43 is larger, and now the aforementioned fin of this main rotor 43 is got over vertical ground.And transfer to the end when this pull bar 45, and the relative angle minimum of aforementioned fin, now the aforementioned fin of this main rotor 43 parallel ground almost, also can't produce raising force even if rotate.
In this preferred embodiment, this first coupling assembling 46 is all to explain with the multisection type connecting rod with this second coupling assembling 48, certainly also can use throttle line instead or electronically controlled mode is made control linkage, should not be limited with the disclosed content of this preferred embodiment.
What specify is, in this preferred embodiment, this rotary wind type carrier 4 is that the micro helicopter with one-seater explains, and certainly also can use the transport helicopter of two main rotors or other rotary wind type carrier instead, should not be limited with the disclosed content of this preferred embodiment.In addition, in this preferred embodiment, the angle of this main rotor 43 has through adjusting, and produces excessive raising force to avoid it when maximum angle is arranged in pairs or groups maximum speed, and the base of this servicing unit 2 21 is drawn high to built on stilts.
This drive unit 5 is arranged on this carrier body 41 and can controls this throttle 421.Wherein, in this preferred embodiment, this drive unit 5, for being connected in the servo motor of this second coupling assembling 48, certainly also can being used other instead and can receive the device replacement of controlling signal and producing corresponding mechanical force, should not be limited with the disclosed content of the present embodiment.Whereby, the driving of this throttle 421 can not terminated in utilize and rotate this handle 47 and implement.And when this drive unit 5 drives this throttle 421, because this second coupling assembling 48 links with this handle 47 mechanism to each other, therefore during this second coupling assembling 48 start, will certainly cause this handle 47 to rotate, feedback mechanism whereby, and allow the beginner can experience this drive unit 5 in the action of controlling this throttle 421.
This automatic speed governing device 6 comprises that one is arranged at this carrier body 41 and is electrically connected on this drive unit 5 and can controls the CPU (central processing unit) 61 of these drive unit 5 starts, first sensor 62 that is electrically connected on this CPU (central processing unit) 61 and can detects the rotating speed of this main rotor 43, second sensor 63 that is electrically connected on this CPU (central processing unit) 61 and can detects the rotating speed of this engine 42, a starting switch 64 that is arranged at this pull bar 45 of this carrier body 41 and is electrically connected on this CPU (central processing unit) 61, and one be arranged at this carrier body 41 and be positioned at this driving cabin 411 and be electrically connected on the rotating speed control change-over switch 65 of this CPU (central processing unit) 61.
Wherein, beginner in being sitting in this driving cabin 411 cuts this starting switch 64, when this starting switch 64 is opened, this CPU (central processing unit) 61 can accept the rotating speed of this main rotor 43 that this first sensor 62 detects, and can control this throttle 421 via this drive unit 5 and the second coupling assembling 48 and strengthen or reduce, with so control the rotating speed of this main rotor 43.On the other hand, when this starting switch 64 is opened, must select the numerical value that this rotating speed is controlled change-over switch 65 simultaneously, to allow this CPU (central processing unit) 61 can control this drive unit 5, and allow this drive unit 5 can drive this throttle 421, and allow the rotating speed of this main rotor 43 maintain a definite value, and in this preferred embodiment, this rotating speed control change-over switch 65 has two kinds of numerical value can be for switching, a kind of is can control this main rotor 43 to export with 100% rotating speed, and another kind is exported with 90% rotating speed for controlling this main rotor 43, certainly this rotating speed is controlled change-over switch 65 also can have three or the above numerical value can be for switching, or directly to input the mode of numerical value, should not be limited with the disclosed scope of this preferred embodiment.In addition, 100% rotating speed output in this preferred embodiment not represents the higher limit of rotating speed, but a reference rotation velocity, if this rotating speed is controlled change-over switch 65, is three numerical value can be for switching the time, also can change 90%, 100% into, 110% 3 kind of numerical value.When the beginner is switched this rotating speed control change-over switch 65, if during the pattern that selection is exported with 100% rotating speed, when the beginner controls the improper and rotating speed that causes this main rotor 43 of this handle 47 too fast (higher than 100%) or too when slow (lower than 100%), this CPU (central processing unit) 61 can drive this drive unit 5 starts, and then control this throttle 421 and allow the rotating speed of this main rotor 43 can maintain the output of 100% rotating speed, and this simultaneously, because the beginner is held on this handle 47, therefore can perceive the start of this handle 47, feedback action whereby, and allow the beginner can understand own operational shortcoming, thus, can promote widely effect in study.
