CN107323668B - A kind of no rotor remotely-piloted vehicle - Google Patents
A kind of no rotor remotely-piloted vehicle Download PDFInfo
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- CN107323668B CN107323668B CN201710599541.4A CN201710599541A CN107323668B CN 107323668 B CN107323668 B CN 107323668B CN 201710599541 A CN201710599541 A CN 201710599541A CN 107323668 B CN107323668 B CN 107323668B
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- 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
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
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- Structures Of Non-Positive Displacement Pumps (AREA)
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Abstract
The invention discloses a kind of no rotor remotely-piloted vehicles, belong to jet aircraft field.It is of the invention without rotor remotely-piloted vehicle, including annular air blast cavity, turbo-blower structure and warehouse, warehouse is fixed on the centre of annular air blast cavity, toroidal cavity is equipped in annular air blast cavity, the at least three groups partitions that toroidal cavity equal part is isolated into mutually indepedent region are equipped in toroidal cavity, the middle part of each isolated area of toroidal cavity is accordingly uniformly arranged one group for blasting the turbo-blower structure of air-flow into toroidal cavity on the lateral wall of annular air blast cavity, annular air blast cavity, which is equipped with a circle, jet to provide the puff prot of lift downwards, the steering mechanism for being able to drive partition rotation to change jet direction is additionally provided in toroidal cavity.Aircraft of the invention, simple and compact for structure, flying power is powerful, has a smooth flight reliable, manipulation is simple and convenient, and cruising ability is strong；Aircraft use simultaneously is safer, meets the use needs of underage child.
Description
Technical field
The present invention relates to a kind of remotely pilotless aircraft, more specifically to a kind of no rotor remotely-piloted vehicle, especially
It is related to the Miniature remote control toy aircraft for being suitble to children to use.
Background technique
Referred to as " unmanned plane (Unmanned Aerial Vehicle) ", english abbreviation is " UAV " to UAV, is
Using the not manned aircraft of radio robot and the presetting apparatus provided for oneself manipulation, or fully by car-mounted computer
Or it intermittently automatically operates.
Currently, aircraft huge number in the market, and mostly multi-rotor aerocraft, it is mainly directed towards in adult, is grasping
Control property aspect be excellent in, and do not need runway can VTOL, can hover in the sky after taking off, meanwhile, in reliability
Aspect, more rotors are also that performance is most outstanding.Existing more rotary wind type unmanned plane noises are big, proprotor drop resistant performance
Difference awing encounters sundries, branch etc. and may directly contribute propeller and scraps, and has that energy consumption is high, cruise duration is shorter
The problems such as.Furthermore, it is contemplated that security hidden trouble, almost without the remotely-piloted vehicle for being directed to underage child design, more rotors
Aircraft is for children, and children easy to cut, there are certain danger coefficients, therefore causes unmanned plane in underage child city
Blank on field.
