CN106114848A - A kind of mooring cruise multi-mode VUAV - Google Patents
A kind of mooring cruise multi-mode VUAV Download PDFInfo
- Publication number
- CN106114848A CN106114848A CN201610741852.5A CN201610741852A CN106114848A CN 106114848 A CN106114848 A CN 106114848A CN 201610741852 A CN201610741852 A CN 201610741852A CN 106114848 A CN106114848 A CN 106114848A
- Authority
- CN
- China
- Prior art keywords
- wing
- fuselage
- vuav
- cruise
- mooring
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/022—Tethered aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of mooring cruise multi-mode VUAV, multiple aerial mission pattern can be at the unmanned plane of small space VTOL can be performed.Including fixed-wing fuselage, wing, empennage, horizontal propeller dynamical system, vertical spin oar electric system, support, rotor fuselage, cable and payload parts.The design feature of the present invention is: for different mission requirementses, can select to be adapted to perform the pattern of this mission requirements at short notice by dismounting the structure of parts change of flight device.When using as mooring unmanned plane pattern, there is the feature such as mobility strong, hovering time length；As cruise VUAV pattern use time, there is efficient cruising flight, can hover in target area and can in small space the feature of VTOL.When not using, can place to save parking space after being dismantled by critical piece.
Description
Technical field
The invention belongs to unmanned air vehicle technique field, be specifically related to a kind of mooring cruise VTOL and various modes can be performed
The unmanned plane of task.Military field can be applicable to army land vehicle or naval vessels, commercial field can be applicable to lasting high-altitude
Shooting or lift-launch emergency communication trunking.
Background technology
Unmanned plane is a kind of Novel air aircraft occurred as the target drone of training use in the twenties in 20th century, because of
Having the features such as with low cost, zero casualties, in nearly several local wars, different types of unmanned plane has all played very
Important effect, becomes a function increasingly comprehensively combat forces, is increasingly paid attention to by the military of various countries.For strengthening aircraft carrier
Comprehensive fight capability, promote aircraft carrier have man-machine with unmanned plane with the use of, USN plan research and development one warship before 2018
Carry unmanned plane, with thinking that nuclear aircraft carrier provides lasting carrier-borne Intelligence, Surveillance and Reconnaissance and part to attack and supports.
Mooring unmanned plane is mainly used in long-time continual aerial monitoring and emergency communication, can carry special visible
Light video camera and infrared thermography, it is also possible to carry special emergency communication trunking.Cruise VUAV conduct
The unmanned plane that one class is special, can take off with zero velocity and land, can VTOL in small space.With conventional unmanned plane phase
Ratio, cruise VUAV has the advantages such as landing mode is flexible, be transmitted back to debit just, mobility is good, also possesses simultaneously
The general utility functions of conventional unmanned plane.Research and develop novel mooring cruise multi-mode VUAV, for winning future battlefield
Initiative has higher practical value.
Chinese invention patent 201610017284.4 is open describes a kind of composite wing VUAV.The program is hung down
Straight power unit is connected to wing bottom by mounting rod, and this unmanned plane can only meet VTOL and cruising flight requirement, nothing
Method meets that mooring UAV Maneuver is strong, the requirement of hovering time length, also cannot be adapted for carrying out multimodal aerial mission.
Summary of the invention
For composite wing VUAV function singleness in above-mentioned prior art, work that small space cannot be applicable to
Make environment and unmanned plane is performed the requirement of multiple-task.The invention discloses a kind of mooring cruise multi-mode VTOL without
Man-machine, mooring unmanned plane pattern or cruise VUAV mould can be assembled into for the different fast quick-detach of mission mode
Formula.
The present invention can not only realize unmanned plane VTOL in the small space of middle-size and small-size carrier, not by cruising flight also
In the requirement of target spatial domain hovering, spatial domain above target of making can also hover for a long time when mooring unmanned plane pattern uses, carry
For continual aerial monitoring and emergency communication.