Coordinate and consult Fig. 4 simultaneously, this far-end control device 7 comprises a controller 71 that is connected in this CPU (central processing unit) 61 in the wireless network mode.Wherein, in this preferred embodiment, this controller 71 is a Portable panel personal computer, and this controller 71 can be also that intelligent mobile phone or other can transmit the device of wireless signal certainly, should not be limited with the disclosed content of this preferred embodiment.During training, the coach can utilize this controller 71 to come far-end to control this rotary wind type carrier 4 or supervise this rotary wind type carrier 4.And, when this far-end control device 7 connects upper this CPU (central processing unit) 61, the beginner can't switch the starting switch 64 and rotating speed control change-over switch 65 of this rotary wind type carrier 4 voluntarily.That is to say, the control of this controller 71 is that the starting switch 64 be greater than on this rotary wind type carrier 4 is controlled change-over switch 65 with rotating speed, further avoids whereby the student to operate without authorization, and disengaging is trained control and caused danger.
This controller 71 has a display interface 711, an automatic speed regulation interface button 712, and an emergency circumstance interface button 713.This display interface 711 can show rotating speed, the rotating speed of this engine 42, the water temperature of this main rotor 43, and oil temperature, whereby, allows the coach can monitor the running situation of this rotary wind type carrier 4.And when starting this automatic speed regulation interface button 712, this rotary wind type carrier 4 that is controlled by this controller 71, and allow the coach can thoroughly by this controller 71, be set the rotating speed of this main rotor 43, after allowing this CPU (central processing unit) 61 can receive the rotating speed of this main rotor 43, to drive this drive unit 5 to control this throttle 421 to adjust the rotating speed of this main rotor 43, and then make this main rotor 43 maintain the rotating speed of expectation.This emergency circumstance interface button 713 can be in order to produce a virtual abnormality, for example, for rotating speed, the rotating speed of this engine 15, water temperature, the oil temperature of this main rotor 12 of virtual controlling, and terrain clearance in abnormality, for testing student's strain functipnal capability.In this preferred embodiment, this display interface 711, this automatic speed regulation interface button 712 and this emergency circumstance interface button 713 are to be incorporated into pattern user interface (Graphical User Interface, GUI) explain, can certainly use physical button or the replacement of knob collocation traditional monitor instead, should not be limited with the disclosed content of this preferred embodiment.
Consult Fig. 1, Fig. 3, and Fig. 7, a preferred embodiment of the method for operating of the utility model rotary wind type carrier operating system, be applicable to as aforementioned described this rotary wind type carrier operating system, and this method of operating comprises following steps:
Step 100: adjust aforementioned support foot rest 31, after allowing aforementioned wheel 24 break away from ground, with spacing this servicing unit 2 that makes, can't move horizontally, as shown in Figure 5, to allow this steering yoke 49 of beginner's Self-operating, this carriage release lever 23, and this handle 47, and then carry out the exercise of offline mode of VTOL (vertical take off and landing), pivot stud or the stagnant sky of this rotary wind type carrier 4 according to difficulty.And carry out above-mentioned various offline mode in, also can change the pressure size of this cylinder body 22 simultaneously, because this cylinder body 22 can produce stronger anchorage force when air pressure is large, therefore the student can reduce in operational difficulty, if the air pressure of this anti-cylinder body 22 reduces, and student's operation easier increases relatively.By allowing descending variation of these cylinder body 22 pressure, allow the student can be from the superficial to the deep, incremental and learn safely step 100 operation skill.And the beginner can start