CN103350752A - Four-rotor aircraft - Google Patents
Four-rotor aircraft Download PDFInfo
- Publication number
- CN103350752A CN103350752A CN2013100635768A CN201310063576A CN103350752A CN 103350752 A CN103350752 A CN 103350752A CN 2013100635768 A CN2013100635768 A CN 2013100635768A CN 201310063576 A CN201310063576 A CN 201310063576A CN 103350752 A CN103350752 A CN 103350752A
- Authority
- CN
- China
- Prior art keywords
- upper arm
- quadrotor
- battery
- machine cover
- lower machine
- 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
- 230000001681 protective effect Effects 0.000 claims description 14
- 239000003292 glue Substances 0.000 claims description 9
- 230000000903 blocking effect Effects 0.000 claims description 6
- 230000000295 complement effect Effects 0.000 claims description 6
- 238000000034 method Methods 0.000 claims description 4
- HBBGRARXTFLTSG-UHFFFAOYSA-N Lithium ion Chemical compound [Li+] HBBGRARXTFLTSG-UHFFFAOYSA-N 0.000 claims description 3
- 230000008878 coupling Effects 0.000 claims description 3
- 238000010168 coupling process Methods 0.000 claims description 3
- 238000005859 coupling reaction Methods 0.000 claims description 3
- 230000017525 heat dissipation Effects 0.000 claims description 3
- 229910001416 lithium ion Inorganic materials 0.000 claims description 3
- KKQWHYGECTYFIA-UHFFFAOYSA-N 2,5-dichlorobiphenyl Chemical compound ClC1=CC=C(Cl)C(C=2C=CC=CC=2)=C1 KKQWHYGECTYFIA-UHFFFAOYSA-N 0.000 description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 230000002929 anti-fatigue Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910000600 Ba alloy Inorganic materials 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
Images
Classifications
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
- A63H27/12—Helicopters ; Flying tops
-
- 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
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/30—Supply or distribution of electrical power
- B64U50/31—Supply or distribution of electrical power generated by photovoltaics
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
- Studio Devices (AREA)
Abstract
The invention provides a four-rotor aircraft. The four-rotor aircraft includes an upper aircraft cover including a first upper arm and a second upper arm; and a lower aircraft cover including a first lower arm and a second lower arm. The first upper arm and the first lower arm include a first upper buckle and a first lower buckle respectively. The second upper arm and the second lower arm include a second upper buckle and a second lower buckle respectively. The first upper buckle joints with the first lower buckle and the second upper buckle joints with the second lower buckle, so that the upper aircraft cover is fixed on the lower aircraft cover.
Description
Technical field
The disclosure relates to vertical takeoff and landing (VTOL) aircraft.
Background technology
Quadrotor such as autogyro etc. can be applicable to military and civilian market.For example, a kind of quadrotor that is commonly referred to quadrotor is used for recreational use.Yet quadrotor never is confined to toy or telecontrolled model.Quadrotor also can be used for measurement, supervision, Aerial photography etc.
Many existing quadrotors comprise the many parts that are distributed in the whole aircraft.The parts of example comprise carbon fibre plate, carbon fibre bar and aluminium alloy plate.These parts have complicated shape usually.The quantity of these parts and complicated shape cause these existing quadrotors to have low anti-collision, low deformation resistance, low wind resistance, low fatigue resistance, low agility and/or low steerability (especially when carrying out complicated maneuvering flight).
Summary of the invention
The objective of the invention is provides a kind of simple in structure in order to overcome the deficiency of present technology, easy to assembly and quadrotor with high anti-collision, high deformation resistance, high wind resistance, high antifatigue, high agility and/or high steerability.
A kind of quadrotor comprises:
Upper hood comprises the first upper arm and the second upper arm;
Lower machine cover comprises the first underarm and the second underarm;
Wherein said the first upper arm and described the first underarm comprise hasp and first time hasp on first accordingly;
Wherein said the second upper arm and described the second underarm comprise hasp and second time hasp on second accordingly;
The described second time hasp of snap-engagement on the described first time hasp of snap-engagement and described second on wherein said first, thus described upper hood is fixed in described lower machine cover.
On wherein said first on the hasp and described second at least one in the hasp comprise slit and groove, at least one in wherein said first time hasp and the described second time hasp comprises projection and step; The described slit of wherein said bump bonds and described step engage described groove.
Wherein said lower machine cover comprises battery tray, and described battery tray is constructed to battery-disassembled ground is fixed on the described lower machine cover.
Wherein said upper hood is at the pit of each end of described the first upper arm and described the second upper arm, and described pit is constructed to wherein hold one or more electrical motors.
Described quadrotor further comprises pcb board, and described pcb board is configured to: receive the signal from satellite, remote controllers; Transmit signals to satellite, remote controllers; Control position, speed, working direction and the track of described quadrotor; Process picture intelligence; Or their combination.
Wherein said pcb board is connected on the described upper hood.
Described quadrotor further comprises solar panel.
Described quadrotor further comprises two the first electrical motors that are installed on described the first upper arm and is installed in two the second electrical motors on described the second upper arm.
Described quadrotor, wherein said two the first electrical motors are configured to clickwise and described two the second electrical motors are configured to left-hand revolution; Perhaps wherein said two the first electrical motors are configured to left-hand revolution and described two the second electrical motors are configured to clickwise.
Comprise the rotor that is installed on each described first electrical motor and each described second electrical motor.
Be installed in the mirror image that rotor on each described first electrical motor is mounted in the rotor on each described second electrical motor.
The axis of described the first electrical motor and described the second electrical motor is parallel to each other and be positioned on the same face of cylinder.
Described rotor produces lift when rotation.
Described quadrotor further comprises battery.
Described battery is chargeable lithium ion battery.
Described battery is configured to removably insert wherein from a side of described quadrotor.
Described lower machine cover further comprises one or more ribs, and described rib is configured to prevent from the described battery of described quadrotor sudden outburst.