The invention provides a kind of mooring cruise multi-mode VUAV, including: fixed-wing fuselage；It is fixed on
The wing of fixed wing machine body both sides；It is distributed in the empennage of fixed-wing afterbody；It is positioned at the rotor fuselage of fixed-wing aircraft body；By
The outward extending support of rotor fuselage surrounding；It is positioned at the horizontal propeller dynamical system of fixed-wing fore-body；It is positioned at bracket end
The vertical spin oar electric system in portion；Connect carrier and the cable of rotor underbelly；It is positioned at fixed-wing underbelly or rotor
The payload parts of underbelly.
All there is mounting groove described fixed-wing aircraft body, bottom and both sides, need use time can quickly by rotor fuselage, have
Effect loaded components, wing plug-in mounting are fixed on fixed-wing aircraft；Fixed-wing fuselage interior is airborne places fuel reserve tank and horizontal helical
Rotation paddle motor.
Described wing level is fixed on fixed-wing fuselage both sides and is symmetric about fixed-wing fuselage mid-plane, unmanned
During machine cruising flight, himself gravity of liter dynamic balance that wing produces.Aileron outside wing wing edge after a while is the main behaviour of aircraft
Making rudder face, rolling moment produced by the differential deflection of left and right aileron makes aircraft rolling on fixed-wing fuselage datum.
Described empennage is divided into tailplane and vertical tail, and tailplane is horizontally arranged at fixed-wing afterbody, level
The pitching moment that the elevator of empennage trailing edge produces controls aircraft pitch flight；Vertical tail is vertically mounted on fixed-wing fuselage tail
Portion, the rudder of vertical tail trailing edge produces yawing, it is achieved directional control.
Described horizontal propeller dynamical system includes propeller, electromotor and fuel reserve tank.Propeller rotates to be unmanned plane
Cruising condition provides flying power.
Described vertical spin oar electric system rotates himself gravity of liter dynamic balance produced, and runs into the interference factors such as high wind
Time, keep its smooth flight attitude by electric rotating machine.Described bracket end installs single screw or coaxial installation twin screw.
Described payload parts can carry visible light camera and infrared thermography, it is also possible to carries special emergent logical
News trunking.
Described wing, support, the equal quick release of rotor fuselage and installation, can save space and deposit, need to make after dismounting
Used time can Fast Installation at short notice.
Described rotor fuselage is made up of airborne power supply and control system, and airborne power supply provides electric power for vertical spin oar motor
Support；Control system controls the rotation of the deflection of rudder face, the rotating speed of propeller and vertical spin oar motor and controls unmanned plane
Flight path also keeps its steady attitude.
Described rotor fuselage, support are respectively provided with the profile that can produce aerodynamic lift, provide part lift when cruising flight
And reduce windage, wing dimension can be reduced, increase voyage.
Described cable inserts rotor underbelly connection jaws, from the electric power of carrier transmission as the master of horizontal propeller motor
The energy is wanted to input.
The invention have the advantages that
1., when needing to scout distant object, can quickly be assembled into cruise VUAV pattern, can be at narrow and small sky
In take off vertically to certain altitude, horizontal propeller dynamical system starts and makes unmanned plane cruising flight subsequently, and wing produces
Rise dynamic balance self gravitation and improve flight efficiency；To overhead, target spatial domain, close horizontal propeller dynamical system and start vertical
Propeller electric system, can realize scouting purpose and data being passed back carrier in real time in the hovering of target overhead.
2. when needing continual aerial monitoring and emergency communication, can quickly be assembled into mooring unmanned plane pattern, can carry
Body overhead continuous firing, has the advantage such as mobility strong and hovering time length.
3., when need not unmanned plane work, the parts such as wing, support, rotor fuselage can be pulled down, deposit in the narrow of carrier
In little space, save memory space.
