CN207374646U - The long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of heavy－duty - Google Patents
The long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of heavy－duty Download PDFInfo
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- CN207374646U CN207374646U CN201721430428.5U CN201721430428U CN207374646U CN 207374646 U CN207374646 U CN 207374646U CN 201721430428 U CN201721430428 U CN 201721430428U CN 207374646 U CN207374646 U CN 207374646U
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Abstract
The utility model discloses a kind of long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of heavy－duty, including：Servomotor, motor, propeller A, propeller B, rocking arm A, rocking arm B, fuel tank, battery pack, undercarriage, flight control system and fuselage, servomotor is fixedly connected by rocking arm A with fuselage, propeller A is mounted on servomotor, for providing lift for aircraft, motor is fixedly connected by rocking arm B with fuselage, propeller B is mounted on motor, for adjusting the posture of aircraft, B number of propeller A and propeller is identical and is arranged alternately, undercarriage is symmetrically mounted on the both sides of fuselage, fuel tank is mounted between lower section and the undercarriage of fuselage, battery pack is mounted between fuel tank and fuselage, flight control system is used to adjust the work shape of servomotor and motor.The long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of the heavy－duty are rational in infrastructure, can improve loading capacity, extend cruising time.
Description
Technical field
The utility model belongs to field of aerospace technology, specifically provides a kind of long endurance oil electric mixed dynamic of heavy－duty
More rotor unmanned aircrafts.
Background technology
Unmanned plane press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone, the people
With aspect, unmanned plane adds sector application, is that unmanned plane has really just needed；At present take photo by plane, agricultural, plant protection, self-timer, express delivery fortune
Defeated, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture
The application in the fields such as romance, has greatly expanded the purposes of unmanned plane in itself, developed country also actively extension sector application with
Develop unmanned air vehicle technique.
General unmanned vehicle only relies on electric power and provides power, and cruising time is short, loading capacity is small, can not meet current nothing
The man-machine demand in terms of agricultural plant protection, logistics transportation；Power is provided according to oily power, propeller is gone back while providing lift
Control direction is needed, reduces the efficiency of propeller.
Therefore, how to extend the cruising time of aircraft, improve the loading capacity of aircraft, become that people are urgently to be resolved hurrily to be asked
Topic.
Utility model content
In consideration of it, the purpose of this utility model is to provide a kind of long more rotors of endurance oil electric mixed dynamic of heavy－duty nobody
Aircraft, to solve the problems such as existing unmanned vehicle cruising time is short, loading capacity is small.
Technical solution provided by the utility model is：The long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of heavy－duty,
Including：Servomotor, motor, propeller A, propeller B, rocking arm A, rocking arm B, fuel tank, battery pack, undercarriage, flight control system
System and fuselage, wherein, servomotor is fixedly connected by rocking arm A with fuselage, and propeller A is on the servomotor, for for flight
Device provides lift, and motor is fixedly connected by rocking arm B with fuselage, and propeller B is mounted on motor, for adjusting aircraft
Posture, B number of propeller A and propeller is identical and is arranged alternately, and undercarriage is symmetrically mounted on the both sides of fuselage, fuel tank installation
It is servomotor fuel feeding between the lower section of fuselage and undercarriage, battery pack is mounted between fuel tank and fuselage, is supplied for motor
Electricity, flight control system are used to control the working condition of servomotor and motor.
It is preferred that the flight control system includes controller, the revolution speed of propeller sensor being connected with controller, speed of flying
Spend recorder, servomotor throttle control and motor controller.
Further preferably, the servomotor is connected with battery pack, for be battery-powered.
Further preferably, the propeller A and propeller B is 4.
The long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of heavy－duty provided by the utility model, by servomotor and
Propeller A provides lift for aircraft, and the posture of aircraft is adjusted by motor and propeller B, substantially increases propeller
Efficiency, by the way that oily power is combined with electric power, the cruising time of aircraft can be extended, improve the loading capacity of aircraft.