this starting switch 64 voluntarily, and select this rotating speed of switching to control change-over switch 65, this drive unit 5 can be controlled by this CPU (central processing unit) 61 and drive this throttle 421, allow the velocity of rotation of this main rotor 43 can maintain the output of certain proportion value, as the output of 100% or 90% rotating speed, thus, allow the beginner can be by the traction rotating force of 47 feedbacks of this handle, and know the operational shortcoming of controlling oneself, to facilitate improvement.On the other hand, the coach can utilize this far-end control device 7, and utilizes this display interface 711 to supervise rotating speed, the rotating speed of this engine 42, the water temperature of this main rotor 43, reaches oil temperature, and utilize this automatic speed regulation interface button 712 of startup, to control the offline mode of this rotary wind type carrier 4.And, also can utilize this emergency interface button 713, in time control these rotary wind type carrier 4 operating systems in a virtual emergency, allow the student how get rid of this emergency and to increase adaptability to changes from learning.Emergency comprises water temperature rising, oil temperature rising, engine failure etc.Under the security context formed being matched with this automatic speed governing device 6 by this auxiliary unit 2, the adaptability to changes of test student emergency treatment.Thus, allow the coach can understand the state of beginner operation, also can increase and the beginner between interaction, to increase in study interactive.
Step 200: adjust aforementioned support foot rest 31, and after making aforementioned support foot rest 31 unsettled, to allow aforementioned wheel 24 kiss the earths, and the moving horizontally of not spacing this servicing unit 2, as shown in Figure 6, to allow this rotary wind type carrier 4 together carry out horizontal shift by this servicing unit 2 of interlock, make the student can control this rotary wind type carrier 4 and carry out horizontal shift, also can synchronously carry out VTOL (vertical take off and landing) in process, turn to, or the exercise of the offline mode of level altitude, and carry out above-mentioned various offline mode in, also can change the pressure size of this cylinder body 22 simultaneously, allow descending variation of these cylinder body 22 pressure, allow the student can be from the superficial to the deep, incremental and learn safely step 200 operation skill.Same, the beginner can start this starting switch 64 voluntarily, and select this rotating speed of switching to control change-over switch 65, this drive unit 5 can be controlled by this CPU (central processing unit) 61 and drive this throttle 421, allow the velocity of rotation of this main rotor 43 can maintain the output of certain proportion value, the rotating speed output as 100% or 90%, thus, allow the beginner can be by the feedback start of this handle 47, and know the operational shortcoming of controlling oneself, to facilitate improvement.On the other hand, the coach can utilize this far-end control device 7, and utilizes this display interface 711 to supervise rotating speed, the rotating speed of this engine 42, the water temperature of this main rotor 43, reaches oil temperature, and utilize this automatic speed regulation interface button 712 of startup, to control the offline mode of this rotary wind type carrier 4.And, also can utilize this emergency interface button 713, in time control these rotary wind type carrier 4 operating systems in a virtual emergency, allow the student how get rid of this emergency and to increase adaptability to changes from learning.Emergency comprises water temperature rising, oil temperature rising, engine failure etc.Under the security context formed being matched with this automatic speed governing device 6 by this auxiliary unit 2, the adaptability to changes of test student emergency treatment.Thus, allow the coach can understand the state of beginner operation, also can increase and the beginner between interaction, to increase in study interactive.
In sum, the utility model rotary wind type carrier operating system has following advantages and effect:
One, utilize this servicing unit 2, drive unit 5 to coordinate with this automatic speed governing device 6, as the beginner during at this rotary wind type carrier 4 of learning manipulation, allow control that this drive unit 5 can be by this automatic speed governing device 6 and in good time this throttle 421 of driving, and allow this rotary wind type carrier 4 fly safely and steadly, to promote beginner's results of learning.
Two, can be connected in this CPU (central processing unit) 61 by this far-end control device 7, the state when coach can be grasped the beginner and flies, and can control the offline mode of this rotary wind type carrier 4, to increase interaction effect in study.