Accompanying drawing explanation
Fig. 1 is the structural representation of present invention embodiment when making mooring unmanned plane pattern.
Fig. 2 be the present invention make to cruise VUAV pattern time the structural representation of an embodiment.
Detailed description of the invention
The invention provides a kind of mooring cruise multi-mode VUAV, can conduct for different aerial missions
Mooring unmanned plane pattern or cruise VUAV pattern use.Technical scheme, it is possible to resolve existing composite wing
VUAV function singleness, the working environment of small space cannot be applicable to and unmanned plane is performed multiple-task
Requirement.
Following two embodiment describes the present invention respectively and makees mooring unmanned plane pattern and cruise VUAV mould
Embodiment during formula, but the present invention is not limited only to following example:
Embodiment 1:
Mooring unmanned plane pattern as shown in Figure 1 is by vertical spin oar electric system 5, support 6, rotor fuselage 7, cable 8
Form with payload parts 9.
Described vertical spin oar electric system 5 is installed on support 6 end, uses coaxial twin screw arrangement form, spiral
Oar rotates himself gravity of liter dynamic balance produced.When running into the interference factors such as high wind, it is kept steadily to fly by electric rotating machine
Row attitude.
Described rotor fuselage 7 outer surface is processed into by titanium alloy material, and internal placement is for horizontal propeller motor
Airborne power supply and stablize the control system of UAV Attitude.
Described support 6 is arranged on rotor fuselage 7 surrounding, is inserted in locating slot and is bolted connection during use,
Its material is titanium alloy or carbon fibre composite.
Described payload parts 9 are inserted into rotor fuselage 7 bottom, are bolted connection.Visible ray can be carried take the photograph
Camera and infrared thermography, it is also possible to carry special emergency communication trunking.
Described cable 8 inserts rotor fuselage 7 bottom connection jaws, from the electric power of carrier transmission as horizontal propeller motor
Main energy sources inputs.
When the present invention makees the use of mooring unmanned plane pattern, the driven by power vertical spin oar relying on carrier to provide when taking off turns
Dynamic so that it is the lift of generation remains a constant speed after exceeding himself gravity rotation, and unmanned plane steadily rises to target area；Unmanned plane
When entering hovering duty, the lift that now vertical spin oar produces is equal to himself gravity, and payload parts 9 enter work
Operation mode, when running into the interference factors such as high wind, airborne power supply drives motor to rotate its smooth flight attitude of holding.
The mounting means of the present embodiment has two kinds: when installing and using for the first time, by support 6 and vertical spin oar electric system 5,
Payload parts 9, cable 8 are arranged on rotor fuselage 7；It is mooring unmanned plane from cruise VUAV patten transformation
During pattern, fixed-wing fuselage 1 is pulled down from the attachment means of rotor fuselage 7 bottom, then payload parts 9, cable 8 are pacified
It is contained in rotor fuselage 7 bottom, the conversion of offline mode can be completed.
Embodiment 2:
Cruise VUAV pattern as shown in Figure 2 is by fixed-wing fuselage 1, wing 2, empennage 3, horizontal propeller
Dynamical system 4, vertical spin oar electric system 5, support 6, rotor fuselage 7 and payload parts 9 form.
Described fixed-wing fuselage 1 is made up of titanium alloy material, and all there is mounting groove its top, bottom and both sides, needs to use
Time can quickly rotor fuselage 7, payload parts 9, wing 2 plug-in mounting be fixed on fixed-wing fuselage 1；In fixed-wing fuselage 1
Portion is airborne places fuel reserve tank and flat spin paddle motor.
Described wing 2 is made up of titanium alloy material or carbon fibre composite, and level is fixed on fixed-wing fuselage 1 both sides and closes
It is symmetric in fixed-wing fuselage 1 mid-plane, during unmanned plane cruising flight, himself weight of the liter dynamic balance that wing 2 produces
Power.The main operation rudder face that aileron is aircraft outside wing 2 wing edge after a while, rolling moment produced by the differential deflection of left and right aileron
Make aircraft rolling on fixed-wing fuselage 1 longitudinal axis.
