CN206437213U - Unmanned airborne vehicle with combined type lift member - Google Patents
Unmanned airborne vehicle with combined type lift member Download PDFInfo
- Publication number
- CN206437213U CN206437213U CN201621496274.5U CN201621496274U CN206437213U CN 206437213 U CN206437213 U CN 206437213U CN 201621496274 U CN201621496274 U CN 201621496274U CN 206437213 U CN206437213 U CN 206437213U
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- lift
- wing
- fixed
- unmanned plane
- lift member
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- 230000007246 mechanism Effects 0.000 claims abstract description 12
- 150000001875 compounds Chemical class 0.000 claims description 14
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 2
- 239000004744 fabric Substances 0.000 claims 1
- 241000985905 Candidatus Phytoplasma solani Species 0.000 abstract description 3
- 210000002105 tongue Anatomy 0.000 abstract 1
- 230000005611 electricity Effects 0.000 description 3
- 238000007664 blowing Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 1
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Abstract
The mankind have invented the fixed-wing unmanned plane of VTOL, the unmanned plane combined by four rotors with fixed-wing unmanned plane, realize the VTOL and hovering of fixed-wing unmanned plane, and it can be flown with extremely low speed, but it has a significant shortcoming i.e. mounted mass too low, present pole needs a kind of fixed-wing unmanned plane, not only can random speed, taking off and can also have big take-off weight in flight course, for this, we are by fixed-wing, four rotors, the efficiency that Chui Yi lift-risings mechanism is combined together improvement aircraft makes its speed freely, can VTOL, also can STOL, and it is remarkably improved take-off weight, extend endurance, in all tongues economic field, this unmanned plane is all desirable.It is particularly important in agricultural, military and express transportation field.
Description
Technical field：
Unmanned airborne vehicle with combined type lift member belongs to unmanned field of aircraft, more particularly to a kind of to have admittedly
Fixed pattern wing, four rotors, install in wing Chui Yi lift-risings mechanisms compound lift member unmanned airborne vehicle.
Background technology：
The mankind have invented the fixed-wing unmanned plane of VTOL, i.e., the nothing combined by four rotors with fixed-wing unmanned plane
It is man-machine, the VTOL and hovering of fixed-wing unmanned plane are realized, and can be flown with extremely low speed, but it has one significantly
Shortcoming be that mounted mass is too low, it is now desired to a kind of fixed-wing unmanned plane, not only can random speed, take off with flight course
Also there can be big take-off weight, be that we are combined together improvement aircraft this by fixed-wing, four rotors, Chui Yi lift-risings mechanism
Efficiency makes its speed freely, can VTOL, also can STOL, and be remarkably improved take-off weight, extend endurance, all
This unmanned plane in national economy field is all desirable.It is particularly important in agricultural, military, express transportation field.
The content of the invention：
Goal of the invention：Lift ducted fan, Chui Yi lift-risings mechanism are installed on inside fixed-wing wing, made this with multiple
The unmanned airborne vehicle of box-like lift member has big load, can VTOL function and STOL function, can be widely used for nobody
Machine and small-sized aerial craft, making is simple, cost is low, function admirable.
The present invention is so completed：Unmanned airborne vehicle with combined type lift member, by fixed-wing, lift duct wind
Fan, blow wing high lift component, fuselage, undercarriage, electric traction propeller, receiver, power storehouse, appliance case, rudder it is mechanical, electrical adjust device,
The unmanned airborne vehicle with combined type lift member of implement quick-attaching couple composition, it is characterised in that：Fuselage interior has power storehouse, set
Standby storehouse, front fuselage has an electric traction propeller, and undercarriage, implement quick-attaching couple arranged at bottom, undercarriage can for wheeled, ski type and
Float-type, the symmetrical four fixed wings in the side of fuselage two, wing end respectively has one group of lift ducted fan and blows wing lift-rising
The compound lift member of mechanism, the coaxial forward-reverse spiral oar of its lift member is driven by two motors, turn of its lower propeller
Sub- internal layer is rotor, is the blade of radial direction air intake blower fan outside rotor, and impeller is arranged within the housing of radial direction air intake blower fan,
The leading edge of radial direction air intake blower fan is provided with strip air inlet, and trailing edge is connected with stepped compound vane cluster, and this compound vane cluster can be with
Steering wheel is moved and swung up and down, and radial direction air intake blower fan air outlet blow-through corresponding with compound vane cluster is combined the upper surface of vane cluster.
Power storehouse, equipment compartment, receiver, rudder are mechanical, electrical to be adjusted device, electric traction propeller, lift ducted fan, blows wing lift-rising
Part is electrically connected.
Equipment compartment described in it includes navigation component, flight-control component and communication component.
Such a airborne vehicle can be pure electronic, or the electric combination drive lift ducted fan of oil is with blowing wing lift-rising multi mechanism compound
Lift member, can individually arrange lift ducted fan and Chui Yi lift-risings mechanism.
