CN205633025U - Power wing helicopter - Google Patents

Power wing helicopter Download PDF

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Publication number
CN205633025U
CN205633025U CN201620458518.4U CN201620458518U CN205633025U CN 205633025 U CN205633025 U CN 205633025U CN 201620458518 U CN201620458518 U CN 201620458518U CN 205633025 U CN205633025 U CN 205633025U
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CN
China
Prior art keywords
helicopter
motor
rotor
power wing
frame
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Application number
CN201620458518.4U
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Chinese (zh)
Inventor
陈小生
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陈小生
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Priority to CN201620458518.4U priority Critical patent/CN205633025U/en
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Publication of CN205633025U publication Critical patent/CN205633025U/en
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Abstract

The utility model relates to a power wing helicopter belongs to the helicopter field, the utility model provides a pair of power wing helicopter, be provided with the motor of taking the screw respectively in first leading edge position to four rotors, such design can provide power by a plurality of motor, through the rotatory thrust that produces of screw, drive the rotatory lift that produces of rotor, realize helicopter's flight, when wherein partial motor breaks down, other motor still can continuation work produce thrust, the drive rotor is rotatory, reduce helicopter's flame -out in flight probability, the security of flight and descending when improving the helicopter trouble.

Description

A kind of power wing helicopter
Technical field
This utility model belongs to helicopter field, is specifically related to a kind of power wing helicopter.
Background technology
Helicopter is by driven by engine rotor rotational at present, it is achieved flight function, but because of engine failure Helicopter flame-out in flight, especially monomotor helicopter is caused this fault to occur, for pilot This is breakneck situation with for passenger, needs to rely on propeller spin safe falling.Fault without When method controls, need abandoning machine and parachute jumping, even if parachuting successfully, but helicopter damage, cause non- The biggest property loss.
Utility model content
In view of this, the purpose of this utility model is to overcome the deficiencies in the prior art, it is provided that a kind of safety Power wing helicopter reliably.
For realizing object above, this utility model adopts the following technical scheme that
A kind of power wing helicopter, including helicopter body and be arranged on described helicopter body Bottom undercarriage, also include connecting rod, bearing, first to fourth rotor, first to fourth motor base (frame), First to fourth motor, first to fourth propeller, steering wheel and battery;
Wherein, first to fourth propeller described is separately positioned on first to fourth motor described, and described the One to four motor is separately positioned in first to fourth motor base (frame) described, first to fourth motor base (frame) described It is separately positioned on the leading edge of first to fourth rotor described, makes first to fourth propeller described be respectively placed in described First to fourth rotor front, first to fourth rotor described is mutually an angle of 90 degrees and is arranged on described bearing, described Bearing is arranged on described connecting rod one end, and the described connecting rod other end is with described helicopter bodies top even Connecing, described steering wheel is arranged on described helicopter body tail section, described battery be arranged at described in go straight up to fly In machine body;
Described power wing helicopter also includes that control system, described set-up of control system fly described going straight up to In machine body, described motor, described steering wheel are respectively connecting to described control system, described control system System is connected to described battery.
Further, first to fourth motor base (frame) described is separately positioned on the centre of first to fourth rotor described Position between wing tip.
Further, first to fourth motor base (frame) described is separately positioned on first to fourth rotor interposition described Put.
Further, described power wing helicopter also includes first to fourth protective cover, described first to fourth Propeller is respectively arranged in first to fourth guard shield described, and first to fourth protective cover described is separately positioned on institute State on first to fourth motor base (frame).
Further, described power wing helicopter also includes that remote controller, described control system are additionally provided with Wireless communication module, described remote controller and described wireless communication module wireless connections.
This utility model uses above technical scheme, at least possesses following beneficial effect:
A kind of power wing helicopter that this utility model provides, the leading edge at rotor is provided with band propeller Motor, by propeller rotate produce thrust, drive rotor wing rotation produce lift, it is achieved go straight up to fly The flight of machine, the so helicopter of design are provided power by multiple motor, when wherein section motor When breaking down, other motor may continue to work and produce thrust, drive rotor wing rotation, and reduction is gone straight up to The flame-out in flight probability of aircraft, thus improve the safety of helicopter.
Accompanying drawing explanation
Fig. 1 is this utility model one power wing helicopter schematic diagram;
Fig. 2 is this utility model rotor partial schematic diagram;
Fig. 3 is that this utility model controls partial schematic diagram.
In figure: 1, helicopter body;2, undercarriage;3, propeller;4, motor;5, electronic Support;6, rotor;7, bearing;8, connecting rod;9, steering wheel;10, battery;11, system is controlled System;12, protective cover;13, remote controller;14, wireless communication module.
Detailed description of the invention
Below by drawings and Examples, the technical solution of the utility model is described in further detail.
As depicted in figs. 1 and 2, this utility model provides a kind of power wing helicopter, including going straight up to fly Machine body 1 and be arranged on the undercarriage 2 of described helicopter body bottom portion, also includes propeller 3, electricity Motivation 4, motor base (frame) 5, rotor 6, bearing 7, connecting rod 8, steering wheel 9 and battery 10, institute State propeller 3, described motor 4, described motor base (frame) 5 and described rotor 6 and have four respectively.
Wherein, described propeller 3 is arranged on described motor 4, and described motor 4 is arranged on described In motor base (frame) 5, described motor base (frame) 5 is arranged on the leading edge of described rotor 6, makes described propeller 3 Being placed in described rotor 6 front, between described rotor 6, angularly distribution is arranged on described bearing 7, institute Stating bearing 7 and be arranged on described connecting rod 8 one end, the described connection 8 bar other end is with described helicopter originally Body 1 top connects, and described steering wheel 9 is arranged on described helicopter body 1 afterbody, described battery 10 It is arranged in described helicopter body 1;
Described power wing helicopter also include control system 11, described control system 11 be arranged on described directly Rising in aircraft body 1, described motor 4, described steering wheel 9 are respectively connecting to described control system 11, Described control system 11 is connected to described battery 10.
It is understood that the power wing helicopter of this utility model offer is in the leading edge of described rotor 6 It is provided with the described motor 4 with described propeller 3, and is provided electric energy by described battery 10, by institute State propeller 3 and rotate generation thrust, drive described rotor 6 to rotate and produce lift, it is achieved helicopter Flight.This design having multiple-motor to provide power, when wherein section motor breaks down, its His motor may continue to work and produces thrust, drives described rotor 6 to rotate, and reduces the sky of helicopter Middle parking probability, thus flight and the safety of landing when improving helicopter fault.
Further, the position of the described motor base (frame) 5 of fixing described motor 4 is arranged on described rotor 6 Middle position between wing tip, it is preferable that described motor base (frame) 5 is arranged on described rotor 6 interposition Put.
Further, in order to security protection considers, protective cover 12 can be set outside described propeller 3, Described protective cover 12 is arranged on described motor base (frame) 5.
Further, described power wing helicopter also includes that remote controller 13, described control system 11 also set It is equipped with wireless communication module 14, described remote controller 13 and described wireless communication module 14 wireless connections, this Sample can realize the remote manipulation to described power wing helicopter.
This utility model is not limited to above-mentioned preferred forms, and anyone is under enlightenment of the present utility model All can draw other various forms of products, no matter but in its shape or structure, make any change, every There is same as the present application or akin technical scheme, within all falling within protection domain of the present utility model.