Described empennage 3 is made up of carbon fibre composite, is divided into tailplane 3 and vertical tail 3, tailplane 3 level
Being arranged on fixed-wing fuselage 1 afterbody, the pitching moment that the elevator of tailplane 3 trailing edge produces controls aircraft pitch flight；Hang down
Fin 3 is vertically mounted on fixed-wing fuselage 1 afterbody, and the rudder of vertical tail 3 trailing edge produces yawing, it is achieved direction is grasped
Vertical.
Described horizontal propeller dynamical system 4 includes propeller, electromotor and fuel reserve tank.Propeller rotates to be unmanned plane
Cruising condition provides flying power.
Described vertical spin oar electric system 5 is installed on support 6 end, uses coaxial twin screw arrangement form, spiral
Oar rotates himself gravity of liter dynamic balance produced.When running into the interference factors such as high wind, it is kept steadily to fly by electric rotating machine
Row attitude.
Described rotor fuselage 7 outer surface is processed into by titanium alloy material, and internal placement is for horizontal propeller motor
Airborne power supply and stablize the control system of UAV Attitude, bottom plug-in mounting fixing with on fixed-wing fuselage 1.
Described support 6 is arranged on rotor fuselage 7 surrounding, is inserted in locating slot and is bolted connection during use,
Its material is titanium alloy or carbon fibre composite.
Described payload parts 9 are inserted into fixed-wing fuselage 1 bottom, are bolted connection.Visible ray can be carried
Video camera and infrared thermography, it is also possible to carry special emergency communication trunking.
When the present invention makees cruise VUAV pattern use, airborne power supply drives vertical spin oar to rotate so that it is
The lift produced remains a constant speed rotations after exceeding himself gravity, and unmanned plane enters, after steadily rising to object height, the shape that hovers
State；Now horizontal propeller dynamical system 4 works, and vertical spin oar rotating speed is gradually reduced, unmanned plane accelerating flight on level until
It reaches average flight state；Unmanned plane arrives specifies above target behind spatial domain, and vertical spin oar rotating speed increase makes it produce
Lift is equal to unmanned plane self gravitation, and horizontal propeller dynamical system 4 is closed, and unmanned plane enters hovering pattern and payload portion
Part 9 enters mode of operation；Flying method when unmanned plane makes a return voyage is similar with above-mentioned principle, does not repeats at this.
The mounting means of the present embodiment has two kinds: when installing and using the most for the first time, by wing 2, payload parts 9, rotor
Fuselage 7 fast inserted respectively and fastens in the mounting groove of fixed-wing fuselage 1, support 6 and vertical spin oar electric system 5 is pacified
It is contained on rotor fuselage 7；From mooring unmanned plane patten transformation for cruise VUAV pattern time, by payload parts
9 and cable 8 after rotor fuselage 7 bottom is dismantled, then wing 2, payload parts 9, rotor fuselage 7 respectively fast inserted is existed
The mounting groove of fixed-wing fuselage 1 is interior and fastens, and can complete the conversion of offline mode.
The above, be only presently preferred embodiments of the present invention, and the present invention not makees any pro forma restriction, though
So the present invention is disclosed above with preferred embodiment, but is not limited to the present invention, any technology people being familiar with this specialty
Member, in the range of without departing from technical solution of the present invention, when the method for available the disclosure above and technology contents make a little more
Move or be modified to the Equivalent embodiments of equivalent variations, as long as being the content without departing from technical solution of the present invention, according to the present invention's
Any simple modification, equivalent variations and the modification that above example is made by technical spirit, still falls within technical solution of the present invention
In the range of.