Described quadrotor, further comprise battery case, described battery case is installed in the described lower machine cover, described battery is installed in the described battery case, the battery loading port correspondence of described battery case is arranged on a side of described quadrotor, described battery is configured to removably insert described battery case from described battery loading port, and the battery loading port of described battery case is provided with elastic blocking key, and described elastic blocking key is configured to prevent skid off described battery from described battery case.
Described quadrotor, further comprise a shooting electronic module, described shooting electronic module comprises camera, described shooting electronic module is arranged on the described lower machine cover, described shooting electronic module is arranged on the described lower machine cover between described lower machine cover and described battery case, described battery case is provided with the camera hold down groove, described camera is installed in the described camera hold down groove, offer the camera via hole on the described lower machine cover, described camera passes described camera via hole, described camera is fixed between the endoporus shoulder and described camera hold down groove of described camera via hole, a side corresponding with described lower machine cover on the described battery case is provided with card column, and described shooting electronic module is positioned between described card column and the described lower machine cover.
Described quadrotor, the bottommost of described first upper arm of wherein said upper hood and the end of described the second upper arm all is lower than the least significant end of described lower machine cover to consist of the lifting support pin of described quadrotor, and the bottom of described lifting support pin also is provided with the flexible glue pad, described lifting support sole end is one-body molded T-shaped dop, what described flexible glue pad was complementary be located on the described T-shaped dop, also offer the wire casing that runs through on the described T-shaped dop, described wire casing is hidden in the described flexible glue pad.
All offer the electric wire storage tank in UNICOM end and the described upper hood in described the first upper arm and described the second upper arm, and the size of described electric wire storage tank and the thickness of single electric wire are complementary, the electric wire that passes described electric wire storage tank fixedly inlay card in described electric wire storage tank, wire casing UNICOM on described electric wire storage tank and the described T-shaped dop, and described the first upper arm and described the second upper arm and the first underarm and the second underarm all adopt triangular shape structure.
Each end of described the first upper arm and described the second upper arm is equipped with the LED lamp, and the luminous end of each described LED lamp all arranges vertically upward, the outermost of each end of described the first upper arm and described the second upper arm offers the caulking groove of setting the LED lamp line, wire casing UNICOM on described caulking groove and the described T-shaped dop, described LED lamp line is embedded in the described caulking groove and passes described wire casing and the electric wire storage tank is connected in the described upper hood.
Described first upper arm of described upper hood and each of described the second upper arm settle the equal hollow out in end of motor that the heat dissipation weight-reducing hole is arranged.
Each end of described the first upper arm and described the second upper arm in order to the internal diameter of the pit that holds electrical motor all less than bore, interference fit between described electrical motor and the described pit.
Described first upper arm of described upper hood and described the second upper arm and the first underarm of corresponding described lower machine cover and jack and the inserting column that the second underarm is respectively arranged with corresponding coupling, described inserting column corresponding between described the first upper arm and described the first underarm is plugged in the described jack, and described inserting column corresponding between described the second upper arm and described the second underarm is plugged in the described jack.
Described lower machine cover is provided with hollow hole.
Described quadrotor also comprises a protective case; the rotor of described quadrotor is positioned at the inboard of described protective case; the fixed support of described protective case is connected to the part that protrudes from described the first upper arm and described the second upper arm on the described motor, and the fixed support of described protective case is positioned at below the plane of rotation of described rotor.
Owing to having adopted said structure, quadrotor of the present invention is simple in structure, and is easy to assembly, and has the characteristics such as high anti-collision, high deformation resistance, high wind resistance, high antifatigue, high agility and/or high steerability.
Description of drawings
Fig. 1 shows the exploded drawings according to the quadrotor of embodiment.
Fig. 2 A shows another exploded drawings of quadrotor.
Fig. 2 B shows the details according to hasp on the shell of the quadrotor of embodiment.
Fig. 3 shows battery is inserted quadrotor.
Fig. 4 shows the electrical motor of quadrotor and the hand of rotation of rotor.
Fig. 5 shows the upward view of quadrotor.
Fig. 6 A shows the lifting support pin decomposing schematic representation of quadrotor.
Fig. 6 B shows the lifting support pin cross-sectional schematic of quadrotor.
Fig. 7 show quadrotor the LED lamp cross-sectional schematic is set.
Fig. 8 A show quadrotor protective case birds-eye view is set.
Fig. 8 B is the cross-sectional schematic of A-A among Fig. 8 A.
Fig. 9 shows the motor setting of quadrotor and the hole post on the shell cooperates schematic diagram.
Figure 10 shows the embodiment decomposing schematic representation of another kind of quadrotor.
Figure 11 shows another angle decomposition schematic diagram of the embodiment among Figure 10.
Figure 12 shows the first upper arm of quadrotor and the cross-sectional schematic that the second upper arm matches with the first underarm and the second underarm.
The specific embodiment
Fig. 1 shows the exploded drawings according to the quadrotor of embodiment.Quadrotor comprises hood 5, lower machine cover 6, PCB 9, one or more electrical motor 10 and 11, battery 12, four rotors 1,2,3 and 4.Quadrotor may further include one or more screws 8 and 7.
Fig. 2 A shows another exploded drawings of quadrotor.As illustrated in fig. 1 and 2, upper hood 5 has the first upper arm 51, the second upper arm 52 and body 53.The first and second upper arm 51 and 52 are connected to body 53 and the first and second upper arm 51 and 52 are intersected with each other.On each end 51a of the first upper arm 51 and 51b, pit 510a and 510b can be arranged respectively.Pit 510a and 510b are constructed to wherein hold electrical motor 11 or any transmission device.On each end 52a of the first arm 52 and 52b, pit 520a and 520b can be arranged respectively.Pit 520a and 520b are serving as the effect of wherein holding electrical motor 10 or any transmission device.
Shown in Fig. 1 and 2 A, lower machine cover 6 also has the first underarm 61, the second underarm 62 and body 63.The first underarm 61 is corresponding to the first upper arm 51 of upper hood 5; The second underarm 62 is corresponding to the second upper arm 52.In an embodiment, lower machine cover 6 comprises battery tray 66, and battery tray is constructed to battery 12 removably is fixed on the lower machine cover 6.