In view of the above-mentioned problems, China Patent No. ZL201520627047.0, authorized announcement date is on December 30th, 2015, hair
Bright creation title are as follows: irrotationality wing formula Multi-axis aircraft, this application are related to a kind of no rotary wind type Multi-axis aircraft, including installation is put down
Platform and multiple lift-jet devices, multiple lift-jet devices are in horizontal or non-horizontal opposed be mounted on mounting platform；Lift
Air-jet device includes total air-breathing supercharging device, annular air outlet device, transmission air hose, power drive unit and impeller and air inlet dress
It sets, the both ends for transmitting air hose are connect with total air-breathing supercharging device and annular air outlet device respectively；Total air-breathing supercharging device in 90 ° to
It is upper or in 90 ° downwards or counterpart is mounted on mounting platform, power drive unit is connected to transmission air hose connection mounting platform
End, impeller and inlet duct are connect with power drive unit；Annular air outlet device is equipped with round wind outlet, round wind outlet
Side is equipped with air loop duct opening air port.The aircraft of this application eliminates traditional unmanned plane rotation using no rotary wind type structure
Wing structure there are the shortcomings that.In this application, multiple annular air outlet devices are connected by transmission air hose in mounting platform setting,
Air is transported to annular air outlet device by transmission air hose to realize that jet lift acts on using total air-breathing supercharging device, and is led to
It crosses and controls angle of annular exhaust apparatus etc. to realize the functions such as hovering steering.But the aircraft of this application still remain with
Lower defect:
The first, its conveying that compressed air is realized by transmission air hose, one facilitates that there are certain energy losses, to flight
There is adverse effect in the continuation of the journey of device, another convenience transmits air hose as connecting rod, is main forced section in flight course
Part, thus it is more demanding to its material, enough intensity was both required, requiring has lighter weight, to increase
The manufacturing cost of aircraft；
Second, the angle of annular exhaust apparatus is controlled to realize the movements such as aircraft rotation by transfer, and control
Annular air outlet device processed is rotated to change air outlet angle and also need to carry out turning joint connection to annular air outlet device, is turned to
The setting of device increases the structural complexity of aircraft, and to the stability of aircraft, there are larger impacts；
Third, total air-breathing supercharging device are realized supercharging air using power drive unit driving impeller, are flown for being remotely controlled
For row device, jet stability is vital, and the rare key occurred whether there is or not rotary wind type jet unmanned plane is former on the market
Because being, the jet lift stability of no rotary wind type jet unmanned plane compared with multi-rotor unmanned aerial vehicle compared to there are larger gaps, therefore
It is further improved for the supercharging air uniformity and stability of no rotary wind type jet unmanned plane.
Summary of the invention
1. technical problems to be solved by the inivention
It is an object of the invention to overcome existing no rotary aircraft above shortcomings, it is distant to provide a kind of no rotor
Control aircraft, using technical solution of the present invention, using turbo-blower structure into annular air blast cavity mutually independent region
Air is inside blasted, flight lift is provided by the downward jet of ring jet mouth being arranged on annular air blast cavity, passes through change
The jet amount of each turbo-blower structure aircraft lifting, hovering and the movement such as can be moved forward and backward, and utilize annular air blast chamber
The partition of change jet direction can be rotated in vivo to control the spinning movement of aircraft, not only the structure of aircraft is simply tight
It gathers, and aircraft flight gesture stability is easily facilitated using the jet structure setting, have a smooth flight reliable, manipulate simple side
Just；Also, more powerful flying power and jet stability are provided using the turbo-blower structure of optimization design, is improved
The cruising ability of aircraft；The round and smooth no sharp component of aircraft appearance and rotor simultaneously, use is safer, meets low age
The use of children needs.
2. technical solution
In order to achieve the above objectives, technical solution provided by the invention are as follows:
A kind of no rotor remotely-piloted vehicle of the invention, including annular air blast cavity, turbo-blower structure and warehouse, it is described
Warehouse be fixed on the centre of annular air blast cavity, toroidal cavity is equipped in the annular air blast cavity, the annular is empty
Intracavitary to be equipped at least three groups partitions that toroidal cavity equal part is isolated into mutually indepedent region, each of described toroidal cavity is only
The middle part in vertical region is accordingly uniformly arranged one group for blasting into toroidal cavity on the lateral wall of annular air blast cavity
The turbo-blower structure of air-flow, the annular air blast cavity, which is equipped with a circle, jet to provide the jet of lift downwards
Mouthful, the steering mechanism for being able to drive partition rotation to change jet direction is additionally provided in the toroidal cavity.
Further, form what Open Side Down between the lateral wall of the warehouse and the inner sidewall of annular air blast cavity
Ring jet channel, the ring jet channel are connected with puff prot.
Further, the inner sidewall of the annular air blast cavity is cone structure, and the inside of annular air blast cavity
Wall is lesser opening up, and the opening of annular air blast cavity upward is fixedly connected with the lateral wall of warehouse, annular air blast cavity
Inner sidewall it is biggish opening down, and to form ring jet logical for the lateral wall of annular air blast cavity opening directed downwardly and warehouse
Road, the puff prot are set to the opening of annular air blast cavity upward.