Claims (10)
1. mooring cruise multi-mode VUAV, it is characterised in that: include fixed-wing fuselage (1), wing (2),
Empennage (3), horizontal propeller dynamical system (4), vertical spin oar electric system (5), support (6), rotor fuselage (7), cable
And payload parts (9) (8)；By vertical spin oar electric system (5), support (6), rotor fuselage (7), cable (8) with have
Effect loaded components (9) constitutes mooring unmanned plane pattern；Moved by fixed-wing fuselage (1), wing (2), empennage (3), horizontal propeller
Force system (4), vertical spin oar electric system (5), support (6), rotor fuselage (7) and payload parts (9) constitute cruise
VUAV pattern.
2. mooring cruise multi-mode VUAV as claimed in claim 1, it is characterised in that: described wing (2) level
It is fixed on fixed-wing fuselage (1) both sides to be symmetric about fixed-wing fuselage (1) mid-plane, during unmanned plane cruising flight,
Himself gravity of liter dynamic balance that wing (2) produces；The main operation rudder face that aileron is aircraft outside wing (2) wing edge after a while,
Rolling moment produced by the differential deflection of left and right aileron makes aircraft rolling on fixed-wing fuselage (1) longitudinal axis.
3. mooring cruise multi-mode VUAV as claimed in claim 1, it is characterised in that: described empennage (3) is distributed
At fixed-wing fuselage (1) afterbody；Empennage (3) is divided into tailplane (3) and vertical tail (3), and tailplane (3) is horizontally arranged at
Fixed-wing fuselage (1) afterbody, the pitching moment that the elevator of tailplane (3) trailing edge produces controls aircraft pitch flight；Vertically
Empennage (3) is vertically mounted on fixed-wing fuselage (1) afterbody, and the rudder of vertical tail (3) trailing edge produces yawing, it is achieved side
To manipulation.
4. mooring cruise multi-mode VUAV as claimed in claim 1, it is characterised in that: described horizontal propeller moves
It is anterior that Force system (4) is positioned at fixed-wing fuselage (1), and including propeller, electromotor and fuel reserve tank, horizontal propeller rotates to be nothing
Man-machine cruising condition provides flying power；Described vertical spin oar electric system (5) is positioned at support (6) end, hangs down for unmanned plane
Lift is provided during straight landing and keeps attitude steady.
5. mooring cruise multi-mode VUAV as claimed in claim 1, it is characterised in that: described support (6) is by revolving
Wing fuselage (7) surrounding stretches out, quick release and installation, and support (6) quantity can be 4,6 or 8, and support (6) is held
Single screw or coaxial installation twin screw are installed by portion.
6. mooring cruise multi-mode VUAV as claimed in claim 1, it is characterised in that: enable mooring unmanned plane mould
During formula, being provided electric power support by carrier to vertical spin oar electric system (5) by cable transmission, airborne power supply is as standby electricity
Power is supported, himself gravity of liter dynamic balance that propeller rotational produces, and when running into the interference factors such as high wind, is protected by electric rotating machine
Hold its smooth flight attitude；When enabling cruise VUAV pattern, airborne power supply is vertical spin oar electric system (5)
Offer electric power is supported.
7. mooring cruise multi-mode VUAV as claimed in claim 1, it is characterised in that: described payload parts
(9) visible light camera and infrared thermography can be carried, it is also possible to carry special emergency communication trunking.
8. mooring cruise multi-mode VUAV as claimed in claim 1, it is characterised in that: described wing (2), support
(6), rotor fuselage (7) all quick releases and installation, space can be saved after dismounting and deposit, needing can be at short notice when using
Fast Installation.
9. mooring cruise multi-mode VUAV as claimed in claim 1, it is characterised in that: described rotor fuselage (7)
Being made up of airborne power supply and control system, airborne power supply provides electric power support for vertical spin oar motor；Control system is by control
The rotation of the deflection of rudder face processed, the rotating speed of propeller and vertical spin oar motor controls the flight path of unmanned plane and keeps it
Steadily attitude.
