CN205216194U - But fixed -wing aircraft of VTOL - Google Patents
But fixed -wing aircraft of VTOL Download PDFInfo
- Publication number
- CN205216194U CN205216194U CN201520377605.2U CN201520377605U CN205216194U CN 205216194 U CN205216194 U CN 205216194U CN 201520377605 U CN201520377605 U CN 201520377605U CN 205216194 U CN205216194 U CN 205216194U
- Authority
- CN
- China
- Prior art keywords
- fuselage
- aircraft
- vtol
- rudder face
- fixed
- 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.)
- Expired - Fee Related
Links
Landscapes
- Toys (AREA)
Abstract
The utility model provides a but fixed -wing aircraft of VTOL, its structure is, it includes nose section, nose section contains the motor again, frame, screw and fixed portion, the fuselage part is carried mechanisms such as thing frame and guide plate and is melted the triangle appearance to a fuselage including the fuselage mainboard, and the vertical tail structure fuses with the fuselage to formation has four vertical fins, two rudders, and two ailerons, the special structural form of two undercarriages, four vertical fins lie in the waist both sides respectively and have a determining deviation, and two liang vertical fins are about center line symmetry, and the perpendicular to fuselage, have the twocouese rudder face, and the rudder lies in the vertical fin below, the fuselage the below be a pair of symmetrical aileron that is trapezoidal form, what be located the fuselage both sides is two undercarriages, plays supporting role, and whole fuselage just leans on the undercarriage on both sides to support, except above structure division aircraft also has the most important electric power system, include power supply system, signal receiving and processing system, brake control system.
Description
Technical field
The utility model relates to the aircraft of vertical lift, particularly relate to a kind of can the fixed wing aircraft of VTOL.
Background technology
Model airplane is with a long history, and it produces along with sending out of mankind's aviation industry.From in spacelike development history, before the invention of the aerodone that navigates as far back as exhibition, aircraft, explore the pioneers of mankind's flight, just imitate the feature of Bird Flight, attempt manufacturing simple aircraft.And first many searchers replace the flight test that need take one's life in one's hands with model.In the development of aviation industry, model airplane plays the effect of pioneer really.Russian big science man Luo Mengnuosuo as done great propelling to the research of rising aircraft has manufactured the model of first aircraft in the world on April 4th, 1.The principle of this airplane flight is very simple, and two screws are contained on same vertical axis, rotate, can rise with contrary direction.But due to they " engine " just a bullet builds, elastic force is very little again, and the model of this helicopter can not fly up into the sky sky.But its first time in human history demonstrates and utilizes the screw rotated at horizontal plane can vertical flight, namely can produce lift with screw, after, others has made the formula that can be used for accurately calculating helicopter screw according to the experiment divided.The application of this principle, just develops into modern close coupled type helicopter.
But along with the development of science and technology, aircraft obtains very important use in a lot of field, but a lot of local aircraft do not have enough fields for taking off, and the place of landing at any time change.Also lack reply at present in bad environments situation, still can the aircraft risen and fallen of vertical lift, the model airplane of current helicopter is generally applicable to home entertaining, make the development of telecontrolled aircraft be tending towards profile improve and manipulation multi-functional while, and have ignored under special circumstances, the transport etc. of article in such as bad weather situation.Meet the helicopter of these conditions because its oil consumption, and can not landing and these requirements can not be met when bad environments.
Aircraft of the present utility model solves this difficult problem just, this aircraft is used for the bad environments that takes off, especially large aircraft can not the place of landing, and the flight of certain weight can be loaded, still flight controller auxiliary operation can be used when harsh environmental conditions, the fixed wing aircraft of VTOL draws simple to operate, and be easy to carry about with one advantage of lower cost, but also is unmanned.And this aircraft can be used for the advantage in the not fly able place of some conventional airplanes.
Utility model content
The purpose of this utility model be to provide a kind of can the fixed wing aircraft of VTOL, it has and uses simple, only needs its to launch assembling energising, opens remote control equipment and exercisable telecontrolled aircraft.
The utility model is achieved like this, a kind of can the fixed wing aircraft of VTOL, it comprises head, fuselage, support, rise and fall support and power system, is a kind of removable UAV.
The head of described aircraft comprises motor, screw and motor fixed rack, and screw is arranged at head upper end and removably connects.
Described fuselage comprises wing, aileron and four vertical fins; Each wing and fuselage sections form spandrel frame, and described aileron is arranged on described fuselage bottom, and are a pair symmetrical ailerons in trapezoidal shape; Described four vertical fins lay respectively at fuselage both sides and at regular intervals, between two at same plane, symmetrical about center line; Also be provided with twocouese rudder face at vertical fin afterbody, described twocouese rudder face is arranged at vertical fin and fuselage junction, adopts that hinge is collapsible to be connected between rudder face with rudder face, is fixed after folding by the snap close be arranged on fuselage.
Described Bracket setting in the both sides of airframe, described support with adopt between fuselage that hinge is collapsible to be connected.