Further, the warehouse is spherical structure.
Further, the steering mechanism is steering engine.
Further, the isolation that the turbo-blower structure includes air blast shell and is sequentially arranged in air blast shell
Pedestal, infundibulate turbine, motor fixing seat, motor, fairing cap and pod, the motor are installed in motor fixing seat,
The fairing cap is fixedly connected with motor fixing seat, and motor is fixed between fairing cap and motor fixing seat, the electricity
The rotary shaft of machine stretches out motor fixing seat and is connected with infundibulate turbine, and the motor fixing seat is equipped with and infundibulate whirlpool
The male cone (strobilus masculinus) structure of the inner conical surface clearance fit of wheel, the isolated base is equipped with matches with the male cone (strobilus masculinus) gap of infundibulate turbine
The inner conical surface structure of conjunction, and the middle part of isolated base is equipped with and is accordingly open with the air entry on air blast shell, the water conservancy diversion
It covers on fairing cap, and forms gas guiding channel between the two.
Further, the periphery of the motor fixing seat is equipped with ventilation corresponding with the air outlet of infundibulate turbine
Grid is equipped at intervals with several diversion fan blades on the fairing cap, and it is logical that adjacent diversion fan blade and pod surround gas flow guiding
Road, and each gas guiding channel is corresponding with ventilation grid.
Further, heat release hole is additionally provided between two neighboring diversion fan blade on the fairing cap.
Further, locating slot corresponding with above-mentioned diversion fan blade position is additionally provided on the inside of the pod.
Further, the periphery of the pod, motor fixing seat and isolated base three connects by the way that screw is fixed
It connects, and the gland by being pressed on pod is fixed in air blast shell.
3. beneficial effect
Using technical solution provided by the invention, compared with existing well-known technique, there is following remarkable result:
(1) a kind of no rotor remotely-piloted vehicle of the invention utilizes turbo-blower structure phase into annular air blast cavity
Air is blasted in mutual independent region, flight is provided by the downward jet of ring jet mouth being arranged on annular air blast cavity and is risen
Power, the jet amount by changing each turbo-blower structure aircraft lifting, hovering and the movement such as can be moved forward and backward, and utilize
It can be rotated in annular air blast cavity and change the partition of jet direction to control the spinning movement of aircraft, not only the knot of aircraft
Structure is simple and compact, and easily facilitates aircraft flight gesture stability using the jet structure setting, has a smooth flight reliable, manipulation
It is simple and convenient；
(2) a kind of no rotor remotely-piloted vehicle of the invention, the inner sidewall of the lateral wall of warehouse and annular air blast cavity
Between form the ring jet channel that Open Side Down, using ring jet channel make aircraft flight lift act on it is more uniform
Steadily, it to improve the flight stability of aircraft, more easily manipulates；Also, the jet being connected to ring jet channel
Mouthful be set to the opening of annular air blast cavity upward, this way it is ensured that the wind pressure that provides of turbo-blower structure by puff prot and
It is distributed more uniform behind the jet path in ring jet channel, jet direction is more stable, reduces air turbulence and bring
Unstability；
(3) a kind of no rotor remotely-piloted vehicle of the invention, warehouse use spherical structure, the annular of cooperation periphery setting