In addition, if an emergency situation is encountered in flight course for aircraft, such as servomotor parking, when can not work normally, electricity
Motivation can full speed operation, continue to aircraft short flight, ensure its safe falling.
Description of the drawings
Below in conjunction with the accompanying drawings and embodiment is described in further detail the utility model：
Fig. 1 is the top view of the long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of heavy－duty；
Fig. 2 is the front view of the long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of heavy－duty；
Fig. 3 is the structure diagram of flight control system.
Specific embodiment
The utility model is further explained below in conjunction with specific embodiment, but does not limit to this practicality
It is new.
As shown in Figure 1 and Figure 2, the utility model provide a kind of long more rotors of endurance oil electric mixed dynamic of heavy－duty nobody
Aircraft, including：Servomotor 1, motor 2, propeller A3, propeller B4, rocking arm A5, rocking arm B6, fuel tank 7, battery pack 8, rise
Fall frame 9, flight control system 10 and fuselage 11, wherein, servomotor 1 is fixedly connected by rocking arm A5 with fuselage 11, propeller A3
On servomotor 1, for providing lift for aircraft, motor 2 is fixedly connected by rocking arm B6 with fuselage 11, propeller
B4 is mounted on motor 2, and for adjusting the posture of aircraft, B4 number of propeller A3 and propeller is identical and is arranged alternately,
Undercarriage 9 is symmetrically mounted on the both sides of fuselage 11, and fuel tank 7 is mounted between the lower section of fuselage 11 and undercarriage 9, is servomotor 1
Fuel feeding, battery pack 8 are mounted between fuel tank 7 and fuselage 11, are powered for motor 2, and flight control system 10 is oily dynamic for controlling
The working condition of machine 1 and motor 2, wherein, fuselage preferably uses the composite material based on carbon fiber.
The long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of the heavy－duty are flight by servomotor and propeller A
Device provides lift, and the posture of aircraft is adjusted by motor and propeller B, substantially increases the efficiency of propeller, pass through by
Oily power is combined with electric power, can be extended the cruising time of aircraft, be improved the loading capacity of aircraft.
As the improvement of technical solution, as shown in figure 3, the flight control system 10 includes controller 110 and controller
Revolution speed of propeller sensor 111, flying speed recorder 112, servomotor throttle control 113 and the motor control of 110 connections
Device 114 processed, controller are mounted on the top of fuselage 11, can be returned according to revolution speed of propeller sensor and flying speed recorder
Data adjust the running parameter of servomotor throttle control and motor controller respectively, and then control servomotor and motor
Working condition.
As the improvement of technical solution, the servomotor 1 is connected with battery pack 8, for powering for battery pack 8, so as to for
Motor electric energy supplement.
As the improvement of technical solution, the propeller A3 and propeller B4 is 4.
Specific embodiment of the present utility model is write according to progressive mode, highlights each embodiment party
The difference of case, similar portion can be with cross-reference.
The embodiment of the utility model is elaborated above in conjunction with attached drawing, but the utility model is not limited to
The above embodiment within the knowledge of a person skilled in the art, can also not depart from the utility model
Various changes can be made on the premise of objective.
Claims (4)
1. the long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of heavy－duty, which is characterized in that including：It is servomotor (1), electronic
Machine (2), propeller A (3), propeller B (4), rocking arm A (5), rocking arm B (6), fuel tank (7), battery pack (8), undercarriage (9), fly
Row control system (10) and fuselage (11), wherein, servomotor (1) is fixedly connected by rocking arm A (5) with fuselage (11), propeller A
(3) it is mounted on servomotor (1), for providing lift for aircraft, motor (2) is fixed by rocking arm B (6) and fuselage (11)
Connection, propeller B (4) are mounted on motor (2), for adjusting the posture of aircraft, propeller A (3) and propeller B (4)
Number is identical and is arranged alternately, and undercarriage (9) is symmetrically mounted on the both sides of fuselage (11), and fuel tank (7) is mounted on fuselage (11)
It is servomotor (1) fuel feeding between lower section and undercarriage (9), battery pack (8) is mounted between fuel tank (7) and fuselage (11), for electricity
Motivation (2) is powered, and flight control system (10) is used to control the working condition of servomotor (1) and motor (2).