According to embodiment, each end of the first and second underarms 61 and each end of 62 and the first and second upper arm 51 and 52 comprises hasp and is constructed to and is engaged with each other when fit on hood 5 and lower machine cover 6.Fig. 2 B shows the details according to the hasp of embodiment.Dull and stereotyped A among Fig. 2 B is corresponding to the dotted line frame A among Fig. 2 A and show the details of hasp on arm 61 and 62.Dull and stereotyped B among Fig. 2 B is corresponding to the dotted line frame B among Fig. 2 A and show the details of hasp on arm 51 and 52.Hasp on the underarm 61 and 62 includes projection 660.Projection 660 is narrower than underarm 61 and 62.Hasp on the underarm 61 and 62 includes step 670, and step separates with projection 660.Hasp on the upper arm 51 and 52 includes slit 560 and groove 570.Slit 560 has in fact and protruding 660 identical width.When fit on hood 5 and lower machine cover 6, the hasp on the snap-engagement upper arm 51 and 52 on the underarm 61 and 62, thus upper hood 5 is fixed in lower machine cover 6.Especially, protruding 660 engagement slot 560 and step 670 engagement groove 570.Dull and stereotyped C referring to Fig. 2 B.Upper hood 5 can further be fixed in lower machine cover 6 by screw 8.
PCB 9 can use any suitable method simultaneously, and such as screw 7, clip or adhesives etc. is installed on the hood 5.For example, PCB 9 can be installed in the body 53 times of hood 5.PCB 9 can comprise any suitable parts, for example remote control transport module, antenna, microprocessor, memory device, amplifier, gps receiver, altimeter and photographic camera.PCB 9 can be constructed to receive the signal from satellite, remote controllers; Transmit signals to satellite, remote controllers; Position, speed, working direction and the track of control aircraft, image data processing; And driving motor 10 and 11.PCB 9 can be by any suitable Power supply, for example battery 12 or solar panel.
As shown in Figure 4, the electrical motor 10 that is installed among pit 520a and the 520b is configured to rotate in same direction.The electrical motor 11 that is installed among pit 510a and the 510b is configured to rotate in same direction, but with the direction of the opposite direction of electrical motor 10.That is, be installed in the electrical motor clickwise on the arm of hood 5 and be installed in electrical motor left-hand revolution on another arm of hood 5, or vice versa.Electrical motor 10 and 11 axis are parallel to each other and be positioned on the same face of cylinder.
Rotor 2 and 3 is installed on the electrical motor 10 and rotor 1 and 4 is installed on the electrical motor 11.In an embodiment, rotor 2 equally with rotor 1 and 4 has an identical angle of attack with 3.Because rotor 2 and 3 rotates in the direction opposite with rotor 1 and 4, so all rotor 1-4 produce lift when rotation, the blade on the rotor 2 and 3 has the rotation opposite with respect to their maincenter spare.Rotor 2 and 3 can be considered as the mirror image of rotor 1 and 4.
As shown in Figure 3, being shaped as of lower machine cover 6 and upper hood 5: when assembling, battery 12 can removably insert the battery tray 66 from a side of aircraft (for example, the direction of four parallel arrows in the upper flat plate of Fig. 3).Lower machine cover 6 or upper hood 5 can comprise one or more ribs 690, and these ribs are constructed to prevent discharge battery 12 from aircraft suddenly.
Fig. 5 shows the upward view of aircraft.Fig. 2 B middle plateform C shows the details of dashed region.
Such as Figure 10, embodiment shown in 11, also comprise battery case 17 between described upper hood 5 and the lower machine cover 6, described battery case 17 is installed in the described lower machine cover 6, described battery 12 is installed in the described battery case 17, battery loading port 171 correspondences of described battery case are arranged on a side of described quadrotor, described battery 12 is configured to removably insert described battery case 17 from described battery loading port 171, the battery loading port 171 of described battery case 17 is provided with elastic blocking key 172, and described elastic blocking key 172 is configured to prevent skid off described battery 12 from described battery case 17.
Such as Figure 10, embodiment shown in 11, further comprise a shooting electronic module 18, described shooting electronic module 18 comprises camera 181, described shooting electronic module 18 is arranged on the described lower machine cover 6, described shooting electronic module 18 is arranged on the described lower machine cover 6 between described lower machine cover 6 and described battery case 17, described battery case 17 is provided with camera hold down groove 173, described camera 181 is installed in the described camera hold down groove 173, offer camera via hole 64 on the described lower machine cover 6, described camera 181 passes described camera via hole 64, described camera 181 is fixed between the endoporus shoulder and described camera hold down groove 173 of described camera via hole 64, a side corresponding with described lower machine cover 6 is provided with the card column 174 for fixing described shooting electronic module 18 on the described battery case 17, and described shooting electronic module 18 is positioned between described card column 174 and the described lower machine cover 6.
Such as Fig. 6 A, shown in the 6B, the bottommost of described first upper arm 51 of described upper hood 5 and the end of described the second upper arm 52 all is lower than the least significant end of described lower machine cover 6 to consist of the lifting support pin 54 of described quadrotor, and the bottom of described lifting support pin 54 also is provided with flexible glue pad 55, described lifting support pin 54 bottoms are one-body molded T-shaped dop 541, what described flexible glue pad 55 was complementary be located on the described T-shaped dop 541, also offer the wire casing 542 that runs through on the described T-shaped dop 541, described wire casing 542 is hidden in the described flexible glue pad 55, thereby the electric wire that passes described wire casing 542 can be stashed.
As shown in figure 12, all offer the electric wire storage tank 56 in UNICOM end and the described upper hood 5 in described the first upper arm 51 and described the second upper arm 52, and the size of described electric wire storage tank 56 and the thickness of single electric wire are complementary, the electric wire that passes described electric wire storage tank 56 fixedly inlay card in described electric wire storage tank 56, so that on assembling is described, can not expose or the impact assembling that gets loose because of electric wire in the process of hood 5 and lower machine cover 6, wire casing 542 UNICOMs on described electric wire storage tank 56 and the described T-shaped dop 541, and described the first upper arm 51 and described the second upper arm 52 and the first underarm 61 and the second underarm 62 all adopt triangular shape structure, its structural stability of having utilized triangular shape structural reinforcing, and can reduce greatly air resistance, be conducive to the flight of described quadrotor.