10. mooring cruise multi-mode VUAV as claimed in claim 1, it is characterised in that: on described cable (8) position
End is connected to rotor fuselage (7) bottom, and lower end is connected to carrier.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610741852.5A CN106114848A (en) | 2016-08-26 | 2016-08-26 | A kind of mooring cruise multi-mode VUAV |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610741852.5A CN106114848A (en) | 2016-08-26 | 2016-08-26 | A kind of mooring cruise multi-mode VUAV |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106114848A true CN106114848A (en) | 2016-11-16 |
Family
ID=57271891
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610741852.5A Pending CN106114848A (en) | 2016-08-26 | 2016-08-26 | A kind of mooring cruise multi-mode VUAV |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106114848A (en) |
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741955A (en) * | 2017-03-10 | 2017-05-31 | 佛山市神风航空科技有限公司 | A kind of fixed wing aircraft landing system and its working method |
| CN106986016A (en) * | 2017-04-06 | 2017-07-28 | 苏州恩济智能科技有限公司 | One kind quickly disconnects adaptive cruise VUAV |
| CN107745804A (en) * | 2017-08-31 | 2018-03-02 | 周鹏跃 | Aircraft and cruising level flight method |
| CN107914893A (en) * | 2017-10-30 | 2018-04-17 | 航宇救生装备有限公司 | One kind is carrier-borne to be tethered at umbrella wing unmanned plane |
| CN108045573A (en) * | 2017-12-05 | 2018-05-18 | 长沙展朔轩兴信息科技有限公司 | Pull in front and others push behind the multi-functional fixed-wing unmanned plane of formula |
| CN108105593A (en) * | 2018-01-29 | 2018-06-01 | 四川尚航智能科技有限公司 | A kind of infrared camera and the unmanned plane that natural gas line inspection is carried out based on infrared camera |
| CN108216607A (en) * | 2018-03-07 | 2018-06-29 | 东莞市锦明运动器材有限公司 | Multi-rotor unmanned aerial vehicle and its control method with hang gliding |
| CN108263606A (en) * | 2018-01-29 | 2018-07-10 | 四川尚航智能科技有限公司 | One kind is based on VTOL fixed-wing unmanned plane and its natural gas line cruising inspection system, method |
| CN108839795A (en) * | 2018-08-01 | 2018-11-20 | 辽宁壮龙无人机科技有限公司 | A kind of Level Promoting multi-rotor unmanned aerial vehicle and control method |
| CN109328161A (en) * | 2017-12-07 | 2019-02-12 | 深圳市大疆创新科技有限公司 | Unmanned vehicle |
| CN109857132A (en) * | 2019-03-12 | 2019-06-07 | 辽宁壮龙无人机科技有限公司 | A kind of flight control assemblies and method |
| CN110740932A (en) * | 2017-04-27 | 2020-01-31 | R·I·米勒 | Systems, methods, and apparatus to improve safety and functionality of aircraft having or more rotors |
| CN111232195A (en) * | 2019-11-05 | 2020-06-05 | 西安羚控电子科技有限公司 | Carrier-borne heavy oil composite wing unmanned aerial vehicle |
| CN112799427A (en) * | 2020-12-28 | 2021-05-14 | 尚良仲毅(沈阳)高新科技有限公司 | Unmanned aerial vehicle control method |
| CN113173246A (en) * | 2021-05-07 | 2021-07-27 | 新疆大学 | Long-endurance composite wing AI automatic detection electric cruise unmanned aerial vehicle and method |
| CN114802734A (en) * | 2022-06-23 | 2022-07-29 | 江苏云端智能科技有限公司 | Cruise unmanned aerial vehicle and system thereof |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103043212A (en) * | 2011-10-17 | 2013-04-17 | 田瑜 | Combined aircraft composed of fixed wing and electric multi-rotor wing |