Claims (13)

1. a rotary wind type carrier operating system, comprise a servicing unit, a rotary wind type carrier, a drive unit, and an automatic speed governing device, it is characterized in that:
This servicing unit comprises a base, a cylinder body that is arranged at this base, and a carriage release lever that can be connected in up or down this cylinder body;
This rotary wind type carrier comprises a carrier body that is connected in this carriage release lever, an engine that is arranged at this carrier body and there is a throttle, one is arranged at this carrier body and driven by this engine and the main rotor of rotation, be arranged at this carrier body to control the pull bar of this main rotor angle an energy pivot pendulum, one be arranged at this carrier body and be connected in this pull bar and this main rotor between the first coupling assembling, one can be arranged at rotationally this pull bar with this throttle of interlock and then control the handle of the rotating speed of this main rotor, and second coupling assembling be connected between this handle and this throttle,
This drive unit is arranged on this carrier body and can controls this throttle;
This automatic speed governing device comprises a CPU (central processing unit) that is electrically connected on this drive unit and can controls this drive unit start.
2. rotary wind type carrier operating system as claimed in claim 1, it is characterized in that: this servicing unit also comprises several wheels that are arranged at respectively this base.
3. rotary wind type carrier operating system as claimed in claim 2, is characterized in that: also comprise a stop means that is arranged at this servicing unit, and can not move horizontally by spacing this servicing unit that makes.
4. rotary wind type carrier operating system as claimed in claim 3, it is characterized in that: this drive unit is the servo motor that is connected in this second coupling assembling.
5. rotary wind type carrier operating system as claimed in claim 1 is characterized in that: this automatic speed governing device also comprises first sensor that is electrically connected on this CPU (central processing unit) and can detects the rotating speed of this main rotor.
6. rotary wind type carrier operating system as claimed in claim 5, it is characterized in that: this automatic speed governing device also comprises a starting switch that is arranged at this carrier body and is electrically connected on this CPU (central processing unit), when this starting switch is opened, this CPU (central processing unit) can be accepted the rotating speed of this main rotor of this first sensor detecting, and control this throttle via this drive unit, with so control the rotating speed of this main rotor.
7. rotary wind type carrier operating system as claimed in claim 1 is characterized in that: this automatic speed governing device also comprises second sensor that is electrically connected on this CPU (central processing unit) and can detects the rotating speed of this engine.
8. rotary wind type carrier operating system as claimed in claim 7 is characterized in that: this automatic speed governing device also comprises that a rotating speed that is arranged at this carrier body and is electrically connected on this CPU (central processing unit) controls change-over switch.
9. rotary wind type carrier operating system as claimed in claim 8 is characterized in that: this rotating speed is controlled change-over switch can control this main rotor with 100% rotating speed output, or with 90% rotating speed output.
As claim 1 to the described rotary wind type carrier of claim 9 any one operating system, it is characterized in that: also comprise a far-end control device, this far-end control device comprises a controller that is connected in this CPU (central processing unit) in the wireless network mode.
11. rotary wind type carrier operating system as claimed in claim 10 is characterized in that: this controller has a display interface, can show rotating speed, the rotating speed of this engine, the water temperature of this main rotor, and oil temperature.
12. rotary wind type carrier operating system as claimed in claim 10, it is characterized in that: this controller has an automatic speed regulation interface button, when starting this automatic speed regulation interface button, after this CPU (central processing unit) can receive the rotating speed of this main rotor, to drive this drive unit, control this throttle to adjust the rotating speed of this main rotor.
13. rotary wind type carrier operating system as claimed in claim 1, is characterized in that: the container that the base of this servicing unit is an energy filling liquid.
CN2013203600535U 2013-06-21 2013-06-21 Rotary wing type carrier operating system Expired - Fee Related CN203325254U (en)

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Application Number Priority Date Filing Date Title
CN2013203600535U CN203325254U (en) 2013-06-21 2013-06-21 Rotary wing type carrier operating system

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Application Number Priority Date Filing Date Title
CN2013203600535U CN203325254U (en) 2013-06-21 2013-06-21 Rotary wing type carrier operating system

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CN203325254U true CN203325254U (en) 2013-12-04

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CN2013203600535U Expired - Fee Related CN203325254U (en) 2013-06-21 2013-06-21 Rotary wing type carrier operating system

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104240552A (en) * 2013-06-21 2014-12-24 威翔航空科技股份有限公司 Rotary wing type carrier operating system and operating method thereof

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104240552A (en) * 2013-06-21 2014-12-24 威翔航空科技股份有限公司 Rotary wing type carrier operating system and operating method thereof

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C14 Grant of patent or utility model
GR01 Patent grant
C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20160802

Address after: Argentina Province, Buenos Aires

Patentee after: CICARE S.A.

Address before: Taichung City, Taiwan, China

Patentee before: AEROJONES AVIATION TECHNOLOGY CO., LTD.

Patentee before: CICARE S.A.

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: 20131204

Termination date: 20180621