As shown in Figure 7, each end of described the first upper arm 51 and described the second upper arm 52 is equipped with LED lamp 57, and the luminous end of each described LED lamp 57 all arranges vertically upward, so that the light that LED lamp 57 sends can be radiated on the rotor, to build better light efficiency, the outermost of each end of described the first upper arm 51 and described the second upper arm 52 offers the caulking groove 571 of setting the LED lamp line, wire casing 542 UNICOMs on described caulking groove 571 and the described T-shaped dop 541, described LED lamp line is embedded in the described caulking groove 571 and passes described wire casing 542 and electric wire storage tank 56 is connected in the described upper hood 5.
As shown in Figure 6A, the equal hollow out of end 51a, 51b, 52a, 52b of each arrangement motor of described first upper arm 51 of wherein said upper hood 5 and described the second upper arm 52 has heat dissipation weight-reducing hole 58.
As shown in Figure 9, each end of wherein said the first upper arm 51 and described the second upper arm 52 in order to the internal diameter that holds electrical motor 10,11 pit 510a, 510b, 520a, 520b all less than bore, described electrical motor 10,11 and described pit 510a, 510b, 520a, 520b between interference fit, and then can better fix described electrical motor 10,11.
As shown in Figure 9, described first upper arm 51 of wherein said upper hood 5 and described the second upper arm 52 and the first underarm 61 of corresponding described lower machine cover 6 and the jack 59 and inserting column 65 that the second underarm 62 is respectively arranged with corresponding coupling, described inserting column 65 corresponding between described the first upper arm 51 and described the first underarm 61 is plugged in the described jack 59, described inserting column 65 corresponding between described the second upper arm 52 and described the second underarm 62 is plugged in the described jack 59, utilize hole post close-fitting design, the assembling between convenient described the first upper arm 51 and the second upper arm 52 and described the first underarm 61 and the second underarm 62.
As shown in figure 10, wherein said lower machine cover 6 is provided with hollow hole 66, conveniently dispels the heat and alleviates the weight of described lower machine cover 6.
Shown in Fig. 8 A, 8B; also comprise a protective case 5a; the rotor of described quadrotor is positioned at the inboard of described protective case 5a; the fixed support 5a1 of described protective case 5a is connected to the part that protrudes from described the first upper arm 51 and described the second upper arm 52 on the described motor 10,11; and the fixed support 5a1 of described protective case 5a is positioned at below the plane of rotation of described rotor; described protective case 5a provides the shatter-resistant protection for described quadrotor, and does not disturb the rotation of described rotor.
Stable, wind resistance, crash-resistant, quick and controollable according to the quadrotor as herein described of one or more embodiment.
About claims, when example is such as the word of " ", " ", " at least one " or " at least one part " etc. before feature, be not to be intended to limit claim to be this feature only, unless make especially on the contrary statement in the claim.
Above explanation is intended to illustrative, rather than restrictive.Therefore, it will be apparent to one skilled in the art that in the scope of the claims that do not break away from following elaboration and can make modification.
Claims (27)
1. quadrotor comprises:
Upper hood comprises the first upper arm and the second upper arm;
Lower machine cover comprises the first underarm and the second underarm;
Wherein said the first upper arm and described the first underarm comprise hasp and first time hasp on first accordingly;
Wherein said the second upper arm and described the second underarm comprise hasp and second time hasp on second accordingly;
The described second time hasp of snap-engagement on the described first time hasp of snap-engagement and described second on wherein said first, thus described upper hood is fixed in described lower machine cover.
2. quadrotor according to claim 1, on wherein said first on the hasp and described second at least one in the hasp comprise slit and groove, at least one in wherein said first time hasp and the described second time hasp comprises projection and step; The described slit of wherein said bump bonds and described step engage described groove.
3. quadrotor according to claim 1, wherein said lower machine cover comprises battery tray, described battery tray is constructed to battery-disassembled ground is fixed on the described lower machine cover.
4. quadrotor according to claim 1, wherein said upper hood is at the pit of each end of described the first upper arm and described the second upper arm, and described pit is constructed to wherein hold one or more electrical motors.
5. quadrotor according to claim 1 further comprises pcb board, and described pcb board is configured to: receive the signal from satellite, remote controllers; Transmit signals to satellite, remote controllers; Control position, speed, working direction and the track of described quadrotor; Process picture intelligence; Or their combination.
6. quadrotor according to claim 5, wherein said pcb board is connected on the described upper hood.
7. quadrotor according to claim 1 further comprises solar panel.
8. quadrotor according to claim 1 further comprises two the first electrical motors that are installed on described the first upper arm and is installed in two the second electrical motors on described the second upper arm.
9. quadrotor according to claim 8, wherein said two the first electrical motors are configured to clickwise and described two the second electrical motors are configured to left-hand revolution; Perhaps wherein said two the first electrical motors are configured to left-hand revolution and described two the second electrical motors are configured to clickwise.
10. quadrotor according to claim 9 further comprises the rotor that is installed on each described first electrical motor and each described second electrical motor.
11. quadrotor according to claim 10 wherein is installed in the mirror image that rotor on each described first electrical motor is mounted in the rotor on each described second electrical motor.
12. quadrotor according to claim 8, the axis of wherein said the first electrical motor and described the second electrical motor is parallel to each other and be positioned on the same face of cylinder.
13. quadrotor according to claim 10, wherein said rotor produce lift when rotation.
14. quadrotor according to claim 1 further comprises battery.
15. quadrotor according to claim 14, wherein said battery are chargeable lithium ion batteries.
16. quadrotor according to claim 14, wherein said battery are configured to removably insert wherein from a side of described quadrotor.
17. quadrotor according to claim 14, wherein said lower machine cover further comprises one or more ribs, and described rib is configured to prevent from the described battery of described quadrotor sudden outburst.
