CN109764106A - Dynamic transfer system - Google Patents

Dynamic transfer system Download PDF

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Publication number
CN109764106A
CN109764106A CN201711104337.7A CN201711104337A CN109764106A CN 109764106 A CN109764106 A CN 109764106A CN 201711104337 A CN201711104337 A CN 201711104337A CN 109764106 A CN109764106 A CN 109764106A
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power
transmission
power transmission
load
transmission end
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CN201711104337.7A
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CN109764106B (en
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林瑤章
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Taiwan Aircraft Co ltd
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Individual
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Abstract

A kind of dynamic transfer system, including power source, the first power transmission distributor, the first load and the second load.The power transmission of power source output is to the first power transmission distributor, it is divided into the first transmission power and the second transmission power via the first power transmission distributor, and it is transmitted separately to the first load and the second load, the transmission direction that power inputs the first power intake is perpendicular to the transmission direction of the first transmission power and the second transmission power, and the transmission direction of the first transmission power is opposite with the transmission direction of the second transmission power.

Description

Dynamic transfer system
Technical field
The present invention relates to a kind of dynamic transfer systems, more particularly to one kind to transmit power towards at least two different directions Dynamic transfer system.
Background technique
Fly up into the sky the empty dream for being not only the mankind and a kind of travel pattern of very effective rate, has and quickly reaches purpose The efficiency on ground, therefore, it is removable in addition to due to space to estrangement caused by people, so, flight be not only have amusement and commercial affairs Property more has other application great demand.
For Fixed Wing AirVehicle, a large amount of personnel and cargo can be no doubt carried, but this kind of carrier needs to grow very much Runway and a large amount of relevant launching and recovering equipment, therefore be confined to airport landing, to overcome this limitation, in addition develop rotation Rotor aircraft, such as helicopter, can be in the range VTOL of small area.But it even can be with the rotor of VTOL Aircraft is still to the airplane parking area of setting equivalent area, can not be as the upper and lower carrying everywhere of the vehicle on ground, and is intensively building In the big city of object, helicopter narrow still difficult to get access and common roof.
Therefore, existing R&D team sets about researching and developing single vertical translation aircraft at present, can be intensive and empty in building Between narrow metropolitan area use, the single vertical translation aircraft some being currently known is using single propeller, and in order to obtain Multiple propellers also can be set in biggish thrust, it is however generally that the pattern for having twin screw and quadruple screw propeller etc. different.So And the volume of single vertical translation aircraft is fairly limited, it, necessarily can not be such as fixed-wing if multiple propellers are arranged Aircraft is the same, and each propeller configures an other engine, but is desirable for an engine while driving multiple propellers, Therefore how the power of engine, which distributes, is transmitted to each propeller and is an important issue.
Summary of the invention
The present invention provides a kind of dynamic transfer system, and multiple power distribution transmitting devices are arranged, the power of power source is put down It distributes and is delivered to multiple loads.And it is applied to light weight flight carrier, such as individual lift device, it can be by the power benefit of engine It is fifty-fifty distributed with power gear box and is delivered to multiple propellers and generates thrust.
Other objects and advantages of the present invention can from disclosed herein technical characteristic in be further understood.
Be up to above-mentioned one or partly or entirely purpose or other purposes, dynamic transfer system provided by the present invention One embodiment includes power source, the first power transmission distributor, the first load and the second load.Power source has power defeated Outlet, to output power, the first power transmission distributor has the first power intake, the first power transmission end and the Two power transmission ends, the first power intake are coupled to the power output end of power source, power ultromotivity output end input first After power intake, it is divided into the first transmission power and the second transmission power, the first transmission power is sent to the transmission of the first power End, the second transmission power are sent to the second power transmission end, and the first load coupled is in the first power transmission end, the first transmission power The first load of input, the second load coupled is in the first power transmission end, second transmission power the second load of input.
In one embodiment of this invention, dynamic transfer system of the invention further includes the second power transmission distributor, With the second power intake, third power transmission end and the 4th power transmission end, the second power intake is coupled to first Power transmission end, third power transmission end are coupled to the first load, and the first transmission power inputs second from the first power transmission end Power intake, and via the first load of third power transmission end driving.
