CN109501539A - One kind downsizes aircraft - Google Patents
One kind downsizes aircraft Download PDFInfo
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- CN109501539A CN109501539A CN201710831283.8A CN201710831283A CN109501539A CN 109501539 A CN109501539 A CN 109501539A CN 201710831283 A CN201710831283 A CN 201710831283A CN 109501539 A CN109501539 A CN 109501539A
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- aircraft
- automatic
- downsizes
- propeller
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Power-Operated Mechanisms For Wings (AREA)
Abstract
Downsize aircraft the invention discloses one kind, feature, can land sailing, VTOL flight also can be switched；The aircraft is made of mechanical part and circuit control part；Wherein, the mechanical part includes: car body and rotor driver；The circuit control part include: can anti-strong wind automatic-balancing system, self-navigation, automatic anti-avoiding device, automatic suspension stop system, automatic height-lock control setting system, propeller be short of power appliance for releasing single parachuting drop system.The present invention uses totally-enclosed opposed access door cabin, more rotor power systems；It can also can on the way be travelled with VTOL airflight, to be multi-functional the be following new vehicles, can carry 2 to 12 people, and the control system of inside installation can be balanced with automatic landing when rising and falling and facing a danger of aircraft etc.；Compared with prior art, have the characteristics that at low cost, easy to operate, control is flexible, highly effective and safe, function-stable.
Description
Technical field
The present invention relates to vehicle technology field, more particularly to one kind downsizes aircraft.
Background technique
In recent years with the development of electronic technology and control technology, electronic quadrotor bug has obtained rapid hair
Exhibition, each rotor have an individual motor control respectively.But the type aircraft is mainly used for taking photo by plane, model plane demonstration flight
Deng.But due to using very big restriction is all received in power drive mode, the horsepower of aircraft and cruise duration, at present
It is also difficult to obtain practical popularization.And four propellers of traditional four-axle aircraft are all the simple mechanisms of motor direct-connected, ten
The layout of font, aircraft obtains the power of main body turning by changing motor speed, so as to adjust flight attitude.
Therefore, how to provide it is a kind of have the characteristics that at low cost, easy to operate, control flexibly, highly effective and safe, function-stable
The problem of aircraft that downsizes is those skilled in the art's urgent need to resolve.
Summary of the invention
In view of this, the present invention provides one kind to have the function of that at low cost, easy to operate, control is flexible, highly effective and safe, steady
Determine the aircraft that downsizes of feature.
To achieve the above object, the invention provides the following technical scheme:
One kind downsizes aircraft, feature, can land sailing, VTOL flight also can be switched；The aircraft is by machine
Tool part and circuit control part composition；Wherein, the mechanical part includes: car body and rotor driver；The circuit control portion
Point including: can anti-strong wind automatic-balancing system, self-navigation, automatic anti-avoiding device, automatic suspension stop system, automatic height-lock control
Setting system, propeller are short of power appliance for releasing single parachuting drop system.
Preferably, downsize in aircraft in above-mentioned one kind, the aircraft uses oil electric mixed dynamic system, straight on land
It connects switching driving dynamical system and carries out land walking, need when flight directly to switch oily power power generating device by conversion and directly power band
Dynamic rotor high-speed motor work, aircraft can fly in the sky at 3000 meters or less, 150 kilometers of speed per hour or more per hour, full
Carrying oil can be non-stop flight 3 hours aerial, it is contemplated that 450 kilometers or more.
Preferably, downsize in aircraft in above-mentioned one kind, the two sides of the car body are provided with car door, cabin can carry 2
To 12 people.
Preferably, downsize in aircraft in above-mentioned one kind, the rotor driver is mounted on the upper end of the car body, by 4
Propeller composition.
Preferably, downsize in aircraft in above-mentioned one kind, be fixed with central axis at the center of the propeller, outside is equipped with
Steel ring.
Preferably, downsize in aircraft in above-mentioned one kind, be the axle center of dynamical system in the centre of the propeller, and
Parachute ejection door.