The monnolithic case of air blast cavity, aircraft is similar to science fiction flying saucer, improves visual effect, stronger both views are brought to people
Sense, excites the interest of child；Also, the round and smooth no sharp component of aircraft appearance and rotor, use is safer, meets low
The use of age children needs；
(4) a kind of no rotor remotely-piloted vehicle of the invention, steering mechanism use steering engine, and compact structure is light, is convenient for
Installation, control is accurate convenient, convenient for manipulation；
(5) a kind of no rotor remotely-piloted vehicle of the invention, turbo-blower structure is using air blast shell and successively sets
It is formed in isolated base, infundibulate turbine, motor fixing seat, motor, fairing cap and the pod etc. in air blast shell, motor is solid
Reservation is equipped with the male cone (strobilus masculinus) structure with the inner conical surface clearance fit of infundibulate turbine, and isolated base is equipped with and infundibulate turbine
Male cone (strobilus masculinus) clearance fit inner conical surface structure, infundibulate turbine is gap-matched inside turbo-blower structure, substantially mentions
The high supercharging effect of turbine, improves blowing efficiency, and then improve the flying power and stability of aircraft, reduces electricity
The energy loss of machine improves the cruising ability of aircraft；
(6) a kind of no rotor remotely-piloted vehicle of the invention, the interior gas constituted equipped with diversion fan blade of turbo-blower structure
Body flow-guiding channel, the gas for blasting turbo-blower structure in annular air blast cavity is more steady, further improves aircraft
Flight stability；
(7) a kind of no rotor remotely-piloted vehicle of the invention, on fairing cap between two neighboring diversion fan blade also
Equipped with heat release hole, the fever of motor can quickly be taken away using heat release hole, reduce the operating temperature of motor, to improve electricity
The service life of machine；
(8) a kind of no rotor remotely-piloted vehicle of the invention, all parts in turbo-blower structure are easy to assembly, lead to
Screw connection is crossed, and turbo-blower structure is easy for installation on annular air blast cavity, convenient for production.
Detailed description of the invention
Fig. 1 is a kind of schematic perspective view of no rotor remotely-piloted vehicle of the invention；
Fig. 2 is a kind of perspective structure schematic diagram of no rotor remotely-piloted vehicle of the invention；
Fig. 3 is the schematic cross-sectional view in the direction A-A in Fig. 1；
Fig. 4 is the fractionation structural representation of one group of turbo-blower structure in a kind of no rotor remotely-piloted vehicle of the invention
Figure；
Fig. 5 is the configuration schematic diagram of the turbo-blower structure in the present invention；
Fig. 6 is the attachment structure schematic diagram of the motor fixing seat and fairing cap in the present invention.
Label declaration in schematic diagram:
100, annular air blast cavity；101, partition；102, steering mechanism；103, toroidal cavity；104, puff prot；105, ring
Shape jet channel；200, turbo-blower structure；201, air blast shell；202, isolated base；203, infundibulate turbine；204, electric
Machine fixing seat；204a, ventilation grid；205, motor；206, fairing cap；206a, diversion fan blade；206b, heat release hole；207, water conservancy diversion
Cover；207a, locating slot；208, gland；300, warehouse.
Specific embodiment
To further appreciate that the contents of the present invention, the present invention is described in detail in conjunction with the accompanying drawings and embodiments.