18. quadrotor according to claim 14, further comprise battery case, described battery case is installed in the described lower machine cover, described battery is installed in the described battery case, the battery loading port correspondence of described battery case is arranged on a side of described quadrotor, described battery is configured to removably insert described battery case from described battery loading port, the battery loading port of described battery case is provided with elastic blocking key, and described elastic blocking key is configured to prevent skid off described battery from described battery case.
19. quadrotor according to claim 18, further comprise a shooting electronic module, described shooting electronic module comprises camera, described shooting electronic module is arranged on the described lower machine cover, described shooting electronic module is arranged on the described lower machine cover between described lower machine cover and described battery case, described battery case is provided with the camera hold down groove, described camera is installed in the described camera hold down groove, offer the camera via hole on the described lower machine cover, described camera passes described camera via hole, described camera is fixed between the endoporus shoulder and described camera hold down groove of described camera via hole, a side corresponding with described lower machine cover on the described battery case is provided with card column, and described shooting electronic module is positioned between described card column and the described lower machine cover.
20. quadrotor according to claim 1, the bottommost of described first upper arm of wherein said upper hood and the end of described the second upper arm all is lower than the least significant end of described lower machine cover to consist of the lifting support pin of described quadrotor, and the bottom of described lifting support pin also is provided with the flexible glue pad, described lifting support sole end is one-body molded T-shaped dop, what described flexible glue pad was complementary be located on the described T-shaped dop, also offer the wire casing that runs through on the described T-shaped dop, described wire casing is hidden in the described flexible glue pad.
21. quadrotor according to claim 20, all offer the electric wire storage tank in UNICOM end and the described upper hood in described the first upper arm and described the second upper arm, and the size of described electric wire storage tank and the thickness of single electric wire are complementary, the electric wire that passes described electric wire storage tank fixedly inlay card in described electric wire storage tank, wire casing UNICOM on described electric wire storage tank and the described T-shaped dop, and described the first upper arm and described the second upper arm and the first underarm and the second underarm all adopt triangular shape structure.
22. quadrotor according to claim 21, each end of described the first upper arm and described the second upper arm is equipped with the LED lamp, and the luminous end of each described LED lamp all arranges vertically upward, the outermost of each end of described the first upper arm and described the second upper arm offers the caulking groove of setting the LED lamp line, wire casing UNICOM on described caulking groove and the described T-shaped dop, described LED lamp line is embedded in the described caulking groove and passes described wire casing and the electric wire storage tank is connected in the described upper hood.
23. quadrotor according to claim 4, described first upper arm of wherein said upper hood and each of described the second upper arm settle the equal hollow out in end of motor that the heat dissipation weight-reducing hole is arranged.
24. quadrotor according to claim 4, each end of wherein said the first upper arm and described the second upper arm in order to the internal diameter of the pit that holds electrical motor all less than bore, interference fit between described electrical motor and the described pit.
25. quadrotor according to claim 1, described first upper arm of wherein said upper hood and described the second upper arm and the first underarm of corresponding described lower machine cover and jack and the inserting column that the second underarm is respectively arranged with corresponding coupling, described inserting column corresponding between described the first upper arm and described the first underarm is plugged in the described jack, and described inserting column corresponding between described the second upper arm and described the second underarm is plugged in the described jack.
26. quadrotor according to claim 1, wherein said lower machine cover is provided with hollow hole.
27. quadrotor according to claim 10; also comprise a protective case; the rotor of described quadrotor is positioned at the inboard of described protective case; the fixed support of described protective case is connected to the part that protrudes from described the first upper arm and described the second upper arm on the described motor, and the fixed support of described protective case is positioned at below the plane of rotation of described rotor.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/CN2013/000417 WO2014067224A1 (en) | 2012-10-29 | 2013-04-11 | Quadcopter |
