CN108313308A - A kind of rotor for manned more rotor flying vehicles - Google Patents
A kind of rotor for manned more rotor flying vehicles Download PDFInfo
- Publication number
- CN108313308A CN108313308A CN201810208983.6A CN201810208983A CN108313308A CN 108313308 A CN108313308 A CN 108313308A CN 201810208983 A CN201810208983 A CN 201810208983A CN 108313308 A CN108313308 A CN 108313308A
- Authority
- CN
- China
- Prior art keywords
- rotor
- manned
- internal combustion
- combustion engine
- flying vehicles
- 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
- 238000002485 combustion reaction Methods 0.000 claims abstract description 44
- 230000000712 assembly Effects 0.000 claims abstract description 15
- 238000000429 assembly Methods 0.000 claims abstract description 15
- 230000033228 biological regulation Effects 0.000 claims description 7
- 239000000498 cooling water Substances 0.000 claims description 6
- 238000010943 off-gassing Methods 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 230000008859 change Effects 0.000 description 4
- 238000001816 cooling Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000005507 spraying Methods 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000011217 control strategy Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 239000008246 gaseous mixture Substances 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 238000013519 translation Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
- B64D33/10—Radiator arrangement
Abstract
The invention discloses a kind of rotor for manned more rotor flying vehicles, including internal combustion engine, rotor assemblies and vert the mounting base on horn positioned at manned more rotor flying vehicles；The internal combustion engine is horizontally installed in the mounting base, and the rotor assemblies are installed on the output shaft of the internal combustion engine；The internal combustion engine includes internal combustion engine main body and carburetor, and the mixed gas outlet pipe of the carburetor is tiltedly arranged downward.The rotor for manned more rotor flying vehicles of the present invention has many advantages, such as simple in structure, reliable operation, perfect heat-dissipating.
Description
Technical field
The invention mainly relates to vehicle technology fields, refer in particular to a kind of rotor for manned more rotor flying vehicles.
Background technology
Currently, small aircraft is used for carrying various measuring instruments (such as camera) mostly, aerological sounding or high-altitude are carried out
On object is thrown, it can apply in various fields such as agricultural, detection, meteorological, hazard forecasting and rescues.But can be manned it is small
Type aircraft is actually rare, there is larger research space.
Existing aircraft is divided into two kinds of Fixed Wing AirVehicle and rotor craft.Fixed Wing AirVehicle mainly passes through acquisition
Larger initial velocity forms lift in aerofoil and realizes flight, but can not hover, and stability is poor when low speed, be easy because stall and
Air crash, and need larger ground run distance.In addition Fixed Wing AirVehicle is generally turned to using two methods, a kind of pure
It is turned to by vertical tail, one is wing aileron cooperation tailplanes to turn to.Wherein purely the case where ratio is turned to by vertical tail
It is more rare because vertical tail in addition to have control aircraft turn function other than, there are one most important function be just to maintain it is winged
The stabilization of machine, it is impossible to significantly be turned using vertical tail.And wing aileron cooperation tailplane turns to, and is to pass through pair
The lifting of the wing, fuselage is tilted, and is turned round by the effect of centrifugal force, and this mode needs aircraft itself to have inclined effect,
It applies on personal aircraft, the security risk of driver can be increased, be not suitable for personal aircraft and use.
Another is rotor craft, and wherein rotor is primarily used to form lift, and flying speed needs by adjusting appearance
State forms lateral resultant force and could realize, larger and headway is relatively low so as to cause energy expenditure.In addition rotor craft is big
More is all to realize that attitude of flight vehicle changes by change of flight device engine output, or change blade screw pitch；And it is
So that aircraft smooth flight when adjusting each flight attitude needs the rotating speed for accurately calculating engine and change
The screw pitch of blade, process is cumbersome, is not suitable for flight environment of vehicle complicated and changeable, and still will appear inclination in flight course,
The same security risk for increasing driver.The tune of posture can be carried out by adjusting the rotor face of rotor by occurring part at present
It is whole, but the change in the rotor face of rotor can not be effectively adapted to for the layout of each component on rotor and mounting means, it leads
There are more problems for cause, such as windage is larger, air inlet is unsmooth.