| CN104118559A (en) * | 2014-06-25 | 2014-10-29 | 中国人民解放军总装备部军械技术研究所 | Virtual mast used for scouting |
| CN104364154A (en) * | 2012-06-01 | 2015-02-18 | 洛高-蒂姆有限责任公司 | Aircraft, preferably unmanned |
| US20160031554A1 (en) * | 2014-07-30 | 2016-02-04 | Siniger LLC | Control system for an aircraft |
| CN105539834A (en) * | 2016-01-12 | 2016-05-04 | 成都纵横自动化技术有限公司 | Composite-wing vertical take-off and landing unmanned aerial vehicle |
| WO2016077391A2 (en) * | 2014-11-11 | 2016-05-19 | Amazon Technologies, Inc. | Unmanned aerial vehicle configuration for extended flight |
-
2016
- 2016-08-26 CN CN201610741852.5A patent/CN106114848A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103043212A (en) * | 2011-10-17 | 2013-04-17 | 田瑜 | Combined aircraft composed of fixed wing and electric multi-rotor wing |
| CN104364154A (en) * | 2012-06-01 | 2015-02-18 | 洛高-蒂姆有限责任公司 | Aircraft, preferably unmanned |
| CN104118559A (en) * | 2014-06-25 | 2014-10-29 | 中国人民解放军总装备部军械技术研究所 | Virtual mast used for scouting |
| US20160031554A1 (en) * | 2014-07-30 | 2016-02-04 | Siniger LLC | Control system for an aircraft |
| WO2016077391A2 (en) * | 2014-11-11 | 2016-05-19 | Amazon Technologies, Inc. | Unmanned aerial vehicle configuration for extended flight |
| CN105539834A (en) * | 2016-01-12 | 2016-05-04 | 成都纵横自动化技术有限公司 | Composite-wing vertical take-off and landing unmanned aerial vehicle |
Cited By (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741955A (en) * | 2017-03-10 | 2017-05-31 | 佛山市神风航空科技有限公司 | A kind of fixed wing aircraft landing system and its working method |
| CN106986016A (en) * | 2017-04-06 | 2017-07-28 | 苏州恩济智能科技有限公司 | One kind quickly disconnects adaptive cruise VUAV |
| CN106986016B (en) * | 2017-04-06 | 2019-09-03 | 苏州恩济智能科技有限公司 | It is a kind of quickly to disconnect adaptive cruise vertical take-off and landing drone |
| CN110740932A (en) * | 2017-04-27 | 2020-01-31 | R·I·米勒 | Systems, methods, and apparatus to improve safety and functionality of aircraft having or more rotors |
| CN107745804A (en) * | 2017-08-31 | 2018-03-02 | 周鹏跃 | Aircraft and cruising level flight method |
| CN107745804B (en) * | 2017-08-31 | 2024-04-16 | 周鹏跃 | Aircraft and cruising flat flight method |
| CN107914893A (en) * | 2017-10-30 | 2018-04-17 | 航宇救生装备有限公司 | One kind is carrier-borne to be tethered at umbrella wing unmanned plane |
| CN108045573A (en) * | 2017-12-05 | 2018-05-18 | 长沙展朔轩兴信息科技有限公司 | Pull in front and others push behind the multi-functional fixed-wing unmanned plane of formula |
| CN109328161A (en) * | 2017-12-07 | 2019-02-12 | 深圳市大疆创新科技有限公司 | Unmanned vehicle |
| WO2019109306A1 (en) * | 2017-12-07 | 2019-06-13 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| CN108263606A (en) * | 2018-01-29 | 2018-07-10 | 四川尚航智能科技有限公司 | One kind is based on VTOL fixed-wing unmanned plane and its natural gas line cruising inspection system, method |
| CN108105593A (en) * | 2018-01-29 | 2018-06-01 | 四川尚航智能科技有限公司 | A kind of infrared camera and the unmanned plane that natural gas line inspection is carried out based on infrared camera |
| CN108216607B (en) * | 2018-03-07 | 2024-03-26 | 东莞市锦明运动器材有限公司 | Multi-rotor unmanned aerial vehicle with gliding wings and control method thereof |