2. the long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of heavy－duty described in accordance with the claim 1, it is characterised in that：
The flight control system (10) include controller (110), be connected with controller (110) revolution speed of propeller sensor (111),
Flying speed recorder (112), servomotor throttle control (113) and motor controller (114).
3. the long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of heavy－duty described in accordance with the claim 1, it is characterised in that：
The servomotor (1) is connected with battery pack (8), for powering for battery pack (8).
4. according to the long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of heavy－duty any one of claims 1 to 3,
It is characterized in that：The propeller A (3) and propeller B (4) are 4.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721430428.5U CN207374646U (en) | 2017-10-30 | 2017-10-30 | The long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of heavy－duty |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721430428.5U CN207374646U (en) | 2017-10-30 | 2017-10-30 | The long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of heavy－duty |
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| CN207374646U true CN207374646U (en) | 2018-05-18 |
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| CN201721430428.5U Active CN207374646U (en) | 2017-10-30 | 2017-10-30 | The long more rotor unmanned aircrafts of endurance oil electric mixed dynamic of heavy－duty |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109601212A (en) * | 2019-01-09 | 2019-04-12 | 四川万智沃达科技有限公司 | A kind of weather influence operational method, unmanned plane and computer readable storage medium based on unmanned plane |
| CN109733622A (en) * | 2019-01-28 | 2019-05-10 | 河南正大航空工业股份有限公司 | A kind of mixed dynamic unmanned plane of oil electricity |
| CN111086642A (en) * | 2020-01-06 | 2020-05-01 | 尚良仲毅(沈阳)高新科技有限公司 | Multi-rotor unmanned aerial vehicle and control method |
| CN112455667A (en) * | 2020-12-08 | 2021-03-09 | 国网河北省电力有限公司雄安新区供电公司 | Unmanned aerial vehicle capable of improving cruising ability |
| CN113212755A (en) * | 2020-01-21 | 2021-08-06 | 辽宁壮龙无人机科技有限公司 | Control method for hybrid-electric multi-rotor unmanned aerial vehicle |
| CN114852338A (en) * | 2022-06-29 | 2022-08-05 | 中国兵器装备集团自动化研究所有限公司 | Hybrid power carrying unmanned aerial vehicle and carrying system |
-
2017
- 2017-10-30 CN CN201721430428.5U patent/CN207374646U/en active Active
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109601212A (en) * | 2019-01-09 | 2019-04-12 | 四川万智沃达科技有限公司 | A kind of weather influence operational method, unmanned plane and computer readable storage medium based on unmanned plane |
| CN109733622A (en) * | 2019-01-28 | 2019-05-10 | 河南正大航空工业股份有限公司 | A kind of mixed dynamic unmanned plane of oil electricity |
| CN109733622B (en) * | 2019-01-28 | 2023-09-08 | 河南正大航空工业股份有限公司 | Oil-electricity hybrid unmanned aerial vehicle |
| CN111086642A (en) * | 2020-01-06 | 2020-05-01 | 尚良仲毅(沈阳)高新科技有限公司 | Multi-rotor unmanned aerial vehicle and control method |
| CN113212755A (en) * | 2020-01-21 | 2021-08-06 | 辽宁壮龙无人机科技有限公司 | Control method for hybrid-electric multi-rotor unmanned aerial vehicle |
| CN112455667A (en) * | 2020-12-08 | 2021-03-09 | 国网河北省电力有限公司雄安新区供电公司 | Unmanned aerial vehicle capable of improving cruising ability |
| CN114852338A (en) * | 2022-06-29 | 2022-08-05 | 中国兵器装备集团自动化研究所有限公司 | Hybrid power carrying unmanned aerial vehicle and carrying system |
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