Invention content
The technical problem to be solved in the present invention is that：For technical problem of the existing technology, the present invention provides one
The kind rotor for manned more rotor flying vehicles simple in structure, stable and reliable in work.
In order to solve the above technical problems, technical solution proposed by the present invention is：
A kind of rotor for manned more rotor flying vehicles, including internal combustion engine, rotor assemblies and be located at manned more rotors
Flight vehicle verts the mounting base on horn；The internal combustion engine is horizontally installed in the mounting base, the rotor assemblies installation
In on the output shaft of the internal combustion engine；The internal combustion engine includes internal combustion engine main body and carburetor, and the gaseous mixture of the carburetor goes out
Mouth pipe is arranged obliquely along outgassing direction.
As a further improvement of the above technical scheme：
Angle between the axis and horizontal line of the mixed gas outlet pipe of the carburetor is 10~20 degree.
The mixed gas outlet pipe of the carburetor is connect by an air flue connector with the internal combustion engine main body；The air flue
Connector is in the shape of a right-angled ladder along the section of central axes.
The rotor assemblies are located at the lower section of the internal combustion engine main body；The upper horizontal of the internal combustion engine main body is placed with water
Cold plate, the cooled plate are connected with the cooling water inlet of the internal combustion engine main body and cooling water outlet respectively.
Compensator is provided with above the cooled plate, the compensator is connected with the cooled plate, for balancing water cooling
Pressure in plate.
The air door of the carburetor includes air door ontology, air flap and stretching assembly, the side setting of the air door ontology
There are mounting portion, the mounting portion to be provided with the sliding slot of the vestibule of connection air door ontology, the sliding slot is parallel to the cross of the vestibule
Section, the air flap are slidedly arranged in the sliding slot, one end of the stretching assembly stretch in sliding slot with the air flap
Side is connected, and is slided in sliding slot to carry out the aperture regulation of vestibule for stretching air flap.
Fixed setting is parallel to sliding slot and the guide rod through air flap in the sliding slot, and one end of the guide rod extends to
On the inner wall of vestibule.
The sliding slot is arranged return elastic component on the guide rod between the side and air flap of vestibule.
The stretching assembly includes actuator, drum and drawstring, and the drum is installed on the output shaft of the actuator,
One end plate of the drawstring is located on the drum, and the other end is connected with the air flap.
The actuator is steering engine or stepper motor or servo motor.
Compared with the prior art, the advantages of the present invention are as follows：
1, the rotor for manned more rotor flying vehicles of the invention, by by the oblique court of mixed gas outlet pipe of carburetor
Lower setting can ensure the case where mixed gas outlet pipe of carburetor will not occur obliquely when rotor face adjusts, to
When mixed gas outlet pipe can be avoided to be in state obliquely, mixed gas can not be successfully the feelings for spraying into internal combustion engine main body and flowing back
Condition ensures the normal work of internal combustion engine.
2, the rotor for manned more rotor flying vehicles of the invention carries out water cooling to internal combustion engine using water-cooling pattern and dissipates
Heat, perfect heat-dissipating；Wherein cooled plate is horizontally disposed, is not only convenient for radiating, and greatly reduce windage.The top of cooled plate
It is provided with compensator, compensator is connected with cooled plate, for balancing the pressure in cooled plate.
3, the rotor for manned more rotor flying vehicles of the invention, by the air flap that is slidedly arranged in sliding slot to vestibule
Carry out aperture regulation, aperture regulation is accurate, and it is simple in structure, be easily achieved.
Description of the drawings
Fig. 1 is the three-dimensional structure diagram of flight vehicle in the present invention.
Fig. 2 is one of the three-dimensional structure diagram of the present invention.
Fig. 3 is the two of the three-dimensional structure diagram of the present invention.
Fig. 4 is the three-dimensional structure diagram of the air flue connector in the present invention.
Fig. 5 is the three-dimensional structure diagram of carburetor in the present invention.
Fig. 6 is the sectional view of carburetor in the present invention.
Figure label indicates：1, rack；2, fixed horn；3, vert horn；31, vert component；4, rotor；41, it installs
Seat；42, internal combustion engine；421, internal combustion engine main body；422, carburetor；4221, air door ontology；4222, air flap；4223, stretching group
Part；42231, actuator；42232, drum；42233, drawstring；4224, mounting portion；42241, sliding slot；42242, guide rod；
42243, return elastic component；423, air flue connector；43, rotor assemblies；44, cooled plate；45, compensator.