Embodiment
In conjunction with shown in Fig. 1, Fig. 2 and Fig. 3, a kind of no rotor remotely-piloted vehicle of the present embodiment, including annular air blast cavity
100, turbo-blower structure 200 and warehouse 300, warehouse 300 are fixed on the centre of annular air blast cavity 100, can pacify in warehouse 300
The components such as controller, power supply and the indicator light of aircraft are filled, 300 bottom of warehouse may also set up floor stand and camera installation branch
The components such as frame；It is equipped with toroidal cavity 103 in annular air blast cavity 100, at least three groups are equipped in toroidal cavity 103 by toroidal cavity
103 equal parts are isolated into the partition 101 in mutually indepedent region, use three pieces of partitions 101 by 103 equal part of toroidal cavity as shown in Figure 2
For three groups of isolated areas, the middle part of each isolated area of toroidal cavity 103 is accordingly in the outside of annular air blast cavity 100
One group is uniformly arranged on wall for blasting the turbo-blower structure 200 of air-flow, annular air blast cavity 100 into toroidal cavity 103
Being equipped with a circle jet can provide the puff prot 104 of lift downwards, after turbo-blower structure 200 draws air into and is pressurized
It in the isolated area for blasting corresponding toroidal cavity 103, is then sprayed downwards by the puff prot 104 of annular, forms reversed make
Firmly, to provide the lift of aircraft；It is additionally provided in toroidal cavity 103 and is able to drive the rotation of partition 101 to change jet side
To steering mechanism 102, the i.e. changeable jet direction of the rotation of partition 101 is controlled by steering mechanism 102, formation is tangential on annular
The active force of air blast cavity 100, so as to control aircraft spinning movement.Using the above structure, turbo-blower structure is utilized
200 blast air in mutually independent region into annular air blast cavity 100, pass through the ring being arranged on annular air blast cavity 100
Shape puff prot 104 downward jet provides flight lift, and the jet amount by changing each turbo-blower structure 200 can fly
The movements such as device lifting, hovering and back-and-forth motion, and utilize the partition that change jet direction can be rotated in annular air blast cavity 100
101 control the spinning movement of aircraft, and not only aircraft is simple and compact for structure, but also more using the jet structure setting
Convenient for aircraft flight gesture stability, has a smooth flight reliable, manipulate simple and convenient.
It is shown in Figure 3, in the present embodiment, between the lateral wall of warehouse 300 and the inner sidewall of annular air blast cavity 100
The ring jet channel 105 that Open Side Down is formed, which is connected with puff prot 104, utilizes ring jet
It is more uniform steady that channel 105 acts on the flight lift of aircraft, to improve the flight stability of aircraft, more easily
In manipulation.Specifically, the inner sidewall of annular air blast cavity 100 is cone structure, in horn-like, and annular air blast cavity 100
Inner sidewall is lesser opening up, and the opening of annular air blast cavity 100 upward is fixedly connected with the lateral wall of warehouse 300, ring
The inner sidewall of shape air blast cavity 100 is biggish opening down, and the opening directed downwardly of annular air blast cavity 100 and warehouse 300 is outer
Side wall forms ring jet channel 105, and puff prot 104 is set to the opening of annular air blast cavity 100 upward, this way it is ensured that
The wind pressure that turbo-blower structure 200 provides behind the jet path in puff prot 104 and ring jet channel 105 by being distributed more
Even, jet direction is more stable, reduces air turbulence and bring unstability.In addition, warehouse 300 is spherical structure, ring
Shape air blast cavity 100 is partial to the top setting of warehouse 300, keeps the center of gravity of aircraft integrally on the lower side, in this way, passing through ring jet
The effect of channel 105 and 300 lower part outer wall of warehouse keeps the gas sprayed vertically downward substantially, and the anti-work of the gas sprayed
It firmly can preferably act on the outer wall of warehouse 300, further ensure the flight stability of aircraft；Meanwhile it using
The monnolithic case of the warehouse 300 of spherical structure, the annular air blast cavity 100 of cooperation periphery setting, aircraft flies similar to science fiction
Dish improves visual effect, and stronger both visual senses are brought to people, excite the interest of child；Also, aircraft appearance circle
It slides without sharp component and rotor, use is safer, meets the use needs of underage child.In the present embodiment, turning machine
Structure 102 is preferably steering engine, and compact structure is light, is easily installed, and control is accurate convenient, convenient for manipulation.
In conjunction with shown in Fig. 4, Fig. 5 and Fig. 6, in the present embodiment, turbo-blower structure 200 include air blast shell 201 and
Isolated base 202, infundibulate turbine 203, motor fixing seat 204, the motor 205, fairing cap being sequentially arranged in air blast shell 201
206 and pod 207, air blast shell 201 is equipped with air entry, and motor 205 is installed in motor fixing seat 204, fairing cap 206
It is fixedly connected with motor fixing seat 204, motor 205 is fixed between fairing cap 206 and motor fixing seat 204, fairing cap 206
Connect with motor fixing seat 204 using screw, the rotary shaft stretching motor fixing seat 204 of motor 205 and with infundibulate whirlpool
Wheel 203 is connected, and motor fixing seat 204 is equipped with the male cone (strobilus masculinus) structure with the inner conical surface clearance fit of infundibulate turbine 203, every
It is equipped with the inner conical surface structure with the male cone (strobilus masculinus) clearance fit of infundibulate turbine 203 from pedestal 202, and in isolated base 202
Portion is equipped with and is accordingly open with the air entry on air blast shell 201, in this way, not by the pressurized air of infundibulate turbine 203
Disorder air-flow being generated in the interior male cone (strobilus masculinus) of infundibulate turbine 203 and causing energy loss, the pressurization effect of turbine greatly improved
Fruit improves blowing efficiency, and then improves the flying power and stability of aircraft, reduces the energy loss of motor, mentions
The high cruising ability of aircraft.Pod 207 covers on fairing cap 206, and forms gas guiding channel between the two, tool
Body, the periphery of motor fixing seat 204 is equipped with ventilation grid 204a corresponding with the air outlet of infundibulate turbine 203, water conservancy diversion
Several diversion fan blade 206a are equipped at intervals on lid 206, it is logical that adjacent diversion fan blade 206a and pod 207 surround gas flow guiding
Road, and each gas guiding channel is corresponding with ventilation grid 204a, and turbo-blower structure 200 is made to blast annular air blast cavity
Gas in 100 is more steady, further improves the flight stability of aircraft.For the ease of pod 207 and fairing cap
206 location fits are additionally provided with locating slot 207a corresponding with the position above-mentioned diversion fan blade 206a in the inside of pod 207,
The assembly of pod 207 Yu fairing cap 206 is easily facilitated, convenient for the formation of gas guiding channel.In addition, on fairing cap 206
It is additionally provided with heat release hole 206b between two neighboring diversion fan blade 206a, when pressurized air is quick from gas guiding channel
When flowing, the heat that motor 205 generates can be extracted out from heat release hole 206b, and quickly be taken away, and reduce the work of motor 205
Temperature, to improve the service life of motor 205.In addition, pod 207, motor fixing seat 204 and isolated base 202 3
The periphery of person is fixedly connected by screw, and the gland 208 by being pressed on pod 207 is fixed in air blast shell 201, tool
When body assembles, motor fixing seat 204, motor 205 and 206 three of fairing cap first can be become into an entirety by screw group, so
Afterwards by the rotation axis connection of infundibulate turbine 203 and motor 205, later by isolated base 202, motor fixing seat 204 and water conservancy diversion
The periphery for covering 207 threes is connected by screw to, and subsequently the overall structure after connection is mounted in air blast shell 201, is passed through
Gland 208 compresses it, and is fixedly connected with gland 208 with air blast shell 201 using screw；Finally, by turbo-blower structure
200 integral installations are on annular air blast cavity 100.All parts in turbo-blower structure 200 are easy to assembly, pass through
Screw connection, and turbo-blower structure 200 is easy for installation on annular air blast cavity 100, convenient for production.
Referring to figure 1 and figure 2, in embodiment, turbo-blower structure 200 is uniformly set on annular air blast cavity 100
There are three groups, certainly, according to specific needs, turbo-blower structure 200 may also set up three groups or more on annular air blast cavity 100.
A kind of no rotor remotely-piloted vehicle of the present embodiment, cooperation remote-control handle can carry out flight manipulation.Turbine air blast
After mechanism 200 starts, air is sucked from side, is blasted after pressurization in annular air blast cavity 100, the air blasted is in annular
Divided by partition 101 for three regions in cavity 103, does not interfere with each other, spray downwards, formed via an internal circle puff prot 104
Reaction force, so that aircraft be made to rise；It is when the air output of each group turbo-blower structure 200 changed simultaneously, i.e., changeable
The size of reaction force completes lifting action, also can control aircraft hovering；When by changing a certain group of turbo-blower structure
200 revolving speed increases some region of jet amount, is tilted a certain angle body, keeps stablizing, forward or backward can be completed
Movement；When the direction that the angle for changing partition 101 by steering engine, i.e., changeable air-flow spray, the effect for being tangential on annulus is formed
Power completes spinning movement.
A kind of no rotor remotely-piloted vehicle of the invention, it is mutually indepedent into annular air blast cavity using turbo-blower structure
Region in blast air, provide flight lift by the downward jet of ring jet mouth being arranged on annular air blast cavity, lead to
Cross change each turbo-blower structure jet amount can aircraft lifting, hovering and be moved forward and backward etc. movement, and using annular
The partition of change jet direction can be rotated in air blast cavity to control the spinning movement of aircraft, not only the structure of aircraft is simple
It is single compact, and aircraft flight gesture stability is easily facilitated using the jet structure setting, it has a smooth flight reliable, manipulation is simple
It is convenient；Also, more powerful flying power and jet stability are provided using the turbo-blower structure of optimization design, is mentioned
The high cruising ability of aircraft；The round and smooth no sharp component of aircraft appearance and rotor simultaneously, use is safer, meets low
The use of age children needs.
Schematically the present invention and embodiments thereof are described above, description is not limiting, institute in attached drawing
What is shown is also one of embodiments of the present invention, and actual structure is not limited to this.So if the common skill of this field
Art personnel are enlightened by it, without departing from the spirit of the invention, without creatively designing and the technical solution
Similar frame mode and embodiment, are within the scope of protection of the invention.
Claims (9)
1. a kind of no rotor remotely-piloted vehicle, it is characterised in that: including annular air blast cavity (100), turbo-blower structure (200)
With warehouse (300), the warehouse (300) is fixed on the centre of annular air blast cavity (100), the annular air blast cavity
(100) toroidal cavity (103) are equipped in, at least three groups are equipped in the toroidal cavity (103) by toroidal cavity (103) equal part
It is isolated into the partition (101) in mutually indepedent region, the middle part of each isolated area of the toroidal cavity (103) is accordingly
One group is uniformly arranged on the lateral wall of annular air blast cavity (100) for blasting the turbine of air-flow into toroidal cavity (103)
Blast mechanism (200), the annular air blast cavity (100), which is equipped with a circle, jet to provide the puff prot of lift downwards
(104), the turning machine for being able to drive partition (101) rotation to change jet direction is additionally provided in the toroidal cavity (103)
Structure (102)；
The isolation that the turbo-blower structure (200) includes air blast shell (201) and is sequentially arranged in air blast shell (201)
Pedestal (202), infundibulate turbine (203), motor fixing seat (204), motor (205), fairing cap (206) and pod (207),
The motor (205) is installed in motor fixing seat (204), and the fairing cap (206) and motor fixing seat (204) are fixed
Connection, motor (205) is fixed between fairing cap (206) and motor fixing seat (204), the rotation of the motor (205)
Axis stretch out motor fixing seat (204) simultaneously be connected with infundibulate turbine (203), the motor fixing seat (204) be equipped with
The male cone (strobilus masculinus) structure of the inner conical surface clearance fit of infundibulate turbine (203), the isolated base (202) is equipped with and infundibulate
The inner conical surface structure of the male cone (strobilus masculinus) clearance fit of turbine (203), and the middle part of isolated base (202) is equipped with and air blast shell
(201) air entry on is accordingly open, and the pod (207) covers on fairing cap (206), and is formed between the two
Gas guiding channel.
2. a kind of no rotor remotely-piloted vehicle according to claim 1, it is characterised in that: outside the warehouse (300)
The ring jet channel (105) that Open Side Down, the ring jet are formed between side wall and the inner sidewall of annular air blast cavity (100)
Channel (105) is connected with puff prot (104).