In one embodiment of this invention, dynamic transfer system of the invention further includes third power transmission distributor, With third power intake, the 5th power transmission end and the 6th power transmission end, third power intake is coupled to second Power transmission end, the 5th power transmission end are coupled to the second load, and the second transmission power inputs third from the second power transmission end Power intake, and via the second load of the 5th power transmission end driving.
In one embodiment of this invention, dynamic transfer system of the invention further include the second power transmission distributor with And third load, the second power transmission distributor have the second power intake, third power transmission end and the 4th power Transmission end, the second power intake are coupled to the first power transmission end, and third power transmission end is coupled to the first load, and third is negative Load is coupled to the 4th power transmission end and is divided into after the first transmission power inputs the second power intake from the first power transmission end Third transmits power and the 4th transmission power, and third transmits power and is sent to the first load via third power transmission end, the Four transmission power are sent to third load via the 4th power transmission end.
In one embodiment of this invention, dynamic transfer system of the invention further include the second power transmission distributor with And third load, the second power transmission distributor have the second power intake, third power transmission end and the 4th power Transmission end, the second power intake are coupled to the first power transmission end, and third power transmission end is coupled to the first load, and third is negative Load is coupled to the 4th power transmission end and is divided into after the first transmission power inputs the second power intake from the first power transmission end Third transmits power and the 4th transmission power, and third transmits power and is sent to the first load via third power transmission end, the Four transmission power are sent to third load via the 4th power transmission end.
In one embodiment of this invention, dynamic transfer system further includes that the first transmission shaft, second driving shaft and third pass Moving axis, the power are torsion, are with the connection of the first transmission shaft, the first power between power output end and the first power intake Transmission end is that the first load is coupled to via second driving shaft, and the second power transmission end is to be coupled to second via third transmission shaft Load.
In one embodiment of this invention, power source includes engine, and the first power transmission distributor includes the first power Gearcase, the first power gear box include the first bevel gear, the second bevel gear and third bevel gear, and the first bevel gear is engaged in Second bevel gear and third bevel gear, the first umbrella tooth are connected to the first transmission shaft, the second bevel gear be connected to second driving shaft and Third bevel gear is connected to third transmission shaft.
Dynamic transfer system of the invention is by using the first power transmission distributor can be by the power court of power source Two different direction transmission, and the power transmitted towards a direction can recycle the second power transmission distributor or third dynamic Power transmission distributor is transmitted in two different loads towards other two different direction respectively, such power source Power can be transmitted to multiple loads.
The above description is only an overview of the technical scheme of the present invention, in order to better understand the technical means of the present invention, And it can be implemented in accordance with the contents of the specification, and in order to allow above and other objects, features and advantages of the invention can It is clearer and more comprehensible, it is special below to lift preferred embodiment, and cooperate attached drawing, detailed description are as follows.
Detailed description of the invention
Fig. 1 is the schematic diagram of an embodiment of dynamic transfer system of the invention.
Specific embodiment
For the present invention aforementioned and other technology contents, feature and effect, it is following cooperation with reference to schema one preferably In the detailed description of embodiment, can clearly it present.The direction term being previously mentioned in following embodiment, such as: upper and lower, left, It is right, front or rear etc., it is only the direction with reference to annexed drawings.Therefore, the direction term used is intended to be illustrative and not intended to limit The present invention.Referring to Fig. 1, it indicates the dynamic transfer system of one embodiment of the invention.The dynamic transfer system 100 of the present embodiment Including power source 10, the first power transmission distributor 20, first load 30 and the second load 40.Power source 10 has power Output end 12, to output power F, there is the first power transmission distributor 20 first power intake 22, the first power to pass Sending end 24 and the second power transmission end 26, the first power intake 22 are coupled to the power output end 12 of power source 10, power F After ultromotivity output end input 12 is input to the first power intake 22, it is divided into the transmission power of the first transmission power F1 and second F2, the first transmission power F1 are sent to the first power transmission end 24, and the second transmission power F2 is sent to the second power transmission end 26, First load 30 is coupled to the first power transmission end 24, and the first transmission power F1 is loaded from the first power transmission end 24 input first 30, the second load 40 is coupled to the second power transmission end 26, and the second transmission power F2 inputs second from the second power transmission end 26 Load 40, in the present embodiment, the transmission direction that power F inputs the first power intake 22 are perpendicular to the first transmission power F1 And second transmission power F2 transmission direction, and first transmission power F1 transmission direction with second transmission power F2 transmission Direction is opposite.