Specific implementation mode
Below in conjunction with Figure of description and specific embodiment, the invention will be further described.
As shown in Figure 1, manned more rotor flying vehicles in the present invention, concrete structure include keel open frame 1, rack 1
Bottom be provided with undercarriage, seat (not shown) is provided in rack 1, the front or dead astern of rack 1 are provided with
The both sides of outwardly extending fixed horn 2, rack 1 are symmetrical and rotation is provided with the outwardly extending horn 3 that verts, and set in rack 1
It is equipped with bearing block, the one end for the horn 3 that verts then is rotatably arranged on by bearing in bearing block, and rotor 4 is fixed on 2 He of fixed horn
It respectively verts the end of horn 3；Be provided between rack 1 and the horn 3 that respectively verts the component 31 that verts (can use conventional belt transmission,
The modes such as chain drive, gear engagement, details are not described herein for concrete structure), for driving the rotation of horn 3 of verting to vert to adjust
The direction (rotor face) of rotor assemblies 43 is tilted along the front or behind of rack 1 on horn 3, coordinates corresponding control strategy, real
Now to the adjustment of the flight attitudes such as the landing of flight vehicle, acceleration and deceleration, steering, translation and hovering, in the process, rack 1 begins
It is in maintenance level state eventually, ensures the traffic safety and riding comfort of driver or passenger.
As shown in Figures 2 and 3, the rotor for manned more rotor flying vehicles of the present embodiment, is installed on the horn 3 that verts
End, specifically include mounting base 41, internal combustion engine 42 and rotor assemblies 43, mounting base 41 is horizontally arranged at the end for the horn 3 that verts
End, internal combustion engine 42 are horizontally installed in mounting base 41, and rotor assemblies 43 are installed on the output shaft of internal combustion engine 42；Internal combustion engine 42 wraps
Internal combustion engine main body 421 and carburetor 422 are included, one end of wherein carburetor 422 is connected with air filtering core device, and the one of carburetor 422
Side is provided with oil inlet, and the mixed gas outlet pipe of carburetor 422 is arranged obliquely along outgassing direction, since the horn 3 that verts is just
It can often rotate when work, be rotated synchronously so as to cause the internal combustion engine 42 that is horizontally arranged in mounting base 41, by by carburetor 422
Mixed gas outlet pipe be tiltedly arranged downward, the mixed gas outlet pipe of carburetor 422 can be ensured when internal combustion engine 42 is integral inclined
The case where will not occurring obliquely, when so as to avoid mixed gas outlet pipe from being in state obliquely, mixed gas can not
The case where smoothly spraying into internal combustion engine main body 421 and flowing back ensures the normal work of internal combustion engine 42.
As shown in Figure 2 to 4, in the present embodiment, between the axis and horizontal line of the mixed gas outlet pipe of carburetor 422
Angle is 10~20 degree, can specifically be selected according to the maximum tilt angle for the horn 3 that verts, i.e., angle is more than maximum tilt angle
Degree；Specifically, the mixed gas outlet pipe of carburetor 422 is connect by an air flue connector 423 with internal combustion engine main body 421, wherein
Air flue connector 423 is in the shape of a right-angled ladder along the section of central axes, as shown in figure 4, wherein one end of i.e. air flue connector 423 is opened
Mouth obliquely, is connected, to make mixed gas outlet pipe obliquely with the fastening of the mixed gas outlet pipe of carburetor 422.
As shown in Figures 2 and 3, in the present embodiment, rotor assemblies 43 are located at the lower section of internal combustion engine main body 421, can avoid
The upper horizontal of damage of the rotor assemblies 43 to driver and passenger, internal combustion engine main body 421 is placed with cooled plate 44, and cooled plate 44 is distinguished
It is connected with the cooling water inlet of internal combustion engine main body 421 and cooling water outlet.Water cooling is carried out to internal combustion engine 42 using cooled plate mode
Heat dissipation, perfect heat-dissipating；Wherein cooled plate 44 is horizontally disposed, is not only convenient for radiating, and greatly reduce windage.Cooled plate 44
Top be provided with compensator 45, compensator 45 is connected with cooled plate 44, for balancing the pressure in cooled plate 44.Certainly, exist
In other embodiments, rotor assemblies 43 can also be located at the top of internal combustion engine main body 421, and water level plate 44 is located at internal combustion engine main body
421 lower section.