Claims (5)

1. a power wing helicopter, including helicopter body and be arranged on described helicopter this Undercarriage bottom body, it is characterised in that: also include connecting rod, bearing, first to fourth rotor, first To four motor base (frame)s, first to fourth motor, first to fourth propeller, steering wheel and battery;
Wherein, first to fourth propeller described is separately positioned on first to fourth motor described, and described the One to four motor is separately positioned in first to fourth motor base (frame) described, first to fourth motor base (frame) described It is separately positioned on the leading edge of first to fourth rotor described, makes first to fourth propeller described be respectively placed in described First to fourth rotor front, first to fourth rotor described is mutually an angle of 90 degrees and is arranged on described bearing, described Bearing is arranged on described connecting rod one end, and the described connecting rod other end is with described helicopter bodies top even Connecing, described steering wheel is arranged on described helicopter body tail section, described battery be arranged at described in go straight up to fly In machine body;
Described power wing helicopter also includes that control system, described set-up of control system fly described going straight up to In machine body, described motor, described steering wheel are respectively connecting to described control system, described control system System is connected to described battery.
Power wing helicopter the most according to claim 1, it is characterised in that: described first to fourth Motor base (frame) is separately positioned on the centre of first to fourth rotor described to position between wing tip.
Power wing helicopter the most according to claim 2, it is characterised in that: described first to fourth Motor base (frame) is separately positioned on first to fourth rotor centre position described.
Power wing helicopter the most according to claim 1, it is characterised in that: described power wing is straight Rise aircraft also include first to fourth protective cover, first to fourth propeller described be respectively arranged at described first to In four guard shields, first to fourth protective cover described is separately positioned on first to fourth motor base (frame) described.
5. according to the power wing helicopter described in any one of Claims 1-4, it is characterised in that: institute State power wing helicopter and also include that remote controller, described control system are additionally provided with wireless communication module, institute State remote controller and described wireless communication module wireless connections.
CN201620458518.4U 2016-05-19 2016-05-19 Power wing helicopter Active CN205633025U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620458518.4U CN205633025U (en) 2016-05-19 2016-05-19 Power wing helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620458518.4U CN205633025U (en) 2016-05-19 2016-05-19 Power wing helicopter

Publications (1)

Publication Number Publication Date
CN205633025U true CN205633025U (en) 2016-10-12

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620458518.4U Active CN205633025U (en) 2016-05-19 2016-05-19 Power wing helicopter

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CN (1) CN205633025U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106379519A (en) * 2016-10-26 2017-02-08 李鹏 Pneumatic layout scheme applying advancing blade concept for tandem-rotor helicopter

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106379519A (en) * 2016-10-26 2017-02-08 李鹏 Pneumatic layout scheme applying advancing blade concept for tandem-rotor helicopter

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