In the present embodiment, power source 10 includes engine 110, and the power F that engine 110 exports is torsion, power transmission system System 100 for example further includes the first transmission shaft L1, second driving shaft L2 and third transmission shaft L3.Power output end 12 and the first power It can be linked between input terminal 22 with the first transmission shaft L1, the first power transmission end 24 can be coupled to first via second driving shaft L2 Load 30, the second power transmission end 26 can be coupled to the second load 40, the first power transmission distribution dress via third transmission shaft L3 20 are set for example including the first power gear box 120, the first power gear box 120 includes the first bevel gear 122, the second bevel gear 124, third bevel gear 126 and one the 4th bevel gear 128, the first bevel gear 122 are engaged in the second bevel gear 124 and third umbrella Gear 126, the 4th bevel gear 128 and the first bevel gear 122 are oppositely arranged and are engaged in the second bevel gear 124 and third umbrella Gear 126, the first umbrella tooth 122 are connected to the first transmission shaft L1, and the second bevel gear 124 is connected to second driving shaft L2 and third umbrella Gear 126 is connected to third transmission shaft L3, and the 4th bevel gear 128 is, for example, an idle pulley, with the second bevel gear of balance 124 with The rotation of third bevel gear 126, the torsion ultromotivity output end 12 (output shaft) that engine 110 generates whereby is via the first transmission shaft L1 is transmitted to the input shaft (the first power intake 22) of the first bevel gear 122 of the first power gear box 120, makes first whereby Bevel gear 122 rotates and rotates with the second bevel gear 124 with third bevel gear 126, and power is divided into the first transmission and is moved The transmission power F2 of power F1 and second, and respectively from the output shaft of the second bevel gear 124 (the first power transmission end 24) and third It is negative that the output shaft (the second power transmission end 26) of bevel gear 126 via second driving shaft L2 and third transmission shaft L3 is transmitted to first Load 30 and the second load 40, in the present embodiment, the first load 30 are propellers, and the second load 40 is also propeller.
In addition, the first power transmission end 24 may be used also other than second driving shaft L2 in the longer situation of transmission range More increase by the 4th transmission shaft L4 and be coupled to the first load 30, is linked between second driving shaft L2 and the 4th transmission shaft L4 with first axle Part C1 connection, the second power transmission end 26 can also more increase by the 5th transmission shaft L5 and be coupled to other than third transmission shaft L3 Two loads 40, with the second axis connecting piece C2 connection between third transmission shaft L3 and the 5th transmission shaft L5.In the present embodiment, first Axis connecting piece C1 can be shaft coupling, and the second axis connecting piece C2 can be shaft coupling.In another embodiment, first axle connecting piece C1 can be universal joint, and the second axis connecting piece C2 can be universal joint.