It can be seen via above technical scheme that compared with prior art, downsize aircraft the present disclosure provides one kind,
Its feature, can land sailing, also can be switched VTOL flight；The aircraft is by mechanical part and circuit control part group
At；Wherein, the mechanical part includes: car body and rotor driver；The circuit control part includes: can anti-strong wind autobalance
System, self-navigation, automatic anti-avoiding device, automatic suspension stop system, automatic height-lock control setting system, propeller are short of power
Appliance for releasing single parachuting drop system.The present invention uses totally-enclosed opposed access door cabin, more rotor power systems；It can vertically rise
Airflight is dropped, can also on the way be travelled, to be multi-functional the be following new vehicles can carry 2 to 12 people, inside installation
Control system can be with aircraft balance of automatic landing when rising and falling and facing a danger etc.；Compared with prior art, have
It is at low cost, easy to operate, control flexibly, highly effective and safe, function-stable the characteristics of.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
The embodiment of invention for those of ordinary skill in the art without creative efforts, can also basis
The attached drawing of offer obtains other attached drawings.
Fig. 1 attached drawing is schematic view of the front view of the invention.
Fig. 2 attached drawing is overlooking structure diagram of the invention.
Fig. 3 attached drawing is side structure schematic view of the invention.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
The embodiment of the invention discloses one kind at low cost, easy to operate, control is flexible, highly effective and safe, function-stable
The aircraft that downsizes of feature.
Attached drawing 1, attached drawing 2, attached drawing 3 are please referred to, downsizes aircraft for one kind disclosed by the invention, specifically includes:
One kind downsizes aircraft, feature, can land sailing, VTOL flight also can be switched；The aircraft is by machine
Tool part and circuit control part composition；Wherein, mechanical part includes: car body 1 and rotor driver 2；Circuit control part includes:
It can anti-strong wind automatic-balancing system, self-navigation, automatic anti-avoiding device, automatic suspension stop system, automatic height-lock control setting system
System, propeller are short of power appliance for releasing single parachuting drop system.
The present invention uses totally-enclosed opposed access door cabin, more rotor power systems；It can with VTOL airflight,
It can on the way travel, to be multi-functional the be following new vehicles can carry 2 to 12 people, the control system of inside installation can
With automatic landing balance when rising and falling and facing a danger etc. of aircraft；Compared with prior art, there is at low cost, operation side
Just, control flexibly, highly effective and safe, function-stable the characteristics of.
In order to further optimize the above technical scheme, aircraft uses oil electric mixed dynamic system, directly switches on land
Dynamical system of driving a vehicle carries out land walking, needs when flight directly to switch oily power power generating device by conversion and directly power drive rotor
High-speed motor work, aircraft can fly in the sky at 3000 meters or less, and 150 kilometers of speed per hour or more per hour, fully loaded oil can
With aerial non-stop flight 3 hours, it is contemplated that 450 kilometers or more.
In order to further optimize the above technical scheme, the two sides of car body 1 are provided with car door 11, cabin can carry 2 to 12
People.
In order to further optimize the above technical scheme, rotor driver is mounted on the upper end of car body 1, by 4 21 groups of propeller
At.
In order to further optimize the above technical scheme, it is fixed with central axis 22 at the center of propeller 21, outside is equipped with steel
Circle 23.
In order to further optimize the above technical scheme, in the axle center that the centre of propeller 21 is dynamical system, and landing
Umbrella ejection door.
Each embodiment in this specification is described in a progressive manner, the highlights of each of the examples are with other
The difference of embodiment, the same or similar parts in each embodiment may refer to each other.For device disclosed in embodiment
For, since it is corresponded to the methods disclosed in the examples, so being described relatively simple, related place is said referring to method part
It is bright.
The foregoing description of the disclosed embodiments enables those skilled in the art to implement or use the present invention.
Various modifications to these embodiments will be readily apparent to those skilled in the art, as defined herein
General Principle can be realized in other embodiments without departing from the spirit or scope of the present invention.Therefore, of the invention
It is not intended to be limited to the embodiments shown herein, and is to fit to and the principles and novel features disclosed herein phase one
The widest scope of cause.
Claims (6)
- The aircraft 1. one kind downsizes, feature, can land sailing, also can be switched VTOL flight；The aircraft is by machinery Part and circuit control part composition；Wherein, the mechanical part includes: car body and rotor driver；The circuit control part Include: can anti-strong wind automatic-balancing system, self-navigation, automatic anti-avoiding device, automatic suspension stop system, automatic height-lock control set Set system, propeller is short of power appliance for releasing single parachuting drop system.