| EP14153034.5A EP2772429A1 (en) | 2013-02-28 | 2014-01-29 | Four-rotor aircraft |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210423957.8 | 2012-10-29 | ||
| US13/672,795 | 2012-11-09 | ||
| US13/672,795 US8973861B2 (en) | 2012-10-29 | 2012-11-09 | Tetra-propeller aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103350752A true CN103350752A (en) | 2013-10-16 |
Family
ID=49307202
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013200918122U Expired - Lifetime CN203318680U (en) | 2012-10-29 | 2013-02-28 | Four-rotor aircraft |
| CN2013100635768A Pending CN103350752A (en) | 2012-10-29 | 2013-02-28 | Four-rotor aircraft |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013200918122U Expired - Lifetime CN203318680U (en) | 2012-10-29 | 2013-02-28 | Four-rotor aircraft |
Country Status (2)
| Country | Link |
|---|---|
| CN (2) | CN203318680U (en) |
| DE (1) | DE202013101170U1 (en) |
Cited By (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103770942A (en) * | 2014-02-28 | 2014-05-07 | 戴维 | Long-endurance solar aircraft capable of vertically taking off and landing |
| CN103895462A (en) * | 2014-04-15 | 2014-07-02 | 北京航空航天大学 | Land and air search and rescue device capable of detecting human face and achieving photovoltaic power generation |
| CN104002964A (en) * | 2014-05-30 | 2014-08-27 | 深圳一电科技有限公司 | Multi-rotor unmanned aerial vehicle |
| CN104276276A (en) * | 2014-10-08 | 2015-01-14 | 中国航空工业集团公司西安飞机设计研究所 | Modularized handling unmanned aerial vehicle layout |
| CN104494805A (en) * | 2014-11-08 | 2015-04-08 | 常州神鹰碳塑复合材料有限公司 | Carbon fiber multi-rotor unmanned aircraft fuselage and method for manufacturing the same |
| WO2015058352A1 (en) * | 2013-10-22 | 2015-04-30 | 深圳市哈博森科技有限公司 | Aircraft and fixing sleeve |
| CN104627361A (en) * | 2015-02-05 | 2015-05-20 | 深圳雷柏科技股份有限公司 | Modularized unmanned aerial vehicle |
| CN104648667A (en) * | 2015-02-17 | 2015-05-27 | 何春旺 | Aircraft |
| CN104843193A (en) * | 2015-05-13 | 2015-08-19 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle lamplight warning system |
| CN105905274A (en) * | 2016-04-18 | 2016-08-31 | 中国科学院遥感与数字地球研究所 | Fuselage structure of octorotor unmanned aerial vehicle |
| CN105947205A (en) * | 2016-04-29 | 2016-09-21 | 易瓦特科技股份公司 | Unmanned aerial vehicle with quick detaching double-propeller structure |
| CN106005356A (en) * | 2014-06-26 | 2016-10-12 | 深圳市大疆创新科技有限公司 | Aircraft and signal line protection assembly thereof |
| WO2016172947A1 (en) * | 2015-04-30 | 2016-11-03 | 深圳市大疆创新科技有限公司 | Thermal management system and thermal management method, and unmanned aerial vehicle for application of the thermal management system |
| CN106143867A (en) * | 2015-04-08 | 2016-11-23 | 优利科技有限公司 | Aircraft fuselage and include its aircraft |
| WO2016192020A1 (en) * | 2015-06-01 | 2016-12-08 | SZ DJI Technology Co., Ltd. | Method, apparatus, and kit for assembling a mobile platform |
| CN106377903A (en) * | 2016-10-12 | 2017-02-08 | 徐付超 | Brain sensing unmanned aerial vehicle |
| CN106672225A (en) * | 2016-12-27 | 2017-05-17 | 昆山优尼电能运动科技有限公司 | Cooling air path system of unmanned aerial vehicle |
| WO2017121038A1 (en) * | 2016-01-14 | 2017-07-20 | 骅星科技发展有限公司 | Novel folding unmanned aerial vehicle |
| US9884681B2 (en) | 2013-01-10 | 2018-02-06 | SZ DJI Technology Co., Ltd. | Aerial vehicle with frame assemblies |
| US9896195B2 (en) | 2014-06-26 | 2018-02-20 | SZ DJI Technology Co., Ltd. | Aerial vehicle and a signal line protection assembly thereof |
| US10155584B2 (en) | 2012-11-15 | 2018-12-18 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
| CN109050894A (en) * | 2013-11-13 | 2018-12-21 | 深圳市大疆创新科技有限公司 | More rotor unmanned aircrafts |
| CN109476376A (en) * | 2016-07-29 | 2019-03-15 | 夏普株式会社 | Moving body |
Families Citing this family (28)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2995875B1 (en) * | 2012-09-21 | 2015-05-29 | A U E V Advanced Unmanned Electric Vehicle | DRONE CHASSIS |
| CN203318680U (en) * | 2012-10-29 | 2013-12-04 | 深圳市哈博森科技有限公司 | Four-rotor aircraft |
| CN203306224U (en) | 2013-05-31 | 2013-11-27 | 深圳市大疆创新科技有限公司 | Propeller and aircraft provided with same |
| DE102013107654A1 (en) * | 2013-07-18 | 2015-01-22 | OIC-GmbH | Aircraft for carrying one or more recording devices through the air |
| DE102013108076A1 (en) * | 2013-07-29 | 2015-01-29 | OIC-GmbH | Aircraft for carrying one or more recording devices and system therefor |
| US9061763B1 (en) * | 2013-08-15 | 2015-06-23 | Traxxas Lp | Rotorcraft with integrated light pipe support members |
| DE102014103847A1 (en) * | 2014-03-20 | 2015-09-24 | Jochen Schmidt | Multicopter, boom for a multicopter and method of making the boom |
| FR3020763B1 (en) | 2014-05-06 | 2016-06-03 | Parrot | QUADRICOPTERE TYPE ROTARY SAILING WHEEL HAVING REMOVABLE PROPERTY PROTECTION BUMPERS |
| ES2787267T3 (en) | 2014-10-27 | 2020-10-15 | Guangzhou Xaircraft Tech Co Ltd | Rotary-wing aircraft and connecting structure for an arm and an aircraft cell of a rotary-wing aircraft |
| WO2016069723A1 (en) * | 2014-10-29 | 2016-05-06 | Identified Technologies Corporation | Structure and manufacturing process for unmanned aerial vehicle |
| CN104590556B (en) * | 2014-10-31 | 2017-06-27 | 易瓦特科技股份公司 | A kind of folding unmanned plane |
| CN104443364B (en) * | 2014-12-22 | 2016-06-15 | 深圳市高巨创新科技开发有限公司 | Detachable undercarriage and four-axle aircraft |
| CN104648654A (en) * | 2015-03-15 | 2015-05-27 | 宁波大观智能科技有限公司 | Multi-rotor-wing aircraft stander |
| CN104816822A (en) * | 2015-04-23 | 2015-08-05 | 张�杰 | Aircraft with four fixed rotor wings |