In the present embodiment, dynamic transfer system 100 may also include the second power transmission distributor 50, and the second power passes Defeated distributor 50 has the second power intake 52, third power transmission end 54 and the 4th power transmission end 56, and second is dynamic Power input terminal 52 is coupled to the first power transmission end 24, and third power transmission end 54 is coupled to the first load 30, and the first transmission is dynamic Power F1 inputs the second power intake 52 from the first power transmission end 24, and it is negative via third power transmission end 54 to be transmitted to first 30 are carried, in the present embodiment, the second power transmission distributor 50 is set between the load of the 4th transmission shaft L4 and first 30, the For two power transmission distributors 50 for example including the second power gear box 150, the second power gear box 150 includes most umbrella tooths Wheel, the structure of the second power gear box 150 can be structure identical with the first power gear box 120 or be different knot Structure, in the present embodiment, the 4th transmission shaft L4 are connected to the input shaft of the bevel gear of the second power gear box 150, by these Bevel gear engaged transmission, in the present embodiment, it is vertical that the first transmission power F1, which inputs the transmission direction of the second power intake 52, Directly in third power transmission end 54 and the power transmission direction of the 4th power transmission end 56, and third power transmission end 54 is dynamic Power transmission direction is contrary with the power transmission of the 4th power transmission end 56, the power transmission direction of third power transmission end 54 It is identical as the power input transmission direction of the first power intake 12.In this way, the first transmission power F1 inputs the second power gear After box 150, it is transmitted to the first load 30 via the second power gear box 150, i.e. driving propeller rotational, generates thrust.
Similarly, dynamic transfer system 100 may also include third power transmission distributor 60, the distribution of third power transmission Device 60 has third power intake 62, the 5th power transmission end 64 and the 6th power transmission end 66, the input of third power End 62 is coupled to the second power transmission end 64, and the 5th power transmission end 66 is coupled to the second load 40, and the second transmission power F2 is certainly Second power transmission end 26 inputs third power intake 62, and loads 40 via the 5th power transmission end 64 driving second, In the present embodiment, third power transmission distributor 60 is set between the load of the 5th transmission shaft L5 and second 40, third power Transmitting distributor 60 includes third power gear box 160, and third power gear box 160 includes most bevel gears, and third is dynamic The structure of powershift gear box 160 can be structure identical with the first power gear box 120 or be different structure, in this implementation In example, the 5th transmission shaft L5 is connected to the input shaft of the bevel gear of third power gear box 160, engages and passes by these bevel gears Dynamic, in the present embodiment, the transmission direction of the second transmission power F2 input third power intake 62 is perpendicular to the 5th power The power transmission direction of transmission end 64 and the 6th power transmission end 66, and the power transmission direction of the 5th power transmission end 64 with The power transmission of 6th power transmission end 66 is contrary, the power transmission direction of the 5th power transmission end 64 and power input the The transmission direction of one power intake 12 is identical.
In the present embodiment, dynamic transfer system 100 may also include third load 70, and it is dynamic that third load 70 is coupled to the 4th Power transmission end 56, the first transmission power F1 are moved from the second of the second power transmission distributor 50 of the first power transmission end 24 input After power input terminal 52, it is divided into the third transmission power F4 of transmission power F3 and the 4th, third transmits power F3 via the second power The third power transmission end 54 of transmission distributor 50 is sent to the first load 30, and the 4th transmission power F4 is passed via the second power 4th power transmission end 56 of defeated distributor 50 is sent to third load 70, and in the present embodiment, third load 70 is spiral Paddle, and the second power transmission distributor 50 is then power gear box as described above.
In addition, in the present embodiment, dynamic transfer system 100 may also include the first speed change gear 80, the first speed change gear 80 the 4th power transmission ends 56 of coupling and third load 70, the 4th transmission power F4 are transmitted simultaneously via the 4th power transmission end 56 70 are loaded to third by the way that the first speed change gear is after 80s, in the present embodiment, the first speed change gear 80 includes planetary gear train, by The revolving speed of the 4th power transmission end 56 (output shaft of the bevel gear of power gear box) can be changed by planetary gear train, and makes The revolving speed of three loads 70 is different from the revolving speed of the first load 30, and in the present embodiment, the first speed change gear 80 is accelerator, makes The revolving speed of third load 70 is the multiple of the revolving speed of the first load 30.
In the present embodiment, dynamic transfer system 100 may also include the 4th load 90, and it is dynamic that the 4th load 90 is coupled to the 6th Power transmission end 66 after second transmission power F2 inputs third power intake 62 from the second power transmission end 26, is divided into the 5th biography The transmission of defeated power F5 and the 6th power F6, the 5th transmission power F5 are sent to the second load via the 5th power transmission end 64 40, the 6th transmission power F6 is sent to the 4th load 90 via the 6th power transmission end 66, in the present embodiment, the 4th load 90 It is propeller, and third power transmission distributor 60 is then power gear box as described above.