Preferably, be provided with deflector and article storeroom at the middle part of described airframe, described article storeroom is woven by gauze and forms, and the material of gauze can be the material that nylon wire, fishing line, crystal elastic line or other pliability and fastness are good.
Preferably, described partial power is made up of electric power system, signal processing system and braking control system, and each rudder face is rotated by steering wheel and controls.
The beneficial effects of the utility model are: this VTOL aircraft is the specific function itself had by the value used, be easy to carry about with one, can the scope of application extensive, in the human world in future, it can be quick, no matter the use in place, has preemptive advantage.In similar aircraft, it is exactly an outstanding person.
Accompanying drawing explanation
Fig. 1 is body element structural representation of the present utility model.
Fig. 2 is accessory part structural representation of the present utility model.
Fig. 3 is parts assembly drawing of the present utility model.
Fig. 4 is assembly and adjustment figure of the present utility model.
In the drawings, 1, main body 2, vertical fin 3, deflector 4, undercarriage 5, aileron 6, rudder 7, loading frame 8, screw 9, battery 10, pilot 11, power-supply controller of electric 12, steering wheel 13, remote controller.
Detailed description of the invention
Below in conjunction with accompanying drawing, detailed description of the invention of the present utility model is described further.
As shown in Figure 1, Figure 2, Figure 3 shows, the utility model is achieved like this, a kind of can the fixed wing aircraft of VTOL, it comprises head, fuselage, empennage, undercarriage and power system, is a kind of removable UAV.
The head of described aircraft comprises motor, screw and motor fixed rack, and screw is arranged at head upper end and removably connects.
Described fuselage comprises wing, aileron and four vertical fins; Each wing and fuselage sections form spandrel frame, and described aileron is arranged on described fuselage bottom, and are a pair symmetrical ailerons in trapezoidal shape; Described four vertical fins lay respectively at fuselage both sides and at regular intervals, between two at same plane, symmetrical about center line; Also be provided with twocouese rudder face at vertical fin afterbody, described twocouese rudder face is arranged at vertical fin and fuselage junction, adopts that hinge is collapsible to be connected between rudder face with rudder face, is fixed after folding by the snap close be arranged on fuselage.Only needing when you will use folded part to launch, during expansion, will noticing that snap close and fuselage to connecting, will open remote control equipment, aircraft have four can be movable rudder face, wherein two is the control for direction, and two is aileron in addition.
Described Bracket setting in the both sides of airframe, described support with adopt between fuselage that hinge is collapsible to be connected.Be provided with deflector and article storeroom at the middle part of described airframe, described article storeroom is woven by gauze and forms, and the material of gauze can be the material that nylon wire, fishing line, crystal elastic line or other pliability and fastness are good.Described partial power is made up of electric power system, signal processing system and braking control system, and each rudder face is rotated by steering wheel and controls.
The manipulation of VTOL aircraft needs to have certain prerequisite, because use the ABC with model manipulation of line electricity equipment manipulation aircraft, can carry with when you go out outside, it also may be used for performance, and the utility model in use, folded part is only needed to launch, to notice during expansion that snap close and fuselage to connecting, will open remote control equipment, aircraft have four can be movable rudder face, wherein two is the control for direction, and also having two is aileron.When determining that plane leaving checks each pith.The correction of all directions to be carried out, to ensure its correct flight after taking off.As the factors such as weather affect your manipulation, you can open flight controller (abbreviation flies control), and the stability of getting off the plane in the assistance flying to control can improve a lot.Should be manual after aircraft flies to certain altitude it is changed into the flat flight attitude of fixed-wing, can greatly reduce in the fixed-wing energy resource consumption of getting off the plane of flying, this contributes to improving flying distance very much.The advantage of Here it is VTOL aircraft aspect, both there is VTOL function, there is again fixed-wing and equal the performance flown, after aircraft flies to destination, aircraft had been changed into VTOL state, and carrying out deceleration landing, aircraft just completes flight task like this.Its operation requirements ability is not high.The fan that can be applicable to liking aircraft uses.This aircraft can be applicable to all kinds of in the activity of public service.Such as in individual class search and rescue task, when some tasks be artificially be difficult to accomplish when, VTOL aircraft can be used on the spot to be contained in search and rescue equipment search and rescue, also have at some Code in Hazardous Special Locations not as high temperature, in situation, VTOL aircraft can replace people for completing.These can reduce and bring larger loss.
Claims (4)
1. can the fixed wing aircraft of VTOL, it is characterized in that, it comprises head, fuselage, support, rise and fall support and power system; The head of described aircraft comprises motor, screw and motor fixed rack, and screw is arranged at head upper end and removably connects; State fuselage and comprise wing, aileron and four vertical fins; Each wing and fuselage sections form spandrel frame, and described aileron is arranged on described fuselage bottom, and are a pair symmetrical ailerons in trapezoidal shape; Described four vertical fins lay respectively at fuselage both sides and at regular intervals, between two at same plane, symmetrical about center line; Also be provided with twocouese rudder face at vertical fin afterbody, described twocouese rudder face is arranged at vertical fin and fuselage junction, adopts that hinge is collapsible to be connected between rudder face with rudder face, is fixed after folding by the snap close be arranged on fuselage.