| CN104787320A (en) * | 2015-04-23 | 2015-07-22 | 张�杰 | Communication anti-interference type four-rotor aircraft |
| USD827724S1 (en) | 2015-09-28 | 2018-09-04 | Traxxas Lp | Set of supporting arms for a quadrotor model helicopter |
| USD827723S1 (en) | 2015-09-28 | 2018-09-04 | Traxxas Lp | Quadrotor model helicopter |
| CN106621378A (en) * | 2015-10-29 | 2017-05-10 | 马铿钧 | Aviation aircraft with automatic charging system |
| FR3043917A1 (en) * | 2015-11-19 | 2017-05-26 | Chouette | ELECTRIC STORAGE DRONE DISTRIBUTED |
| CN105366042B (en) * | 2015-11-30 | 2018-05-25 | 易瓦特科技股份公司 | Unmanned flight's equipment |
| FR3045569B1 (en) * | 2015-12-17 | 2017-12-08 | Arthur Gardin | DRONE WITH LOW VIBRATION LEVEL |
| WO2017128050A1 (en) * | 2016-01-26 | 2017-08-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and multi-lens imaging system |
| CN106152018A (en) * | 2016-08-16 | 2016-11-23 | 谭圆圆 | Unmanned vehicle is from illuminator and means of illumination thereof |
| US11141673B1 (en) | 2016-09-28 | 2021-10-12 | Traxxas Lp | Model rotorcraft with light pipe support members |
| CN106428539B (en) * | 2016-11-13 | 2019-05-28 | 天津黎明时代信息技术有限公司 | Unmanned plane with rapid disassembling wing function |
| CN106275409A (en) * | 2016-11-16 | 2017-01-04 | 腾讯科技（深圳）有限公司 | A kind of unmanned plane |
| CN106516103B (en) * | 2016-11-24 | 2019-06-28 | 腾讯科技（深圳）有限公司 | A kind of multi-rotor unmanned aerial vehicle |
| CN108513740B (en) * | 2017-02-24 | 2020-04-07 | 深圳市大疆创新科技有限公司 | Frame and unmanned vehicles |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2455374A (en) * | 2008-06-16 | 2009-06-10 | Middlesex University Higher Ed | Unmanned aerial vehicle comprising a triangular array of rotors |
| CN201367115Y (en) * | 2008-11-17 | 2009-12-23 | 西安智澜科技发展有限公司 | Foldable four-axis multi-rotor wing aerocraft |
| US20100001120A1 (en) * | 2008-07-02 | 2010-01-07 | Sun wei hong | High-speed aircraft with vertical lift and self-revolving ability |
| US20100108801A1 (en) * | 2008-08-22 | 2010-05-06 | Orville Olm | Dual rotor helicopter with tilted rotational axes |
| CN201565139U (en) * | 2009-11-12 | 2010-09-01 | 陈立光 | Novel toy helicopter |
| CN201565141U (en) * | 2009-12-31 | 2010-09-01 | 贵阳帝三数字技术有限公司 | Eight-oar intelligent aerial-photography unmanned air-vehicle mortise-and-tenon joint fuselage structure |
| CN102381471A (en) * | 2010-09-02 | 2012-03-21 | 梦想空间世界有限公司 | Unmanned flying vehicle made with PCB |
| KR20120065546A (en) * | 2010-12-13 | 2012-06-21 | 주병규 | Quad-copter structure |
| CN203318680U (en) * | 2012-10-29 | 2013-12-04 | 深圳市哈博森科技有限公司 | Four-rotor aircraft |
-
2013
- 2013-02-28 CN CN2013200918122U patent/CN203318680U/en not_active Expired - Lifetime
- 2013-02-28 CN CN2013100635768A patent/CN103350752A/en active Pending
- 2013-03-19 DE DE202013101170U patent/DE202013101170U1/en not_active Expired - Lifetime
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2455374A (en) * | 2008-06-16 | 2009-06-10 | Middlesex University Higher Ed | Unmanned aerial vehicle comprising a triangular array of rotors |
| US20100001120A1 (en) * | 2008-07-02 | 2010-01-07 | Sun wei hong | High-speed aircraft with vertical lift and self-revolving ability |
| US20100108801A1 (en) * | 2008-08-22 | 2010-05-06 | Orville Olm | Dual rotor helicopter with tilted rotational axes |
| CN201367115Y (en) * | 2008-11-17 | 2009-12-23 | 西安智澜科技发展有限公司 | Foldable four-axis multi-rotor wing aerocraft |
| CN201565139U (en) * | 2009-11-12 | 2010-09-01 | 陈立光 | Novel toy helicopter |
| CN201565141U (en) * | 2009-12-31 | 2010-09-01 | 贵阳帝三数字技术有限公司 | Eight-oar intelligent aerial-photography unmanned air-vehicle mortise-and-tenon joint fuselage structure |
| CN102381471A (en) * | 2010-09-02 | 2012-03-21 | 梦想空间世界有限公司 | Unmanned flying vehicle made with PCB |
| KR20120065546A (en) * | 2010-12-13 | 2012-06-21 | 주병규 | Quad-copter structure |
| CN203318680U (en) * | 2012-10-29 | 2013-12-04 | 深圳市哈博森科技有限公司 | Four-rotor aircraft |
Non-Patent Citations (1)
| Title |
|---|
| TRAXXAS: "《QR-1 Canopy and Motor Replacement Instructions》", 《QR-1 CANOPY AND MOTOR REPLACEMENT INSTRUCTIONS》 * |
Cited By (40)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10196137B2 (en) | 2012-11-15 | 2019-02-05 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
| US10155584B2 (en) | 2012-11-15 | 2018-12-18 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
| US11338912B2 (en) | 2012-11-15 | 2022-05-24 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
| US10472056B2 (en) | 2012-11-15 | 2019-11-12 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
| US10272994B2 (en) | 2012-11-15 | 2019-04-30 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
| US10189562B2 (en) | 2012-11-15 | 2019-01-29 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
| US9884681B2 (en) | 2013-01-10 | 2018-02-06 | SZ DJI Technology Co., Ltd. | Aerial vehicle with frame assemblies |
| US10046844B2 (en) | 2013-01-10 | 2018-08-14 | SZ DJI Technology Co., Ltd. | Aerial vehicle with frame assemblies |
| US9099902B2 (en) | 2013-10-22 | 2015-08-04 | Shenzhen Hubsan Intelligent Co., Ltd. | Aircraft vehicle and a fixing sleeve |
| GB2534330A (en) * | 2013-10-22 | 2016-07-27 | Shenzhen Hubsan Tech Co Ltd | Aircraft and fixing sleeve |
| GB2534330B (en) * | 2013-10-22 | 2016-11-30 | Shenzhen Hubsan Tech Co Ltd | Aircraft and retainer sleeve |
| WO2015058352A1 (en) * | 2013-10-22 | 2015-04-30 | 深圳市哈博森科技有限公司 | Aircraft and fixing sleeve |
| CN109050894A (en) * | 2013-11-13 | 2018-12-21 | 深圳市大疆创新科技有限公司 | More rotor unmanned aircrafts |