| CN108216607A (en) * | 2018-03-07 | 2018-06-29 | 东莞市锦明运动器材有限公司 | Multi-rotor unmanned aerial vehicle and its control method with hang gliding |
| CN108839795A (en) * | 2018-08-01 | 2018-11-20 | 辽宁壮龙无人机科技有限公司 | A kind of Level Promoting multi-rotor unmanned aerial vehicle and control method |
| CN109857132A (en) * | 2019-03-12 | 2019-06-07 | 辽宁壮龙无人机科技有限公司 | A kind of flight control assemblies and method |
| CN111232195A (en) * | 2019-11-05 | 2020-06-05 | 西安羚控电子科技有限公司 | Carrier-borne heavy oil composite wing unmanned aerial vehicle |
| CN112799427A (en) * | 2020-12-28 | 2021-05-14 | 尚良仲毅(沈阳)高新科技有限公司 | Unmanned aerial vehicle control method |
| CN113173246A (en) * | 2021-05-07 | 2021-07-27 | 新疆大学 | Long-endurance composite wing AI automatic detection electric cruise unmanned aerial vehicle and method |
| CN114802734A (en) * | 2022-06-23 | 2022-07-29 | 江苏云端智能科技有限公司 | Cruise unmanned aerial vehicle and system thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106114848A (en) | A kind of mooring cruise multi-mode VUAV | |
| CN108367803B (en) | Hybrid propulsion type vertical take-off and landing aircraft | |
| CN106394856B (en) | A kind of composite wing unmanned plane | |
| CN106143898B (en) | A kind of VTOL tilting rotor fixed wing aircraft | |
| US9862486B2 (en) | Vertical takeoff and landing aircraft | |
| CA2947688C (en) | Tethered wing structures complex flight path | |
| CN106945827B (en) | Floating body throwing type amphibious four-rotor unmanned aerial vehicle | |
| WO2015200345A1 (en) | Five-wing aircraft to permit smooth transitions between vertical and horizontal flight | |
| CN108750101A (en) | A kind of super maneuver high speed compound unmanned rotary wing aircraft, assembly, assembly and disassembly methods | |
| CN105947192A (en) | Tilting double-duct unmanned aerial vehicle | |
| US11021251B2 (en) | Inset turret assemblies for tiltrotor aircraft | |
| CN110194259B (en) | Intelligent cage-shaped rotor unmanned aerial vehicle | |
| RU2635431C1 (en) | Convertible aircraft | |
| CN203666995U (en) | Three-shaft aerial shooting holder | |
| CN110466750A (en) | A kind of Portable vertical landing scouting monitoring unmanned plane | |
| CN106005371B (en) | Difference directly drives dynamic three rudder face unmanned planes entirely | |
| CN206954505U (en) | One kind is tethered at cruise multi-mode VUAV | |
| CN110466754A (en) | A kind of tailstock formula tilting rotor vertical take-off and landing drone | |
| CN113184185A (en) | Streamlined coaxial many rotor unmanned aerial vehicle of adaptable adverse circumstances | |
| CN112849412A (en) | Hydrogen-electricity nacelle body integrated scouting and batting unmanned aerial vehicle | |
| CN116573179A (en) | Box-type layout tilting rotor miniature unmanned aerial vehicle | |
| CN110562448A (en) | Tailstock type unmanned aerial vehicle | |
| CN111766888A (en) | Aircraft-based control method and aircraft | |
| CN112722264B (en) | Tail sitting type vertical take-off and landing unmanned aerial vehicle | |
| CN104229130A (en) | Four-rotor wing unmanned aerial vehicle with pneumatic structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161116 |