In the present embodiment, dynamic transfer system 100 may also include the second speed change gear 170, coupling the 6th power transmission End 66 and the 4th load 90, the 6th transmission power F6 are conveyed to and through the second speed change gear via the 6th power transmission end 66 To the 4th load 90 after 170.In the present embodiment, the second speed change gear 170 includes planetary gear train, can by planetary gear train To change the revolving speed of the 6th power transmission end 66 (output shaft of the bevel gear of power gear box), and make the revolving speed of the 4th load 90 Different from the revolving speed of the second load 40, in the present embodiment, the second speed change gear 170 is accelerator, makes the 4th load 90 Revolving speed is the multiple of the revolving speed of the second load 40.
Dynamic transfer system 100 of the invention is by using the first power transmission distributor 20 (power gear box 120) The power of power source 10 (engine 110) can be transmitted in two different directions, and the power transmitted towards a direction can be again It is passed respectively towards other two different direction using the second power transmission distributor 50 or third power transmission distributor 60 It transports in two different loads, the power of such power source 10 can be transmitted to multiple loads.Fly when being applied to one When row device, the power of engine 110 can be transmitted to 110 or so two side of engine two tool propellers (twin screw type, does not use Third load 70 with the 4th load 90) or the power of engine 110 can be transmitted to 110 or so two side of engine four have spiral shells Revolve paddle (quadruple screw propeller type, as shown in this embodiment), it might even be possible to be applied to the aircraft for having more than four propellers. In addition, the length of transmission shaft can be increased using first axle connecting piece C1 and the second axis connecting piece C2, simultaneously because meeting when flight There is the problem of vibration, is also easier receiving vibration using the structure that axis connecting piece links two transmission shafts and is hardly damaged.
The above described is only a preferred embodiment of the present invention, be not intended to limit the present invention in any form, though So the present invention has been disclosed as a preferred embodiment, and however, it is not intended to limit the invention, any technology people for being familiar with this profession Member, without departing from the scope of the present invention, when the method and technique content using the disclosure above make it is a little more Equivalent embodiment that is dynamic or being modified to equivalent variations, but anything that does not depart from the technical scheme of the invention content, according to the present invention Technical spirit any simple modification, equivalent change and modification to the above embodiments, still fall within technical solution of the present invention In the range of.

Claims (20)

1. a kind of dynamic transfer system characterized by comprising
Power source has power output end, to output power;
First power transmission distributor has the first power intake, the first power transmission end and the second power transmission end, First power intake is coupled to the power output end of the power source, and it is first dynamic which from the power output end inputs this After power input terminal, it is divided into the first transmission power and the second transmission power, which is sent to first power biography Sending end, the second transmission power are sent to the second power transmission end;
First load, is coupled to the first power transmission end, the first transmission power from the first power transmission end input this One load;And
Second load, is coupled to the second power transmission end, the second transmission power from the second power transmission end input this Two loads.
2. dynamic transfer system according to claim 1, which is characterized in that the power inputs first power intake Transmission direction is perpendicular to the transmission direction of the first transmission power and the second transmission power, and the first transmission power Transmission direction is opposite with the transmission direction of the second transmission power.
3. dynamic transfer system according to claim 1, which is characterized in that the dynamic transfer system further includes second dynamic Power transmits distributor, which is coupled to the first power transmission end by the second power transmission distributor, In the second power transmission distributor have the second power intake, third power transmission end and the 4th power transmission end, Second power intake is coupled to the first power transmission end, which is coupled to first load, this One transmission power inputs second power intake from the first power transmission end, and should via third power transmission end driving First load.
4. dynamic transfer system according to claim 3, which is characterized in that the first transmission power inputs second power The transmission direction of input terminal is perpendicular to the power transmission direction of the third power transmission end and the 4th power transmission end, and The power transmission direction of the third power transmission end is contrary with the power transmission of the 4th power transmission end, the third power The power transmission direction of transmission end is identical as the transmission direction that the power inputs first power intake.