| CN103770942A (en) * | 2014-02-28 | 2014-05-07 | 戴维 | Long-endurance solar aircraft capable of vertically taking off and landing |
| CN103895462A (en) * | 2014-04-15 | 2014-07-02 | 北京航空航天大学 | Land and air search and rescue device capable of detecting human face and achieving photovoltaic power generation |
| CN104002964B (en) * | 2014-05-30 | 2016-02-03 | 深圳一电科技有限公司 | Many rotor wing unmanned aerial vehicles |
| CN104002964A (en) * | 2014-05-30 | 2014-08-27 | 深圳一电科技有限公司 | Multi-rotor unmanned aerial vehicle |
| US9896195B2 (en) | 2014-06-26 | 2018-02-20 | SZ DJI Technology Co., Ltd. | Aerial vehicle and a signal line protection assembly thereof |
| US11180246B2 (en) | 2014-06-26 | 2021-11-23 | SZ DJI Technology Co., Ltd. | Aerial vehicle and a signal line protection assembly thereof |
| US10513329B2 (en) | 2014-06-26 | 2019-12-24 | SZ DJI Technology Co., Ltd. | Aerial vehicle and a signal line protection assembly thereof |
| US10227131B2 (en) | 2014-06-26 | 2019-03-12 | SZ DJI Technology Co., Ltd. | Aerial vehicle and a signal line protection assembly thereof |
| CN106005356B (en) * | 2014-06-26 | 2018-11-27 | 深圳市大疆创新科技有限公司 | A kind of aircraft and its signal wire protect component |
| CN106005356A (en) * | 2014-06-26 | 2016-10-12 | 深圳市大疆创新科技有限公司 | Aircraft and signal line protection assembly thereof |
| CN104276276A (en) * | 2014-10-08 | 2015-01-14 | 中国航空工业集团公司西安飞机设计研究所 | Modularized handling unmanned aerial vehicle layout |
| CN104494805A (en) * | 2014-11-08 | 2015-04-08 | 常州神鹰碳塑复合材料有限公司 | Carbon fiber multi-rotor unmanned aircraft fuselage and method for manufacturing the same |
| CN104627361A (en) * | 2015-02-05 | 2015-05-20 | 深圳雷柏科技股份有限公司 | Modularized unmanned aerial vehicle |
| CN104648667A (en) * | 2015-02-17 | 2015-05-27 | 何春旺 | Aircraft |
| CN106143867B (en) * | 2015-04-08 | 2020-10-02 | 优利科技有限公司 | Aircraft fuselage reaches aircraft including it |
| CN106143867A (en) * | 2015-04-08 | 2016-11-23 | 优利科技有限公司 | Aircraft fuselage and include its aircraft |
| WO2016172947A1 (en) * | 2015-04-30 | 2016-11-03 | 深圳市大疆创新科技有限公司 | Thermal management system and thermal management method, and unmanned aerial vehicle for application of the thermal management system |
| CN104843193A (en) * | 2015-05-13 | 2015-08-19 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle lamplight warning system |
| US10661900B2 (en) | 2015-06-01 | 2020-05-26 | SZ DJI Technology Co., Ltd. | Method, apparatus, and kit for assembling a mobile platform |
| WO2016192020A1 (en) * | 2015-06-01 | 2016-12-08 | SZ DJI Technology Co., Ltd. | Method, apparatus, and kit for assembling a mobile platform |
| WO2017121038A1 (en) * | 2016-01-14 | 2017-07-20 | 骅星科技发展有限公司 | Novel folding unmanned aerial vehicle |
| CN105905274A (en) * | 2016-04-18 | 2016-08-31 | 中国科学院遥感与数字地球研究所 | Fuselage structure of octorotor unmanned aerial vehicle |
| CN105947205A (en) * | 2016-04-29 | 2016-09-21 | 易瓦特科技股份公司 | Unmanned aerial vehicle with quick detaching double-propeller structure |
| CN109476376A (en) * | 2016-07-29 | 2019-03-15 | 夏普株式会社 | Moving body |
| CN106377903B (en) * | 2016-10-12 | 2018-12-21 | 徐州惠博机电科技有限公司 | A kind of brain sensing unmanned aerial vehicle |
| CN106377903A (en) * | 2016-10-12 | 2017-02-08 | 徐付超 | Brain sensing unmanned aerial vehicle |
| CN106672225A (en) * | 2016-12-27 | 2017-05-17 | 昆山优尼电能运动科技有限公司 | Cooling air path system of unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN203318680U (en) | 2013-12-04 |
| DE202013101170U1 (en) | 2013-03-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203318680U (en) | Four-rotor aircraft | |
| US8973861B2 (en) | Tetra-propeller aircraft | |
| CN107223108B (en) | Power supply module, unmanned vehicle and remote-controlled movement device | |
| EP3795474A1 (en) | Unmanned aerial vehicle | |
| CN204895862U (en) | Four light -duty rotor unmanned aerial vehicle of high balanced symmetry plug -in | |
| CN105292477A (en) | Wrist type portable accompanying flight autonomous supervision unmanned aerial vehicle | |
| CN203593169U (en) | Aerial photography unmanned plane | |
| CN103754379B (en) | A kind of automatic photography stable platform of many lens aerial | |
| CN205010466U (en) | A casing for folding rotor unmanned aerial vehicle | |
| CN205044948U (en) | Solar energy unmanned aerial vehicle | |
| CN208102317U (en) | A kind of unmanned plane of taking photo by plane with antidetonation shatter-resistant | |
| CN205405267U (en) | Six spool miniature aircraft | |
| CN205952317U (en) | Disk -type unmanned vehicles | |
| CN209993649U (en) | Quick assembly disassembly formula battery reaches unmanned aerial vehicle who contains it for unmanned aerial vehicle | |
| CN205633086U (en) | Unmanned aerial vehicle who has alarming function | |
| CN207173949U (en) | A kind of long endurance multi-rotor unmanned aerial vehicle | |
| CN207890009U (en) | A kind of combined modular unmanned plane during flying device | |
| CN213323677U (en) | Unmanned plane | |
| CN205707333U (en) | A kind of four-axle aircraft | |
| CN205256676U (en) | Octahedra aircraft | |
| CN205221113U (en) | Portable companion of wrist formula flies autonomic control unmanned aerial vehicle | |
| CN113511342A (en) | Electric control device and unmanned aerial vehicle | |
| CN219806973U (en) | Integrated compact unmanned aerial vehicle with shell | |
| CN207242046U (en) | A kind of light-operated dispenser electromechanical equipment of unmanned plane | |
| CN208110346U (en) | Unmanned plane master control borad |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20131016 |