As shown in Figure 5 and Figure 6, in the present embodiment, the air door structure in carburetor 422 includes air door ontology 4221, air door
Piece 4222 and stretching assembly 4223, the side of air door ontology 4221 are provided with the mounting portion 4224 of a protrusion, and mounting portion 4224 is set
It is equipped with the sliding slot 42241 of 4221 vestibule of connection air door ontology, sliding slot 42241 is parallel to the cross section of vestibule, wherein air flap
4222 are slidedly arranged in sliding slot 42241, and one end of stretching assembly 4223 stretches to the side phase in sliding slot 42241 with air flap 4222
Even, air flap 4222 is stretched in the interior sliding of sliding slot 42241 to carry out the aperture regulation of vestibule for driving.By being slidedly arranged on sliding slot
Air flap 4222 in 42241 carries out aperture regulation to vestibule, and aperture regulation is accurate, and it is simple in structure, be easily achieved.
It is fixedly installed in the present embodiment, in sliding slot 42241 and is parallel to sliding slot 42241 and the guide rod through air flap 4222
42242, one end of guide rod 42242 extends on the inner wall of vestibule.Specifically, the middle part of air flap 4222 is provided with cavity, leads
Bar 42242 is in the cavity of air flap 4222, and wherein one end is connected with the inner wall of vestibule, and air flap 4222 is in guide rod 42242
Upper sliding ensures the smoothness of sliding.In addition, guide rod of the sliding slot 42241 between the side and air flap 4222 of vestibule
Return elastic component 42243 (such as compressed spring) is arranged on 42242, when stretching assembly 4223 does not work, return elastic component 42243
Air flap 4222 is recoiled to initial position (closed position) by rebound.
In the present embodiment, stretching assembly 4223 includes actuator 42231, drum 42232 and drawstring 42233, drum 42232
It is installed on the output shaft of actuator 42231, an end plate of drawstring 42233 is located on drum 42232, the other end and air flap
4222 are connected.Actuator 42231 is steering engine or stepper motor or servo motor.Wherein preferred steering engine, passes through the rotation of steering engine, line
Disk 42232 rotates therewith, and pulls drawstring 42233 to be rotated in the wire casing of drum 42232, makes air flap 4222 in sliding slot 42241
Interior sliding, to realize the accurate adjusting of aperture.
The above is only the preferred embodiment of the present invention, protection scope of the present invention is not limited merely to above-described embodiment,
All technical solutions belonged under thinking of the present invention all belong to the scope of protection of the present invention.It should be pointed out that for the art
For those of ordinary skill, several improvements and modifications without departing from the principles of the present invention should be regarded as the protection of the present invention
Range.
Claims (10)
1. a kind of rotor for manned more rotor flying vehicles, which is characterized in that including internal combustion engine (42), rotor assemblies (43)
With the mounting base (41) on the horn that verts (3) of manned more rotor flying vehicles；The internal combustion engine (42) is horizontally installed to
On the mounting base (41), the rotor assemblies (43) are installed on the output shaft of the internal combustion engine (42)；The internal combustion engine
(42) include internal combustion engine main body (421) and carburetor (422), the mixed gas outlet pipe of the carburetor (422) is along outgassing direction
It is arranged obliquely.
2. the rotor according to claim 1 for manned more rotor flying vehicles, which is characterized in that the carburetor
(422) angle between the axis and horizontal line of mixed gas outlet pipe is 10~20 degree.
3. the rotor according to claim 1 for manned more rotor flying vehicles, which is characterized in that the carburetor
(422) mixed gas outlet pipe is connect by an air flue connector (423) with the internal combustion engine main body (421)；The air flue connects
Fitting (423) is in the shape of a right-angled ladder along the section of central axes.