5. dynamic transfer system according to claim 2, which is characterized in that the dynamic transfer system further includes that third is dynamic Power transmits distributor, which is coupled to the second power transmission end by the third power transmission distributor, the Three power transmission distributors have third power intake, the 5th power transmission end and the 6th power transmission end, the third Power intake is coupled to the second power transmission end, and the 5th power transmission end is coupled to second load, second transmission Power inputs the third power intake from the second power transmission end, and drives this second negative via the 5th power transmission end It carries.
6. dynamic transfer system according to claim 5, which is characterized in that the second transmission power inputs the third power The transmission direction of input terminal is perpendicular to the power transmission direction of the 5th power transmission end and the 6th power transmission end, and The power transmission direction of 5th power transmission end is contrary with the power transmission of the 6th power transmission end, the 5th power The power transmission direction of transmission end is identical as the transmission direction that the power inputs first power intake.
7. dynamic transfer system according to claim 1, which is characterized in that the dynamic transfer system further includes second dynamic Power transmit distributor and third load, this first load by the second power transmission distributor be coupled to this first move Power transmission end, the second power transmission distributor have the second power intake, third power transmission end and the 4th power Transmission end, second power intake are coupled to the first power transmission end, and it is first negative which is coupled to this Carry, the third load coupled in the 4th power transmission end, the first transmission power from the first power transmission end input this After two power intakes, it is divided into third transmission power and the 4th transmission power, the third transmits power via the third power Transmission end is sent to first load, and the 4th transmission power is sent to third load via the 4th power transmission end.
8. dynamic transfer system according to claim 7, which is characterized in that the dynamic transfer system further includes the first change Speed variator couples the 4th power transmission end and third load, and the 4th transmission power is via the 4th power transmission end It is conveyed to and through after first speed change gear to the third and loads.
9. dynamic transfer system according to claim 8, which is characterized in that the second power transmission distributor includes the Two power gear boxes, the second power gear box include most bevel gears, those bevel gears are engaged with each other, and first speed change For device for accelerator and including planetary gear train, third load is propeller.
10. dynamic transfer system according to claim 8, which is characterized in that the dynamic transfer system further includes third Power transmission distributor and the 4th load, this second load by the third power transmission distributor be coupled to this second Power transmission end, the third power transmission distributor have third power intake, the 5th power transmission end and the 6th dynamic Power transmission end, the third power intake are coupled to the second power transmission end, the 5th power transmission end be coupled to this second Load, the 4th load coupled is in the 6th power transmission end, and input should from the second power transmission end for the second transmission power After third power intake, it is divided into the 5th transmission power and the 6th transmission power, the 5th transmission power is dynamic via the 5th Power transmission end is sent to second load, and the 6th transmission power is sent to the 4th load via the 6th power transmission end.
11. dynamic transfer system according to claim 10, which is characterized in that the dynamic transfer system also further includes Two speed change gears, couple the 6th power transmission end and the 4th load, and the 6th transmission power is passed via the 6th power Sending end is conveyed to and through after second speed change gear to the 4th load.
12. dynamic transfer system according to claim 11, which is characterized in that the third power transmission distributor includes Third power gear box, the third power gear box include most bevel gears, those bevel gears are engaged with each other, and second change Quick-mounting is set to accelerator and including planetary gear train, and the 4th load is propeller.
13. dynamic transfer system according to claim 7, which is characterized in that the dynamic transfer system further includes third Power transmission distributor and the 4th load, this second load by the third power transmission distributor be coupled to this second Power transmission end, the third power transmission distributor have third power intake, the 5th power transmission end and the 6th dynamic Power transmission end, the third power intake are coupled to the second power transmission end, the 5th power transmission end be coupled to this second Load, the 4th load coupled is in the 6th power transmission end, and input should from the second power transmission end for the second transmission power After third power intake, it is divided into the 5th transmission power and the 6th transmission power, the 5th transmission power is dynamic via the 5th Power transmission end is sent to second load, and the 6th transmission power is sent to the 4th load via the 6th power transmission end.