2. as claimed in claim 1 can the fixed wing aircraft of VTOL, it is characterized in that, described Bracket setting in the both sides of airframe, described support with adopt between fuselage that hinge is collapsible to be connected.
3. as claimed in claim 2 can the fixed wing aircraft of VTOL, it is characterized in that, deflector and article storeroom is provided with at the middle part of described airframe, described article storeroom is woven by gauze and forms, and the material of gauze can be the material that nylon wire, fishing line, crystal elastic line or other pliability and fastness are good.
4. as claimed in claim 3 can the fixed wing aircraft of VTOL, it is characterized in that, described partial power is made up of electric power system, signal processing system and braking control system, and each rudder face is rotated by steering wheel and controls.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520377605.2U CN205216194U (en) | 2015-06-05 | 2015-06-05 | But fixed -wing aircraft of VTOL |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520377605.2U CN205216194U (en) | 2015-06-05 | 2015-06-05 | But fixed -wing aircraft of VTOL |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205216194U true CN205216194U (en) | 2016-05-11 |
Family
ID=55891292
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520377605.2U Expired - Fee Related CN205216194U (en) | 2015-06-05 | 2015-06-05 | But fixed -wing aircraft of VTOL |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205216194U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106516097A (en) * | 2016-10-19 | 2017-03-22 | 吴瑞霞 | Unpiloted aircraft |
| CN107364572A (en) * | 2017-08-11 | 2017-11-21 | 红河学院 | Fixed-wing vector unmanned plane |
| CN114080352A (en) * | 2019-08-09 | 2022-02-22 | 迪斯尼实业公司 | Air performance system using Unmanned Aerial Vehicle (UAV) energy to animate creative performance elements |
-
2015
- 2015-06-05 CN CN201520377605.2U patent/CN205216194U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106516097A (en) * | 2016-10-19 | 2017-03-22 | 吴瑞霞 | Unpiloted aircraft |
| CN107364572A (en) * | 2017-08-11 | 2017-11-21 | 红河学院 | Fixed-wing vector unmanned plane |
| CN107364572B (en) * | 2017-08-11 | 2024-01-30 | 昆明学院 | Fixed wing vector unmanned plane |
| CN114080352A (en) * | 2019-08-09 | 2022-02-22 | 迪斯尼实业公司 | Air performance system using Unmanned Aerial Vehicle (UAV) energy to animate creative performance elements |
| CN114080352B (en) * | 2019-08-09 | 2024-05-24 | 迪斯尼实业公司 | Air performance system using Unmanned Aerial Vehicle (UAV) energy to animate creative performance elements |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104816824B (en) | Fixed structure formula VTOL aircraft based on round trip flight Ore-controlling Role and control method thereof | |
| US7922115B2 (en) | Modular unmanned air-vehicle | |
| US20140197280A1 (en) | Delta Wing Unmanned Aerial Vehicle (UAV) and Method of Manufacture of the Same | |
| CN111315655B (en) | Assembly of three composite wings for an air, water, land or space vehicle | |
| CN103979104B (en) | One can variant X-type wing vertical landing minute vehicle | |
| CN103332293A (en) | Tilting double-duct subminiature unmanned plane | |
| US10562626B2 (en) | Tandem wing aircraft with variable lift and enhanced safety | |
| CN105947192A (en) | Tilting double-duct unmanned aerial vehicle | |
| CN205256677U (en) | Modular solar energy spacecraft | |
| CN103600843B (en) | The unmanned plane that hand-thrown takes off | |
| CN204173155U (en) | A kind of delta-wing aircraft | |
| CN205216194U (en) | But fixed -wing aircraft of VTOL | |
| CN110844065A (en) | Unmanned aerial vehicle with strong loading capacity and capable of vertically taking off and landing | |
| US20170369163A1 (en) | Aircraft system and method for vertical takeoff and landing | |
| CN205221105U (en) | Solar energy VTOL fixed wing uavs | |
| CN108528710B (en) | Aerodynamic layout of flapping wing matrix aircraft | |
| CN106005394A (en) | Rescue aircraft | |
| CN106005371B (en) | Difference directly drives dynamic three rudder face unmanned planes entirely | |
| CN204489187U (en) | A kind of vertical takeoff and landing horizontal flight unmanned plane | |
| CN104260873A (en) | Delta wing aircraft | |
| CN205022854U (en) | Deformable compound aircraft | |
| CN110466754A (en) | A kind of tailstock formula tilting rotor vertical take-off and landing drone | |
| CN203842313U (en) | Novel remote control model with combination of vertical take-off and landing and level fight characteristic of fixed wing | |
| CN209581875U (en) | A kind of combined dual-purpose unmanned plane | |
| CN206384131U (en) | A kind of composite wing unmanned plane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160511 Termination date: 20170605 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |