CN107512390A - A kind of disc-shaped unmanned machine - Google Patents
A kind of disc-shaped unmanned machine Download PDFInfo
- Publication number
- CN107512390A CN107512390A CN201710725565.XA CN201710725565A CN107512390A CN 107512390 A CN107512390 A CN 107512390A CN 201710725565 A CN201710725565 A CN 201710725565A CN 107512390 A CN107512390 A CN 107512390A
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- Prior art keywords
- main part
- foot stool
- horn
- disc
- cover portion
- Prior art date
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- 238000009434 installation Methods 0.000 claims description 25
- 238000003780 insertion Methods 0.000 claims description 13
- 230000037431 insertion Effects 0.000 claims description 13
- 241000883966 Astrophytum capricorne Species 0.000 claims description 3
- 230000002093 peripheral effect Effects 0.000 claims description 3
- 238000005096 rolling process Methods 0.000 claims description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 8
- 230000005484 gravity Effects 0.000 description 6
- 238000012856 packing Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 238000001727 in vivo Methods 0.000 description 3
- 238000005259 measurement Methods 0.000 description 3
- 230000000630 rising effect Effects 0.000 description 3
- 238000001514 detection method Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- CVOFKRWYWCSDMA-UHFFFAOYSA-N 2-chloro-n-(2,6-diethylphenyl)-n-(methoxymethyl)acetamide;2,6-dinitro-n,n-dipropyl-4-(trifluoromethyl)aniline Chemical compound CCC1=CC=CC(CC)=C1N(COC)C(=O)CCl.CCCN(CCC)C1=C([N+]([O-])=O)C=C(C(F)(F)F)C=C1[N+]([O-])=O CVOFKRWYWCSDMA-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- 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; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of disc-shaped unmanned machine, it is characterised in that including：Dish-shaped primary structural component, it has the main part for forming dish-shaped periphery, and the engine department for protruding from main part at dish middle part is formed positioned at main part side；Positioned at main part opposite side, the cover portion for the cabin for protruding from main part is installed；The main part periphery has certain thickness, and periphery edge is uniformly distributed at least three horns for being provided with and flexing outward, and horn end is equipped with the blade and motor as power；Foot stool installing structure is provided with the engine department and the cover portion, the engine department and the cover portion select one bottom as unmanned plane, removably in installing foot stool on foot stool installing structure.By upper, the application is advantageous to user and sets thrust paddle or pulling force oar in same unmanned plane according to the voluntarily selection of different use demands.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, and in particular to a kind of disc-shaped unmanned machine.
Background technology
Unmanned plane is air-robot, the mankind can be replaced to complete aerial work, and can form aerial platform, with reference to
Miscellaneous part expands application.At present, unmanned plane take photo by plane and entertain, agricultural, security protection, the field such as electric power have shown wide hair
Exhibition prospect.
In the prior art, propeller is merely able to direction selection one is arranged on unmanned plane upward or down.That is, when
The unmanned plane for selecting propeller to install upward when user needs to be provided with the unmanned plane of pulling force oar；When user needs to be provided with thrust
It need to be selected else during the unmanned plane of oar and select the unmanned plane that propeller is installed upward；As can be seen here, prior art, it is different to be unfavorable for user
The voluntarily selection of use demand is provided with thrust paddle or pulling force oar in same unmanned plane, easily causes the inconvenient for use of unmanned plane and holds
Easily cause the waste of resource.
Therefore, need badly at present and a kind of be advantageous to user and set according to the voluntarily selection of different use demands in same unmanned plane
Put the unmanned plane of thrust paddle or pulling force oar.
The content of the invention
In view of this, the application provides a kind of disc-shaped unmanned machine, is advantageous to user according to different use demands voluntarily
Selection sets thrust paddle or pulling force oar in same unmanned plane.
The application provides a kind of disc-shaped unmanned machine, including：
Dish-shaped primary structural component, it has the main part for forming dish-shaped periphery, and dish middle part is formed positioned at main part side
Protrude from the engine department of main part；
Positioned at main part opposite side, the cover portion for the cabin for protruding from main part is installed；
The main part periphery has certain thickness, and periphery edge is uniformly distributed at least three machines for being provided with and flexing outward
Arm, horn end are equipped with the blade and motor as power；
Foot stool installing structure is provided with the engine department and the cover portion, the engine department and the cover portion select one work
For the bottom of unmanned plane, removably in installing foot stool on foot stool installing structure.
By upper, the disc-shaped unmanned machine of the application on engine department and the cover portion by being provided with foot stool installing structure, institute
State engine department and the cover portion select one the bottom as unmanned plane, removably in installing foot stool on foot stool installing structure.Have
Voluntarily selection beneficial to the different use demand of user is provided with thrust paddle or pulling force oar on same unmanned plane, facilitates unmanned plane
Use, and be advantageous to economize on resources.
Preferably, the foot stool installing structure includes：It is arranged on the surface of the engine department and the cover portion, inwardly prolongs
At least three hole slots stretched, and the direction convergence that extends internally；
The foot stool, which corresponds to the mounting structure, has the insertion end that can be inserted into the hole slot.
Preferably, the hole slot and the insertion end is engages or thread fiting mode assembling.
By upper, the fast assembling-disassembling of foot stool is advantageously implemented.Wherein, the foot stool can also take folded form, i.e. carry
When, it is not necessary to dismantle, need to only be folded.
Preferably, the inner fovea part that described horn one end is stretched into the body peripheral edge, and horizontally rotate with main body and be connected；It is logical
Cross a fixture and horn is fixed on certain turned position；
The main part is peripherally provided with the groove with horn form fit by the inner fovea part, and the notch end is corresponding
Main part has the recess that match with the motor, is respectively used to house and horizontally rotates the horn and electricity to the groove
Machine.
By upper, the application can realize is arranged in unmanned plane primary structural component by horn along after the rotation of horn rotary shaft
In the groove for being used to house the horn after rotary folding that the one of upper setting matches with the horn, so as to be advantageous to convenient pair
The loading packing of unmanned plane and carrying.
Preferably, inner fovea part described in main part has the vertical axle of horn one end described in rolling assembling, the fixture
For the vertical goat's horn bolt detachably installed.
By upper, the application, can be spacing to the rotating range of the horn and to rotary folding by setting positioning limiting fixator
The horn afterwards is fixed.
Preferably, the engine department or/and the cover portion have hand-held through hole close to outer circumference.
By upper, user can be carried out by the through hole set in the unmanned plane shell or the groove to the unmanned plane
It is hand-held to carry.
Preferably, there is outwardly external components installation portion at the engine department or/and the cover portion center.
By upper, the external components installation portion is advantageous to the external components such as accommodating camera, battery.
Preferably, the external components installation portion is provided with camera.
By upper, be advantageous to be taken photo by plane during unmanned plane during flying.User also may be used when selecting pulling force oar or thrust paddle to install
According to different application and scene, load (camera) mounting means is selected, that is, is installed on engine department or/and the cover
Portion, i.e., the external components installation portion for being both mountable to back are also mountable to the external components installation portion (pin of underbelly
The side of frame installation), in general, installed in underbelly installation portion position, application is wider, is suitable for various in height
Idle job, ground installation equipment and personnel etc. are looked down, but under special circumstances, for example similar detection checks tunnel upper wall situation
When, load is just particularly important installed in top installation portion.User can according to oneself need be selectively mounted to engine department
Or/and the cover portion.
Preferably, the unmanned plane is in its horizontal section Central Symmetry.
By upper, unmanned plane is advantageous to improve the stability during unmanned plane during flying in its horizontal section Central Symmetry.Its
In, asymmetric design can also be selected as needed.
In summary, the disc-shaped unmanned machine of the application on engine department and the cover portion by being provided with foot stool installation knot
Structure, the engine department and the cover portion select one bottom as unmanned plane, removably in installation foot on foot stool installing structure
Frame.The voluntarily selection for being advantageous to the different use demand of user is provided with thrust paddle or pulling force oar on same unmanned plane, convenient
Unmanned plane is used, and is advantageous to economize on resources.Wherein, dried downwards using thrust paddle mounting means, propeller, lower section is inorganic
Arm blocks, and energy loss is few, can effectively lift the unmanned plane cruise time, and actual measurement cruising time probably lifts 10%-15%；Pulling force
Oar mounting means, machine gravity is relatively low, and oar plane is easier to operate to above center of gravity, during flight, and flight is more steady, and fuselage
Bottom free space is more, can in vivo dispose a greater variety of loads.And horn can be realized and revolve horn along horn
Rotating shaft rotation after be arranged in set on unmanned plane primary structural component one with the horn match be used for house rotary folding
In the groove of the horn of poststack, so as to be advantageous to the convenient loading packing to unmanned plane and carrying.Meanwhile the application passes through setting
Positioning limiting fixator, can be spacing to the rotating range of the horn and the horn after rotary folding be fixed.The application
Unmanned plane shell on be additionally provided with through hole or groove in order to be held to unmanned plane.Carry to carry and more facilitate.
Brief description of the drawings
Fig. 1 is the front view of disc-shaped unmanned machine (thrust paddle) structure that the embodiment of the present application provides；
Fig. 2 is the stereogram of disc-shaped unmanned machine (pulling force oar) structure that the embodiment of the present application provides；
Three-dimensional signal when Fig. 3 is disc-shaped unmanned machine (not installing foot stool) horn deployed condition that the embodiment of the present application provides
Figure；
Three-dimensional signal when Fig. 4 is disc-shaped unmanned machine (not installing foot stool) horn folded state that the embodiment of the present application provides
Figure；
Fig. 5 is the horn and the enlarged diagram of the junction of unmanned plane primary structural component that the embodiment of the present application provides；
Fig. 6 A are the decomposing schematic representation for the foot stool installing structure (thread fiting mode assembling) that the embodiment of the present application provides；
Fig. 6 B are the signal after the assembling for the foot stool installing structure (thread fiting mode assembling) that the embodiment of the present application provides
Figure；
Fig. 7 A are the decomposing schematic representation for the foot stool installing structure (snap-fit) that the embodiment of the present application provides；
Fig. 7 B are the schematic diagram after the assembling for the foot stool installing structure (snap-fit) that the embodiment of the present application provides；
Fig. 8 A are the top view of the interface arrangment for the foot stool installing structure (snap-fit) that the embodiment of the present application provides；
Fig. 8 B are the upward view of the interface arrangment for the foot stool installing structure (snap-fit) that the embodiment of the present application provides；
Fig. 8 C are the side view of the interface arrangment for the foot stool installing structure (snap-fit) that the embodiment of the present application provides.
Embodiment
Below in conjunction with the drawings and specific embodiments, the present invention is further illustrated.
As shown in figures 1-8, the disc-shaped unmanned machine that the application provides, including：Dish-shaped primary structural component, it, which has, forms dish week
The main part 10 on side, the engine department 20 for protruding from main part at dish middle part is formed positioned at main part side；It is another positioned at main part
Side, the cover portion 30 for the cabin for protruding from main part is installed；The main part periphery has a certain thickness, and periphery edge is uniform
Distributing installation has at least three horns 40 flexed outward, and horn end is equipped with the blade 50 and motor as power
60；Foot stool installing structure 70 is provided with the engine department and the cover portion, the engine department and the cover portion select one conduct
The bottom of unmanned plane, removably in installation foot stool 120 on foot stool installing structure.
Wherein, the foot stool 120 includes but is not limited to：Prop stand, parallel bars foot stool or annular foot stool；Wherein, the list
Foot stool, quantity are at least 30, and its one end is arranged on primary structural component or shell.
The parallel bars foot stool, including 4 prop stands and connected two cross bar；Wherein, one end of two adjacent prop stands
It is arranged on the primary structural component or shell, the other end as illustrated in figures 7 a-b, is hinged by ball head universal and a cross bar；
One end of another two adjacent prop stand is arranged on the primary structural component or shell, and the other end as illustrated in figures 7 a-b, passes through bulb
Universal joint is hinged with another cross bar.
The annular foot stool, including at least three prop stand and a connected annulus；Wherein, the one of the prop stand
End is arranged on the primary structural component or shell, and the other end as illustrated in figures 7 a-b, passes through ball head universal 130 and the circle
Ring is hinged.
Wherein, prop stand adapts to various landform, and parallel bars foot stool adapts to relatively flat landform, and stationarity when it lands is better than
Prop stand, annular foot stool adapt to level terrain, and stationarity when it lands is better than foregoing two kinds of foot stools.User can be according to specific
Need to be selected.
Wherein, the foot stool installing structure includes：It is arranged on the surface of the engine department and the cover portion, extends internally
At least three hole slots, and extend internally direction convergence；The foot stool, which corresponds to the mounting structure, has the pluggable hole slot
Insertion end.
Wherein, the hole slot and foot stool insertion end is engages or thread fiting mode assembling.Thus, it is advantageously implemented pin
The fast assembling-disassembling of frame.Wherein, when hole slot and foot stool insertion end are that thread fiting mode assembles, as shown in Fig. 6 A, 6B, wherein,
Fig. 6 A show the schematic diagram of foot stool installing structure and foot stool separated position.Wherein, Fig. 6 B show that foot stool is tied with foot stool installation
Schematic diagram after the connection of structure spiral.Wherein, the foot stool installing structure includes：One insertion end for being sheathed on the foot stool
Outer wall is provided with external screw thread, and the set 71 of through hole 711 is provided with wall, and one be assemblied in it is described be arranged at the engine department and
The one female helical structure 72 of setting coordinated with 71 screw threads of the set at the hole slot end on the surface of the cover portion；Its
In, internal thread is provided with the wall of the through hole 711 set on the set 71, by inserting the spiral shell matched with the size of through hole 711
Bolt is simultaneously tightened, and can closely be connected the foot stool for inserting the set 71 with the set 71.And further by it is described set 71 with it is described
Foot stool and the connection of unmanned plane engine department or cover portion can be achieved in the threaded connection of helical structure 72.
Wherein, when the hole slot and foot stool insertion end are snap-fit, as illustrated in figures 7 a-b, the foot stool installation knot
Structure includes：The interface arrangment 73 at the hole slot end of the engine department and the cover portion is assemblied in, is arranged at the foot stool insertion end
The projecting shaft 74 of both sides, wherein, the diameter that width and the projecting shaft 74 are provided with the wall of the interface arrangment 73 matches
Neck, wherein, the neck include insertion one end open rising part 731, horizontal component 732, fovea superior slot part 733
And recessed slot part 734.Wherein, the top that the attachment structure is fixed in an one end is provided with the interface arrangment 73
Spring 735.Wherein, stretched out outside the both sides of insertion end of the projecting shaft 74 towards foot stool, the projecting shaft can be through
The two side of the foot stool, it is respectively 2 to stretch to the quantity stretched out outside foot stool wall or be arranged on foot stool lateral wall
Shaft, the quantity of the neck correspond to 2.The engaging principle of the snap-in structure is：The foot stool for being provided with projecting shaft 74 is inserted
End, inserts the interface arrangment 73, wherein, the openend for the rising part 731 that the projecting shaft 74 passes through interface arrangment 73 is stretched
Enter the neck, and be moved to horizontal component 732 all the way up, (in the process, the insertion end of foot stool is by from spring
Elastic force), rotate the foot stool, make its projecting shaft 74 along the transverse shifting of horizontal component 732, finally spring elastic force work
The projecting shaft 74 is pressed on into the recessed slot part 734 with lower.To complete the clamping of foot stool and interface arrangment 73.Work as needs
When dismantling foot stool, foot stool is moved up, so that projecting shaft 74 is moved upward to the horizontal component 732, rotates the foot stool,
Its projecting shaft 74 is set to laterally move to rising part 731 along the horizontal component 732, further by projecting shaft 74 from riser portions
Divide 731 opening to stretch out to separate it with interface arrangment 73.By upper, by above-mentioned foot stool quick-disassembly structure, pin is advantageously implemented
Frame is rapidly assembled and disassembled.Wherein, the foot stool can also take folded form.That is, carrying when, it is not necessary to dismantle, only need by
It is folded.
Wherein, as in Figure 3-5, the inner fovea part that described horn one end is stretched into the body peripheral edge, and it is horizontal with main body
Rotation connection；Horn is fixed on by certain turned position by a fixture；The main part is peripherally set by the inner fovea part
There is the groove with horn form fit, the notch end, which corresponds to main part, has the recess matched with the motor, is respectively used to
It is accommodating to horizontally rotate the horn and motor to the groove.Thus, the application, which can realize, rotates horn along horn
Axle rotation after be arranged in set on unmanned plane primary structural component one with the horn match be used for house rotary folding
In the groove of horn afterwards, so as to be advantageous to the convenient loading packing to unmanned plane and carrying.
Wherein, inner fovea part described in main part has the vertical axle 80 of horn one end described in rolling assembling, the fixture
For the vertical goat's horn bolt 90 detachably installed.Thus, the application, can be to the rotation of the horn by setting positioning limiting fixator
It is spacing and the horn after rotary folding is fixed to turn scope.
Wherein, the engine department or/and the cover portion have to hold close to outer circumference uses through hole 100.Thus, Yong Huke
To carry out hand-held carrying to the unmanned plane by the through hole set in the unmanned plane shell or the groove.
Wherein, there is outwardly external components installation portion 110 at the engine department or/and the cover portion center.By
This, the external components installation portion is advantageous to the external components such as accommodating camera, battery.
Wherein, flight control system HY-01 or PLC are additionally provided with the engine department or/and the cover portion,
Other stronger flight control systems of business specific aim can also be selected according to customer requirement.Wherein, flight control system is installed
In disc-shaped unmanned machine integral central position.Battery is additionally provided with the engine department or/and the cover portion, battery passes through internal electricity
Road plate is powered to motor.
Wherein, as shown in Figure 1-2, the outwardly external components peace at the engine department or/and the cover portion center
Dress portion 11 is provided with camera.Thus, be advantageous to be taken photo by plane during unmanned plane during flying.
Wherein, the unmanned plane is its horizontal section Central Symmetry (also can non complete symmetry).Thus, be advantageous to improve nothing
Stability in man-machine flight course.
Wherein, the propeller includes：Propeller blade and propeller fixed cover；Wherein, the propeller blade
It is fixedly connected on the side of the propeller fixed cover；The propeller fixed cover is sheathed on institute by a propeller quick-disassembly structure
State on the output shaft of motor.
Wherein, the propeller quick-disassembly structure includes：
It is arranged at the buckle being connected by spring in the propeller fixed cover and with the propeller fixed cover inwall；Its
In, the output shaft of the motor is provided with the overhead kick being clasped with this.By above-mentioned propeller quick-disassembly structure, it is advantageously implemented
The fast assembling-disassembling of propeller.Wherein, propeller need not can also be dismantled, and directly it is folded by foldable structure.
Wherein, the disc-shaped unmanned machine, in addition to：Remote control, it is controlled with the flight control system HY-01 or PLC
Device wireless signal connection processed.By setting remote control to realize the Remote to disc-shaped unmanned machine.
For the technical scheme of further instruction the application, now the operation principle of the disc-shaped unmanned machine of the application is illustrated such as
Under：
Due to being provided with foot stool installing structure on the engine department and cover portion of the application.Because the propeller is towards main knot
The side of component is set.
As shown in figure 1, when the foot stool is arranged on the engine department, the propeller is arranged to thrust paddle；By distant
Flight control system HY-01 or PLC described in device remote control are controlled, and passes through flight control system HY-01 or PLC
The rotation of the output shaft of the further controlled motor of controller, the rotation of propeller is further driven by motor output shaft.With production
Raw upward thrust makes unmanned plane take off.Wherein, dried downwards using thrust paddle mounting means, propeller, lower section hides without horn
Gear, energy loss is few, can effectively lift the unmanned plane cruise time, and actual measurement cruising time probably lifts 10%-15%.
As shown in Fig. 2 when the foot stool is arranged in the cover portion, the propeller is arranged to pulling force oar.By being remotely controlled
Flight control system HY-01 or PLC described in device remote control, and controlled by flight control system HY-01 or PLC
The rotation of the output shaft of the further controlled motor of device processed, the rotation of propeller is further driven by motor output shaft.To produce
Upward pulling force makes unmanned plane take off.Pulling force oar mounting means, machine gravity is relatively low, and oar plane is above center of gravity, during flight more
Easily operation, flight is more steady, and underbelly free space is more, can in vivo dispose a greater variety of loads.
As shown in figure 4, when needing to pack unmanned plane or carry, the horn of unmanned plane is revolved along horn rotary shaft
One set on unmanned plane primary structural component is arranged in after turning with what the horn matched to be used for after housing rotary folding
In the groove of horn；Meanwhile the propeller of unmanned plane is dismantled or folded, foot stool is dismantled or folded, so as to be advantageous to
Convenient loading packing and carrying to unmanned plane.
In summary, the disc-shaped unmanned machine of application is on engine department and the cover portion by being provided with foot stool installing structure,
The engine department and the cover portion select one bottom as unmanned plane, removably in installing foot stool on foot stool installing structure.
The voluntarily selection for being advantageous to the different use demand of user is provided with thrust paddle or pulling force oar on same unmanned plane, convenient to nothing
Man-machine use, and be advantageous to economize on resources.Wherein, dried downwards using thrust paddle mounting means, propeller, lower section hides without horn
Gear, energy loss is few, can effectively lift the unmanned plane cruise time, and actual measurement cruising time probably lifts 10%-15%；Pulling force oar is pacified
Dress mode, machine gravity is relatively low, and oar plane is easier to operate to above center of gravity, during flight, and flight is more steady, and underbelly
Free space is more, can in vivo dispose a greater variety of loads.User also can root when selecting pulling force oar or thrust paddle to install
According to different application and scene, load (camera) mounting means is selected, that is, being installed on back installation portion, (foot stool is pacified
Fill the opposite side of side) or bottom installation portion (side of foot stool installation), in general, installed in underbelly installation position
It is wider to put application, is suitable for various in work high above the ground, looks down ground installation equipment and personnel etc., but in special circumstances
Under, for example during similar detection inspection tunnel upper wall situation, load is just particularly important installed in top installation portion.And horn can
Horn is arranged in set on unmanned plane primary structural component one and the horn along after the rotation of horn rotary shaft to realize
In the groove for being used to house the horn after rotary folding to match, so as to be advantageous to the convenient loading packing to unmanned plane and take
Band., can be spacing to the rotating range of the horn and to the institute after rotary folding meanwhile the application is by setting positioning limiting fixator
Horn is stated to be fixed.Through hole or groove are additionally provided with the unmanned plane shell of the application in order to be held to unmanned plane.
Carry to carry and more facilitate.And the machine shell water resistance is preferable, can fly in the rain, even if fuselage interior is intake accidentally, water
Pearl can also flow downwardly to the discharge of minimum point osculum along shell shape.
In addition, dish-shaped primary structural component is circular disk like in the embodiment of the present invention, it can be appreciated that in the middle part of dish for rectangle etc. just
Polygon, or/and, dish-shaped edge is the regular polygons such as rectangle,.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention.In a word, it is all in the present invention
Spirit and principle within, any modification, equivalent substitution and improvements made etc., should be included in protection scope of the present invention it
It is interior.
Claims (9)
- A kind of 1. disc-shaped unmanned machine, it is characterised in that including：Dish-shaped primary structural component, it has the main part for forming dish-shaped periphery, and the protrusion at dish middle part is formed positioned at main part side In the engine department of main part；Positioned at main part opposite side, the cover portion for the cabin for protruding from main part is installed；The main part periphery has certain thickness, and periphery edge is uniformly distributed at least three horns for being provided with and flexing outward, Horn end is equipped with the blade and motor as power；Be provided with foot stool installing structure on the engine department and the cover portion, the engine department and the cover portion select one conduct without Man-machine bottom, removably in installing foot stool on foot stool installing structure.
- 2. disc-shaped unmanned machine according to claim 1, it is characterised in that the foot stool installing structure includes：It is arranged at institute On the surface for stating engine department and the cover portion, at least three hole slots that extend internally, and the direction convergence that extends internally；The foot stool, which corresponds to the mounting structure, has the insertion end that can be inserted into the hole slot.
- 3. disc-shaped unmanned machine according to claim 2, it is characterised in that the hole slot and the insertion end to engage or Thread fiting mode assembles.
- 4. disc-shaped unmanned machine according to claim 1, it is characterised in that described horn one end is stretched into the body peripheral edge Inner fovea part, and horizontally rotate with main body and be connected；Horn is fixed on by certain turned position by a fixture；The main part is peripherally provided with the groove with horn form fit by the inner fovea part, and the notch end corresponds to main body Portion has the recess that match with the motor, is respectively used to house and horizontally rotates the horn and motor to the groove.
- 5. disc-shaped unmanned machine according to claim 4, it is characterised in that inner fovea part described in main part has rolling assembling institute The vertical axle of horn one end is stated, the fixture is the vertical goat's horn screw rod detachably installed.
- 6. disc-shaped unmanned machine according to claim 1, it is characterised in that the engine department or/and the cover portion are close to outer There is hand-held through hole at periphery.
- 7. disc-shaped unmanned machine according to claim 1, it is characterised in that at the engine department or/and the cover portion center With outwardly external components installation portion.
- 8. disc-shaped unmanned machine according to claim 1, it is characterised in that the external components installation portion is provided with shooting Head.
- 9. according to the disc-shaped unmanned machine described in claim any one of 1-8, it is characterised in that the unmanned plane is in its horizontal section Central Symmetry.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201710725565.XA CN107512390A (en) | 2017-08-22 | 2017-08-22 | A kind of disc-shaped unmanned machine |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201710725565.XA CN107512390A (en) | 2017-08-22 | 2017-08-22 | A kind of disc-shaped unmanned machine |
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| CN107512390A true CN107512390A (en) | 2017-12-26 |
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| CN201710725565.XA Pending CN107512390A (en) | 2017-08-22 | 2017-08-22 | A kind of disc-shaped unmanned machine |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110494361A (en) * | 2018-03-28 | 2019-11-22 | 深圳市大疆创新科技有限公司 | Unmanned plane with panorama camera |
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Application publication date: 20171226 |
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