14. dynamic transfer system according to claim 13, which is characterized in that the dynamic transfer system also further includes Two speed change gears, couple the 6th power transmission end and the 4th load, and the 6th transmission power is passed via the 6th power Sending end is conveyed to and through after second speed change gear to the 4th load.
15. dynamic transfer system according to claim 14, which is characterized in that the third power transmission distributor includes Third power gear box, the third power gear box include most bevel gears, those bevel gears are engaged with each other, and second change Quick-mounting is set to accelerator and including planetary gear train, and the 4th load is propeller.
16. according to claim 1 to 15 described in any item dynamic transfer systems, which is characterized in that the power is torsion, described Dynamic transfer system further includes the first transmission shaft, second driving shaft and third transmission shaft, the power output end and first power Be between input terminal with first transmission shaft connection, the first power transmission end be coupled to via the second driving shaft this first Load, the second power transmission end are that second load is coupled to via the third transmission shaft.
17. dynamic transfer system according to claim 16, which is characterized in that the dynamic transfer system further includes the 4th Transmission shaft, the 5th transmission shaft, first axle connecting piece and the second axis connecting piece, the first power transmission end are more passed via the 4th Moving axis is coupled to first load, and with first axle connecting piece connection between the second driving shaft and the 4th transmission shaft, this Two power transmission ends are more coupled to second load via the 5th transmission shaft, between the third transmission shaft and the 5th transmission shaft With the second axis connecting piece connection.
18. dynamic transfer system according to claim 17, which is characterized in that the first axle connecting piece is shaft coupling, should Second axis connecting piece is shaft coupling.
19. dynamic transfer system according to claim 16, which is characterized in that the power source includes engine, this is first dynamic Power transmit distributor include the first power gear box, the first power gear box include the first bevel gear, the second bevel gear with And third bevel gear, first bevel gear are engaged in second bevel gear and the third bevel gear, which is connected to this First transmission shaft, which is connected to the second driving shaft and the third bevel gear is connected to the third transmission shaft.
20. dynamic transfer system according to claim 16, which is characterized in that first load is propeller, this second Load is propeller.
CN201711104337.7A 2017-11-10 2017-11-10 Power transmission system Active CN109764106B (en)

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103991539A (en) * 2014-06-13 2014-08-20 国家电网公司 Device for driving multiple rotors of airplane
CN104859854A (en) * 2015-04-16 2015-08-26 北京航空航天大学 Heavy-load low-structure-complexity double-coaxial-twin-rotor unmanned aerial vehicle
CN205396531U (en) * 2016-03-17 2016-07-27 山西施普乐航空植保科技有限公司 Electric control oil moves many rotor unmanned aerial vehicle
CN205633039U (en) * 2016-03-28 2016-10-12 冯江 Oil moves many rotors of planetary gear train differential formula agricultural and sprays aircraft
CN206125448U (en) * 2016-10-11 2017-04-26 北京深远世宁科技有限公司 Oil moves coaxial many rotor unmanned aerial vehicle
CN106956770A (en) * 2017-05-08 2017-07-18 莆田市双普信息科技有限公司 A kind of aircraft active differential mechanism speed adjusting gear

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103991539A (en) * 2014-06-13 2014-08-20 国家电网公司 Device for driving multiple rotors of airplane
CN104859854A (en) * 2015-04-16 2015-08-26 北京航空航天大学 Heavy-load low-structure-complexity double-coaxial-twin-rotor unmanned aerial vehicle
CN205396531U (en) * 2016-03-17 2016-07-27 山西施普乐航空植保科技有限公司 Electric control oil moves many rotor unmanned aerial vehicle
CN205633039U (en) * 2016-03-28 2016-10-12 冯江 Oil moves many rotors of planetary gear train differential formula agricultural and sprays aircraft
CN206125448U (en) * 2016-10-11 2017-04-26 北京深远世宁科技有限公司 Oil moves coaxial many rotor unmanned aerial vehicle
CN106956770A (en) * 2017-05-08 2017-07-18 莆田市双普信息科技有限公司 A kind of aircraft active differential mechanism speed adjusting gear

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