3. a kind of no rotor remotely-piloted vehicle according to claim 2, it is characterised in that: the annular air blast cavity
(100) inner sidewall is cone structure, and the inner sidewall of annular air blast cavity (100) is lesser opening up, and annular air blast
The opening of cavity (100) upward is fixedly connected with the lateral wall of warehouse (300), and the inner sidewall of annular air blast cavity (100) is larger
It is opening down, and annular air blast cavity (100) opening directed downwardly and the lateral wall of warehouse (300) form ring jet channel
(105), the puff prot (104) is set to the opening of annular air blast cavity (100) upward.
4. a kind of no rotor remotely-piloted vehicle according to claim 3, it is characterised in that: the warehouse (300) is ball
Shape structure.
5. a kind of no rotor remotely-piloted vehicle according to claim 1, it is characterised in that: the steering mechanism (102)
For steering engine.
6. according to claim 1 to a kind of no rotor remotely-piloted vehicle described in 5 any one, it is characterised in that: the electricity
The periphery of machine fixing seat (204) is equipped with ventilation grid (204a) corresponding with the air outlet of infundibulate turbine (203), described
It is equipped at intervals on fairing cap (206) several diversion fan blades (206a), adjacent diversion fan blade (206a) is surrounded with pod (207)
Gas guiding channel, and each gas guiding channel is corresponding with ventilation grid (204a).
7. a kind of no rotor remotely-piloted vehicle according to claim 6, it is characterised in that: on the fairing cap (206)
Heat release hole (206b) is additionally provided between two neighboring diversion fan blade (206a).
8. a kind of no rotor remotely-piloted vehicle according to claim 7, it is characterised in that: the pod (207)
Inside is additionally provided with locating slot (207a) corresponding with the above-mentioned diversion fan blade position (206a).
9. a kind of no rotor remotely-piloted vehicle according to claim 8, it is characterised in that: the pod (207), electricity
Machine fixing seat (204) is fixedly connected with the periphery of isolated base (202) three by screw, and by being pressed in pod (207)
On gland (208) be fixed in air blast shell (201).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710599541.4A CN107323668B (en) | 2017-07-21 | 2017-07-21 | A kind of no rotor remotely-piloted vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710599541.4A CN107323668B (en) | 2017-07-21 | 2017-07-21 | A kind of no rotor remotely-piloted vehicle |
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| CN107323668A CN107323668A (en) | 2017-11-07 |
| CN107323668B true CN107323668B (en) | 2019-11-01 |
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| CN107985555A (en) * | 2017-11-13 | 2018-05-04 | 上海顺砾智能科技有限公司 | One kind is without the mute unmanned plane of wing formula |
| CN113184200B (en) * | 2021-06-10 | 2024-08-20 | 江苏航空职业技术学院 | Structure of unmanned aerial vehicle without rotary wing |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4979363A (en) * | 1984-11-17 | 1990-12-25 | Rolls-Royce Plc | Diverter valve with bypass duct obturator |
| CN1424234A (en) * | 2003-01-15 | 2003-06-18 | 肖立峰 | Cyclone jet aircraft |
| CN1480376A (en) * | 2003-07-16 | 2004-03-10 | 肖立峰 | Umbrella wings shaped jet aerocraft |
| CN206107556U (en) * | 2016-08-29 | 2017-04-19 | 高新卫 | High -speed type dish -shaped aircraft |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US9550566B2 (en) * | 2015-05-27 | 2017-01-24 | John Francis Henning, JR. | Disc-shaped turbo-jet aircraft |
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Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4979363A (en) * | 1984-11-17 | 1990-12-25 | Rolls-Royce Plc | Diverter valve with bypass duct obturator |
| CN1424234A (en) * | 2003-01-15 | 2003-06-18 | 肖立峰 | Cyclone jet aircraft |
| CN1480376A (en) * | 2003-07-16 | 2004-03-10 | 肖立峰 | Umbrella wings shaped jet aerocraft |
| CN206107556U (en) * | 2016-08-29 | 2017-04-19 | 高新卫 | High -speed type dish -shaped aircraft |
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