- The aircraft 2. one kind according to claim 1 downsizes, which is characterized in that the aircraft uses oil electric mixed dynamic System directly switches driving dynamical system on land and carries out land walking, needs directly to switch oily power conversion power generation when flight Device, which is directly powered, drives the work of rotor high-speed motor, and aircraft can fly in the sky at 3000 meters or less, per hour speed per hour 150 kilometers or more, fully loaded oil can be non-stop flight 3 hours aerial, it is contemplated that 450 kilometers or more.
- The aircraft 3. one kind according to claim 1 downsizes, which is characterized in that the two sides of the car body are provided with vehicle Door, cabin can carry 2 to 12 people.
- The aircraft 4. one kind according to claim 1 downsizes, which is characterized in that the rotor driver is mounted on the car body Upper end, be made of 4 propellers.
- The aircraft 5. one kind according to claim 4 downsizes, which is characterized in that in the center of the propeller is fixed with Mandrel, outside are equipped with steel ring.
- The aircraft 6. one kind according to claim 4 downsizes, which is characterized in that in the centre of the propeller be dynamical system The axle center of system and parachute ejection door.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710831283.8A CN109501539A (en) | 2017-09-15 | 2017-09-15 | One kind downsizes aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710831283.8A CN109501539A (en) | 2017-09-15 | 2017-09-15 | One kind downsizes aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109501539A true CN109501539A (en) | 2019-03-22 |
Family
ID=65744782
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710831283.8A Pending CN109501539A (en) | 2017-09-15 | 2017-09-15 | One kind downsizes aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109501539A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110001823A (en) * | 2019-04-19 | 2019-07-12 | 南昌航空大学 | A kind of combined intelligent communication tool system |
| WO2021199051A1 (en) * | 2020-04-03 | 2021-10-07 | Boris Kipnis | Roadable vtol flying car |
Citations (6)
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|---|---|---|---|---|
| CN201390114Y (en) * | 2009-03-06 | 2010-01-27 | 刘国斌 | Triphibian hybrid vehicle |
| CN103522858A (en) * | 2013-10-16 | 2014-01-22 | 北京航空航天大学 | Flying passenger car |
| KR20160137764A (en) * | 2015-05-21 | 2016-12-01 | 한국항공우주연구원 | Personal air vehicle for road-driving and vertical takeoff and landing |
| CN106427434A (en) * | 2016-11-16 | 2017-02-22 | 龙川 | Flying car |
| US20170072755A1 (en) * | 2002-10-01 | 2017-03-16 | Andrew H B Zhou | Amphibious vertical takeoff and landing (vtol) unmanned device with ai (artificial intelligence) data processing mobile and wearable applications apparatus, same as jet drone, jet flying car, private vtol jet, personal jet aircraft with gsp vtol jet engines and self-jet charged and solar cells powered hybrid super jet electrical car all in one (electricity/fuel) |
| CN106799942A (en) * | 2017-04-11 | 2017-06-06 | 李春石 | A kind of air-ground amphibious manned loading aircraft |
-
2017
- 2017-09-15 CN CN201710831283.8A patent/CN109501539A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20170072755A1 (en) * | 2002-10-01 | 2017-03-16 | Andrew H B Zhou | Amphibious vertical takeoff and landing (vtol) unmanned device with ai (artificial intelligence) data processing mobile and wearable applications apparatus, same as jet drone, jet flying car, private vtol jet, personal jet aircraft with gsp vtol jet engines and self-jet charged and solar cells powered hybrid super jet electrical car all in one (electricity/fuel) |
| CN201390114Y (en) * | 2009-03-06 | 2010-01-27 | 刘国斌 | Triphibian hybrid vehicle |
| CN103522858A (en) * | 2013-10-16 | 2014-01-22 | 北京航空航天大学 | Flying passenger car |
| KR20160137764A (en) * | 2015-05-21 | 2016-12-01 | 한국항공우주연구원 | Personal air vehicle for road-driving and vertical takeoff and landing |
| CN106427434A (en) * | 2016-11-16 | 2017-02-22 | 龙川 | Flying car |
| CN106799942A (en) * | 2017-04-11 | 2017-06-06 | 李春石 | A kind of air-ground amphibious manned loading aircraft |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110001823A (en) * | 2019-04-19 | 2019-07-12 | 南昌航空大学 | A kind of combined intelligent communication tool system |
| WO2021199051A1 (en) * | 2020-04-03 | 2021-10-07 | Boris Kipnis | Roadable vtol flying car |
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| PB01 | Publication | ||
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| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190322 |