Brief description of the drawings：
Fig. 1 is the top view of the unmanned airborne vehicle with combined type lift member
Fig. 2 is the front view of the unmanned airborne vehicle with combined type lift member
Fig. 3 is the side view of the unmanned airborne vehicle with combined type lift member
Fig. 4 is the structure chart top view of combined type lift member
Fig. 5 is the structure chart B-B sectional views of combined type lift member
Fig. 6 is the structural representation of propeller rotor under combined type lift member
Fig. 7 is combined type lift member structure chart Fig. 4 C-C sectional views
In figure：1 fuselage, 2 electric traction propellers, 3 fixed wings, 4 lift ducted fans and Chui Yi lift-risings mechanism are multiple
The lift member of conjunction, 5 undercarriages, 6 rotors, rotor, 8 air inlets, 9 radial direction air intake blower fan housings, 10 outlets of 7 times propellers
Mouth, 11 steering wheels, 12 stepped compound vane clusters, 13 implement quick-attaching couples, 14 power storehouses, 15 equipment compartments, 16 receivers, 17 electricity are adjusted
Device, 18 radial direction air intake blower fan impeller blades, 19 bracing rings, 20 times proprotors, 21 motors, 22 times proprotor rotors
Embodiment：
Embodiment 1：
3 fixed wings are installed on 1 fuselage, 4 lift ducted fans are installed in 3 fixed wing ends and wing lift-rising is blown
The lift member of multi mechanism compound, installs 5 undercarriages, installs 13 implement quick-attaching couples, and 16 receivers, 17 electricity are installed in 1 fuselage body
Device is adjusted, 14 power storehouses, 15 equipment compartments are installed, 14 power storehouses, 15 equipment compartments, 16 receivers, 11 steering wheels, 17 electricity adjust devices, 2 electronic to lead
Draw propeller, 4 lift ducted fans to electrically connect with blowing the lift member of wing lift-rising multi mechanism compound, the action of 2 electric traction propellers
Traction fly forward, by 3 fixed wings, 4 lift ducted fans and blow wing lift-rising multi mechanism compound lift member provide lift and
Part thrust, four rotors provide aircraft balance.
Claims (1)
1. with combined type lift member unmanned airborne vehicle, by fixed-wing, lift ducted fan, blow wing high lift component, fuselage,
What the mechanical, electrical tune device of undercarriage, electric traction propeller, receiver, power storehouse, appliance case, rudder, implement quick-attaching couple were constituted has multiple
The unmanned airborne vehicle of box-like lift member, it is characterised in that：Fuselage interior has power storehouse, equipment compartment, and front fuselage has electronic lead
Draw propeller, undercarriage, implement quick-attaching couple are arranged at bottom, and undercarriage can be wheeled, slide-type and float-type, and the side of fuselage two is symmetrically divided
Four fixed wings of cloth, wing end respectively has one group of lift ducted fan and blows the compound lift portion of wing lift-rising mechanism
Part, the coaxial forward-reverse spiral oar of its lift member is driven by two motors, and the rotor inner layer of its lower propeller is rotor, in rotor
Outside is the blade of radial direction air intake blower fan, and impeller is arranged within the housing of radial direction air intake blower fan, the leading edge of radial direction air intake blower fan
Strip air inlet is provided with, trailing edge is connected with stepped compound vane cluster, this compound vane cluster can be moved and swung up and down with steering wheel,
Radial direction air intake blower fan air outlet blow-through corresponding with compound vane cluster is combined the upper surface of vane cluster, power storehouse, equipment compartment, reception
Machine, rudder be mechanical, electrical to be adjusted device, electric traction propeller, lift ducted fan, blows wing high lift component and electrically connect, the equipment compartment described in it
Including navigation component, flight-control component communication component.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621496274.5U CN206437213U (en) | 2016-12-30 | 2016-12-30 | Unmanned airborne vehicle with combined type lift member |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621496274.5U CN206437213U (en) | 2016-12-30 | 2016-12-30 | Unmanned airborne vehicle with combined type lift member |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206437213U true CN206437213U (en) | 2017-08-25 |
Family
ID=59642347
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621496274.5U Withdrawn - After Issue CN206437213U (en) | 2016-12-30 | 2016-12-30 | Unmanned airborne vehicle with combined type lift member |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206437213U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108263607A (en) * | 2016-12-30 | 2018-07-10 | 珠海天空速递有限公司 | Unmanned aircraft with combined type lift member |
-
2016
- 2016-12-30 CN CN201621496274.5U patent/CN206437213U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108263607A (en) * | 2016-12-30 | 2018-07-10 | 珠海天空速递有限公司 | Unmanned aircraft with combined type lift member |
| CN108263607B (en) * | 2016-12-30 | 2024-04-12 | 珠海天空速递有限公司 | Unmanned aerial vehicle with composite lift elements |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20170825 Effective date of abandoning: 20240412 |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20170825 Effective date of abandoning: 20240412 |