4. the rotor according to claim 1 for manned more rotor flying vehicles, which is characterized in that the rotor assemblies
(43) it is located at the lower section of the internal combustion engine main body (421)；The upper horizontal of the internal combustion engine main body (421) is placed with cooled plate
(44), the cooled plate (44) is connected with the cooling water inlet of the internal combustion engine main body (421) and cooling water outlet respectively.
5. the rotor according to claim 4 for manned more rotor flying vehicles, which is characterized in that the cooled plate
(44) compensator (45) is provided with above, the compensator (45) is connected with the cooled plate (44), for balancing cooled plate
(44) pressure in.
6. the rotor as claimed in any of claims 1 to 5 for manned more rotor flying vehicles, feature exists
In the air door of, the carburetor (422) include air door ontology (4221), air flap (4222) and stretching assembly (4223), it is described
The side of air door ontology (4221) is provided with mounting portion (4224), and the mounting portion (4224) is provided with connection air door ontology
(4221) sliding slot (42241) of vestibule, the sliding slot (42241) are parallel to the cross section of the vestibule, the air flap
(4222) it is slidedly arranged in the sliding slot (42241), one end of the stretching assembly (4223) stretches in sliding slot (42241) and institute
The side for stating air flap (4222) is connected, and is slided in sliding slot (42241) to carry out vestibule for stretching air flap (4222)
Aperture regulation.
7. the rotor according to claim 6 for manned more rotor flying vehicles, which is characterized in that the sliding slot
(42241) fixed setting is parallel to sliding slot (42241) and the guide rod (42242) through air flap (4222), the guide rod in
(42242) one end extends on the inner wall of vestibule.
8. the rotor according to claim 7 for manned more rotor flying vehicles, which is characterized in that the sliding slot
(42241) it is arranged return elastic component on the guide rod (42242) between the side of vestibule and air flap (4222)
(42243)。
9. the rotor according to claim 6 for manned more rotor flying vehicles, which is characterized in that the stretching assembly
(4223) include actuator (42231), drum (42232) and drawstring (42233), the drum (42232) is installed on the drive
On the output shaft of moving part (42231), an end plate of the drawstring (42233) is located on the drum (42232), the other end and institute
Air flap (4222) is stated to be connected.
10. the rotor according to claim 9 for manned more rotor flying vehicles, which is characterized in that the actuator
(42231) it is steering engine or stepper motor or servo motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810208983.6A CN108313308A (en) | 2018-03-14 | 2018-03-14 | A kind of rotor for manned more rotor flying vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810208983.6A CN108313308A (en) | 2018-03-14 | 2018-03-14 | A kind of rotor for manned more rotor flying vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108313308A true CN108313308A (en) | 2018-07-24 |
Family
ID=62901964
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810208983.6A Pending CN108313308A (en) | 2018-03-14 | 2018-03-14 | A kind of rotor for manned more rotor flying vehicles |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108313308A (en) |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR970049946U (en) * | 1996-01-31 | 1997-08-12 | 대우전자주식회사 | Primary air control device for blower for oil combustor |
| CN1683773A (en) * | 2004-03-03 | 2005-10-19 | 本田技研工业株式会社 | Device for controlling choke valve of carburetor |
| CN102991673A (en) * | 2012-12-17 | 2013-03-27 | 刘斌 | New type one-man flight vehicle capable of vertically taking off and landing and with fixed wings |
| CN103883429A (en) * | 2013-07-24 | 2014-06-25 | 王树卿 | Three-level regulation type novel carburetor |
| CN203727646U (en) * | 2014-03-13 | 2014-07-23 | 中国科学院沈阳自动化研究所 | Unmanned helicopter |
| CN104295368A (en) * | 2014-09-25 | 2015-01-21 | 重庆特飞航空动力科技有限公司 | Single-cylinder two-stroke water-cooled engine integrating silencer with cooling system |
| CN104727980A (en) * | 2013-12-19 | 2015-06-24 | 本田技研工业株式会社 | Control apparatus for general purpose machine |
| CN105121188A (en) * | 2013-03-15 | 2015-12-02 | 特力飞车股份有限公司 | Combined flying/driving vehicle with vertical takeoff and fixed-wing cruise capabilities |
| CN105398570A (en) * | 2015-11-26 | 2016-03-16 | 北京浩恒征途航空科技有限公司 | Oil-operated multi- rotor aerocraft |
| CN107288779A (en) * | 2016-04-12 | 2017-10-24 | 哈尔滨飞机工业集团有限责任公司 | A kind of operating mechanism of control engine choke aperture |
| CN208007305U (en) * | 2018-03-14 | 2018-10-26 | 长沙市云智航科技有限公司 | A kind of rotor for manned more rotor flying vehicles |
-
2018
- 2018-03-14 CN CN201810208983.6A patent/CN108313308A/en active Pending
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR970049946U (en) * | 1996-01-31 | 1997-08-12 | 대우전자주식회사 | Primary air control device for blower for oil combustor |
| CN1683773A (en) * | 2004-03-03 | 2005-10-19 | 本田技研工业株式会社 | Device for controlling choke valve of carburetor |
| CN102991673A (en) * | 2012-12-17 | 2013-03-27 | 刘斌 | New type one-man flight vehicle capable of vertically taking off and landing and with fixed wings |
| CN105121188A (en) * | 2013-03-15 | 2015-12-02 | 特力飞车股份有限公司 | Combined flying/driving vehicle with vertical takeoff and fixed-wing cruise capabilities |
| CN103883429A (en) * | 2013-07-24 | 2014-06-25 | 王树卿 | Three-level regulation type novel carburetor |
| CN104727980A (en) * | 2013-12-19 | 2015-06-24 | 本田技研工业株式会社 | Control apparatus for general purpose machine |
| CN203727646U (en) * | 2014-03-13 | 2014-07-23 | 中国科学院沈阳自动化研究所 | Unmanned helicopter |
| CN104295368A (en) * | 2014-09-25 | 2015-01-21 | 重庆特飞航空动力科技有限公司 | Single-cylinder two-stroke water-cooled engine integrating silencer with cooling system |
| CN105398570A (en) * | 2015-11-26 | 2016-03-16 | 北京浩恒征途航空科技有限公司 | Oil-operated multi- rotor aerocraft |
| CN107288779A (en) * | 2016-04-12 | 2017-10-24 | 哈尔滨飞机工业集团有限责任公司 | A kind of operating mechanism of control engine choke aperture |
| CN208007305U (en) * | 2018-03-14 | 2018-10-26 | 长沙市云智航科技有限公司 | A kind of rotor for manned more rotor flying vehicles |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103395491B (en) | Shrouded propeller system of can cracking and use the hovercar of this system | |
| CN105346719B (en) | Vertically taking off and landing flyer | |
| CN108082466A (en) | A kind of tilting duct connection wing layout vertically taking off and landing flyer | |
| CN104816823A (en) | Duct rotary wing aircraft | |
| CN110418755A (en) | A kind of unmanned vehicle | |
| CN106697282A (en) | Duct type tilting aircraft with vertical take-off and landing functions | |
| CN204623838U (en) | A kind of duct rotor craft | |
| CN104787322B (en) | Power system and multi-axis aircraft | |
| CN108275263A (en) | A kind of manned more rotor flying vehicles | |
| CN208007305U (en) | A kind of rotor for manned more rotor flying vehicles | |
| CN108298071A (en) | A kind of more rotor flying vehicles of manned duct | |
| CN207972814U (en) | Rotor for manned more rotor flying vehicles | |
| CN208248492U (en) | A kind of manned more rotor flying vehicles | |
| CN207972801U (en) | The component that verts for the more rotor flying vehicles of manned duct | |
| CN106314789A (en) | Wing, fixed-wing aircraft and fixed-wing aircraft lifting method | |
| CN109398072A (en) | Intelligent air-inlet grille | |
| CN207045724U (en) | Rotor craft | |
| CN106945826B (en) | Aircraft | |
| CN108313308A (en) | A kind of rotor for manned more rotor flying vehicles | |
| CN108298074A (en) | The component that verts for the more rotor flying vehicles of manned duct | |
| CN108313310A (en) | Rotor for manned more rotor flying vehicles | |
| CN206031774U (en) | Wing reaches decides wing machine | |
| CN106516100A (en) | Vertical takeoff and landing aircraft | |
| CN206155777U (en) | Aircraft | |
| CN207972798U (en) | The component that verts for manned more rotor flying vehicles |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |