CN112874753A - Integrated platy laminated rack unmanned aerial vehicle - Google Patents
Integrated platy laminated rack unmanned aerial vehicle Download PDFInfo
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- CN112874753A CN112874753A CN202110190453.5A CN202110190453A CN112874753A CN 112874753 A CN112874753 A CN 112874753A CN 202110190453 A CN202110190453 A CN 202110190453A CN 112874753 A CN112874753 A CN 112874753A
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- 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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
- B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
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- 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
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Abstract
The invention relates to an integrated platy stacked rack unmanned aerial vehicle which is characterized in that an integrated platy stacked rack comprises at least two layers of integrated rack plates, each integrated rack plate comprises a central circle and an outer circle, the outer circles are connected to the periphery of the central circle, and the integrated rack plates of all layers are connected and fixed through a vertical supporting connecting rod; a rotor motor mounting component is arranged in the peripheral circle, and a motor and a rotor are mounted on the rotor motor mounting component; a power supply and control module is arranged in the central circle; the foot rest is positioned below the integrated plate-shaped laminated frame. According to the integrated platy laminated frame unmanned aerial vehicle without the horn, the horn is not arranged in the frame, the plurality of layers of rotors can be installed through the integrated frame plate and the protection plate, so that the number of the rotors is greatly increased, and the rotors can be installed by fixing the motor at the center of the frame and used for constructing the unmanned aerial vehicle with small size and long endurance; the overall structural strength of the rack is greatly improved, the flight stability and the wind resistance are improved, and the rotor wing is located in the laminated rack and has high safety.
Description
Technical Field
The invention relates to an unmanned aerial vehicle, in particular to an integrated platy laminated rack unmanned aerial vehicle.
Background
In recent years, with the development of unmanned aerial vehicle technology, multi-rotor unmanned aerial vehicles have been developed in a comprehensive way from toys to various industrial applications.
Many rotor unmanned aerial vehicle's constitution includes motor, rotor, frame, battery, control circuit and undercarriage etc.. In addition, many rotor unmanned aerial vehicles contain rotor protection device, prevent that high-speed rotatory rotor and external object from contacting, cause the damage of object, personnel or rotor. Through sufficient and deep retrieval and investigation, the invention patents and the utility model patents which comprise a plurality of unmanned aerial vehicle frames in the Chinese patent which is disclosed at present mainly comprise the structure of the unmanned aerial vehicle frames and the technologies of folding, shock resistance, rain resistance and the like, and the patent application in the aspect of a large number of unmanned aerial vehicles reflects the great progress of China in the field of unmanned aerial vehicles and the like.
Analysis of a number of drone patents shows that the existing drone airframe technique, as shown in figure 1, is mainly composed of three parts: the frame central part 1, the horn 2, the rotor fixing piece 3, etc. Wherein the rack central part is an installation space for a battery, a control circuit, an undercarriage and the like; meanwhile, according to the number of the rotors, the rack central piece provides installation positions for the plurality of the arms 2; and the other end of the horn 2 is provided with a rotor fixing piece 3 for fixing a driving motor of the rotor. Many rotor unmanned aerial vehicle's horn's material majority is the hollow tube, is the general structure in the frame patent, and some then adopt the panel of thickening to replace the hollow tube to do the horn, has reduced the weight of manufacturing cost and horn. Another direction of improvement in the horn is the folding method of the horn, such as the new truss type horn structure.
At present many rotor unmanned aerial vehicle generally has the commonality problem that the load is low, the journey is short, and its leading cause is many rotor aircraft rack construction, and the length of the horn of its spoke shape distribution and the quantity of rotor all are difficult to increase, have restricted rotor size's increase to load, the continuation of the journey mileage that have finally restricted many rotor unmanned aerial vehicle.
Disclosure of Invention
The invention provides an integrated plate-shaped laminated frame unmanned aerial vehicle without a horn, wherein the frame consists of an upper integrated frame plate, a lower integrated frame plate and a vertical support connecting rod between the frame plates, the vertical support connecting rod is not provided with the horn, a rotor motor is fixed on the integrated frame plate, the horn of the traditional multi-rotor unmanned aerial vehicle is not provided, so that the center of the frame can also fix the motor to install a rotor, the traditional structure that the rotors are installed on the periphery of the multi-rotor unmanned aerial vehicle and batteries are installed in the middle of the multi-rotor unmanned aerial vehicle is broken through, the integral structural strength of the frame is greatly improved, the vibration caused by the fixation of the rotor motor at the tail end of the horn of the traditional unmanned aerial vehicle is avoided, and the flight stability.
The integrated platy-laminated rack unmanned aerial vehicle provided by the invention can be composed of a plurality of integrated rack plates, and a plurality of layers of rotors are installed. Two rotor motors of installation can only be one at most just one anti-at last on the horn end of traditional unmanned aerial vehicle frame, form the unmanned aerial vehicle of double-deck rotor. For example, in a rack having four arms, two rotor motors are mounted at the end of each arm, one forward and one reverse, to form an eight-rotor drone. The integrated platy-laminated-rack unmanned aerial vehicle provided by the invention has high structural strength and can build a multilayer rotor wing. For example, integration frame plate comprises a central circle and four periphery circles, designs multilayer frame plate, can install four layers of rotors for the quantity of rotor reaches sixteen, sixteen rotor unmanned aerial vehicle promptly. Theoretically, can build more multilayer's rotor based on the slabby stromatolite frame of integration, the compound twelve rotor unmanned aerial vehicle of one deck four rotors even, one deck eight rotors.
In addition, the motor can also be fixed in the center of the integrated platy stacked rack, the rotor wing is installed, and the traditional structure that the rotor wings are installed around and the battery is installed in the middle of the multi-rotor unmanned aerial vehicle is broken through. For example, based on the characteristic that the integrated platy stacked airframe unmanned aerial vehicle provided by the invention has high structural strength, a central double-layer rotor wing and four peripheral single-layer rotor wings can be built, namely, a six-rotor unmanned aerial vehicle.
In a word, the platy stromatolite frame of integration makes the quantity of rotor increase by a wide margin on the unmanned aerial vehicle, and the frame antitorque commentaries on classics ability is strong, and whole light in weight can build more rotors, bigger load, the many stromatolites formula rotor unmanned aerial vehicle of longer duration.
The integrated frame plate comprises a central circle and a plurality of peripheral circles connected with the periphery of the central circle. The central circle is provided with a supporting structure which is a central part of the unmanned aerial vehicle frame and is used for installing an unmanned aerial vehicle motor and a rotor wing, or an unmanned aerial vehicle battery, a control circuit, a waterproof device and the like; the outer circle has a supporting structure for supporting and protecting the rotor wings, and the number of the supporting structure is the same as that of the rotor wings. For example, in a quad-rotor unmanned aerial vehicle, four peripheral circles are connected to a central circle of an integrated frame plate; six rotor unmanned aerial vehicle then have six periphery circles to analogize in this way.
The center circle and the periphery circle of integration frame plate open and to have a plurality of apertures for reduce the weight of frame plate, improve the aerodynamic performance of frame plate, and for the vertical support connecting rod between upper and lower or the multi-disc frame plate provides the mounting hole.
The vertical supporting connecting rod between the two frame plates is a slender rod, and two ends of the connecting rod are fixed on the frame plates through screws. The length of all vertical support connecting rods between two frame plates is the same, and its length can be adjusted according to rotor and rotor driving motor's height for the rotor is located between two frame plates. The support of multi-disc rack board through the vertical braces connecting rod forms multilayer rotor unmanned aerial vehicle. The frame that constitutes by integration frame board and vertical braces connecting rod both provides the support for unmanned aerial vehicle parts such as rotor, battery, control panel, foot rest, provides protection device for the rotor again.
In order to solve the technical problems, based on the invention principle, the invention adopts the following technical scheme:
(1) an integrated plate-shaped laminated rack unmanned aerial vehicle comprises at least two layers of integrated rack plates, wherein each integrated rack plate comprises a central circle and an outer circle, the outer circle is connected to the periphery of the central circle, and the integrated rack plates are fixedly connected through vertical support connecting rods; a rotor motor mounting component is arranged in the peripheral circle, and a motor and a rotor are mounted on the rotor motor mounting component; a power supply and control module is arranged in the central circle; the foot rest is positioned below the integrated plate-shaped laminated frame.
(2) According to (1) slabby stromatolite frame unmanned aerial vehicle of integration, the periphery circle of topmost layer integration frame plate is not equipped with rotor motor installation component.
(3) According to (1) or (2) integrated platy stacked rack unmanned aerial vehicle, be equipped with the aperture on the integrated frame board, the vertical braces connecting rod is installed through the aperture. The small holes in the integrated frame plate can reduce the weight of the integrated frame plate, improve the aerodynamic performance of the integrated frame plate and be used for installing the vertical support connecting rods.
(4) According to the slabby stromatolite frame unmanned aerial vehicle of integration of (1) - (3), the slabby stromatolite of integration includes two-layer integration frame plate, and upper and lower two-layer integration frame plate all includes a central circle and four periphery circles, constitutes four rotor unmanned aerial vehicle.
(5) According to the integrated platy-laminated rack unmanned aerial vehicle in the step (4), a layer of protection plate is further arranged below the two layers of integrated rack plates; the protection plate comprises four circular arcs corresponding to the peripheral circles; a small hole is formed in the arc, and the vertical support connecting rod is installed through the small hole; four rotors are installed between two-layer integrated frame plate, four rotors are installed between lower floor integrated frame plate and protection shield, constitute two-layer eight rotor unmanned aerial vehicle.
(6) The integrated platy stacked rack unmanned aerial vehicle according to any one of (1) to (3), wherein the integrated platy stack comprises three integrated rack plates, a first layer of protective plate is arranged between a second layer of integrated rack plate and a third layer of integrated rack plate, and a second layer of protective plate is arranged below the third layer of integrated rack plate; each layer of integrated frame plate comprises a central circle and four peripheral circles; each layer of protection plate comprises four arcs corresponding to the peripheral circles; a small hole is formed in the arc, and the vertical support connecting rod is installed through the small hole; four rotors are respectively installed between the first layer of integrated frame plate and the second layer of integrated frame plate, between the second layer of integrated frame plate and the first layer of protection plate, between the first layer of protection plate and the third layer of integrated frame plate, and between the third layer of integrated frame plate and the second layer of protection plate, so that the four-layer sixteen-rotor unmanned aerial vehicle is formed.
(7) According to the slabby stromatolite frame unmanned aerial vehicle of integration of (1) - (3), the slabby stromatolite of integration includes two-layer integration frame plate, and upper and lower two-layer integration frame plate all includes a central circle and six periphery circles, constitutes six rotor unmanned aerial vehicle.
(8) According to the integrated platy-laminated rack unmanned aerial vehicle in the step (7), a layer of protection plate is further arranged below the two layers of integrated rack plates; the protection plate comprises six circular arcs corresponding to the peripheral circles; a small hole is formed in the arc, and the vertical support connecting rod is installed through the small hole; six rotors are installed between the two layers of integrated frame plates, six rotors are installed between the lower layer of integrated frame plate and the protection plate, and the two layers of twelve-rotor unmanned aerial vehicles are formed.
(9) The integrated platy stacked rack unmanned aerial vehicle according to any one of (1) to (3), wherein the integrated platy stack comprises three integrated rack plates, a first layer of protective plate is arranged between a second layer of integrated rack plate and a third layer of integrated rack plate, and a second layer of protective plate is arranged below the third layer of integrated rack plate; each layer of integrated frame plate comprises a central circle and six peripheral circles; each layer of protection plate comprises six circular arcs corresponding to the peripheral circles; the arc is provided with a small hole, and the vertical support connecting rod is installed through the small hole; six rotors are respectively installed between the first layer of integrated frame plate and the second layer of integrated frame plate, between the second layer of integrated frame plate and the first layer of protection plate, between the first layer of protection plate and the third layer of integrated frame plate and between the third layer of integrated frame plate and the second layer of protection plate, so that the four-layer twenty-four rotor unmanned aerial vehicle is formed.
(10) According to the slabby stromatolite frame unmanned aerial vehicle of integration of (1) - (3), the slabby stromatolite of integration includes two-layer integration frame plate, and upper and lower two-layer integration frame plate all includes a central circle and eight periphery circles, constitutes eight rotor unmanned aerial vehicle.
(11) According to the integrated platy-laminated rack unmanned aerial vehicle in the step (10), a layer of protection plate is further arranged below the two layers of integrated rack plates; the protection plate comprises eight circular arcs corresponding to the peripheral circles; a small hole is formed in the arc, and the vertical support connecting rod is installed through the small hole; install eight rotors between two-layer integration frame plate, install eight rotors between lower floor integration frame plate and protection shield, constitute two-layer sixteen rotor unmanned aerial vehicle.
(12) The integrated platy stacked rack unmanned aerial vehicle according to any one of (1) to (3), wherein the integrated platy stack comprises three integrated rack plates, a first layer of protective plate is arranged between a second layer of integrated rack plate and a third layer of integrated rack plate, and a second layer of protective plate is arranged below the third layer of integrated rack plate; each layer of integrated frame plate comprises a central circle and eight peripheral circles; each layer of protection plate comprises eight arcs corresponding to the peripheral circles; a small hole is formed in the arc, and the vertical support connecting rod is installed through the small hole; eight rotors are respectively installed between the first layer of integrated frame plate and the second layer of integrated frame plate, between the second layer of integrated frame plate and the first layer of protection plate, between the first layer of protection plate and the third layer of integrated frame plate, and between the third layer of integrated frame plate and the second layer of protection plate, so that the four-layer thirty-two rotor unmanned aerial vehicle is formed.
(13) An integrated plate-shaped laminated rack unmanned aerial vehicle comprises an upper protection plate, an integrated rack plate and a lower protection plate, wherein the integrated rack plate comprises a central circle and a peripheral circle, the peripheral circle is connected to the periphery of the central circle, the diameter of the central circle is larger than that of the peripheral circle, rotor motor installation members are arranged in the central circle and the peripheral circle, a motor and a rotor wing are installed on the rotor motor installation members, the rotor wing in the central circle is a central rotor wing, and the diameter of the rotor wing in the central circle is larger than that of the rotor wing in the peripheral circle; the central rotor wings are in a pair and are arranged in an up-and-down symmetrical mode; the upper protective plate is in a circle structure corresponding to the central circle; the lower protective plate is of an arc structure corresponding to the peripheral circle; the upper protection plate, the integrated frame plate and the lower protection plate are fixedly connected through a vertical support connecting rod; the foot rest is positioned below the integrated platy stacked rack; the load bin is integrated in the foot rest, and the control module and the power supply are located in the load bin.
(14) The integrated platy stacked rack unmanned aerial vehicle is characterized in that the upper protection plate, the integrated rack plate and the lower protection plate are provided with small holes, and the vertical support connecting rod is installed through the small holes. The small holes in the integrated frame plate can reduce the weight of the integrated frame plate, improve the aerodynamic performance of the integrated frame plate and be used for installing the vertical support connecting rods.
(15) According to (13) or (14) slabby stromatolite frame unmanned aerial vehicle of integration, integration frame plate includes a center circle and six periphery circles two center rotors of installation on the center circle a rotor is installed respectively in six periphery circles, constitutes eight rotor unmanned aerial vehicle.
(16) The unmanned aerial vehicle with integrated plate-shaped laminated frames, according to (1) to (15), wherein the outer circumference circles are connected with each other.
(17) According to the integrated platy stacked rack unmanned aerial vehicle in the (1) - (16), the vertical supporting connecting rod is a slender rod, and two ends of the vertical supporting connecting rod are fixed on the integrated rack plate or the protection plate through screws.
(18) According to the integrated platy-laminated rack unmanned aerial vehicle in (1) - (17), all the vertical supporting connecting rods have the same length, and the length of the vertical supporting connecting rods is adjusted according to the heights of the rotor and the rotor driving motor.
According to the integrated platy laminated rack unmanned aerial vehicle provided by the invention, the rack is not provided with the horn, the integrated rack plate and the protection plate can be used for mounting the multi-layer rotor wings, so that the number of the rotor wings is greatly increased, and the center of the rack can also be used for fixing the motor to mount the rotor wings and constructing the unmanned aerial vehicle with small size and long endurance; greatly improved the holistic structural strength of frame, increased flight stability and wind resistance ability, and the rotor is located stromatolite frame, has high security, compares with prior art and has following technological effect: (1) the frame of the unmanned aerial vehicle is completely free of the horn, so that the overall structural strength of the frame is greatly improved, the vibration caused by the fixation of the rotor motor at the tail end of the horn of the traditional unmanned aerial vehicle is avoided, and the flight stability and the wind resistance of the unmanned aerial vehicle are improved; (2) the rack of the invention is formed by laminating at least two integrated rack plates, the rotor wing is arranged between the two rack plates, and the laminated rotor wing is formed by a plurality of layers of vertically overlapped rotor wings, so that the number of the rotor wings is greatly increased; (3) the center and the periphery of the rack can be provided with the rotor wings to form a novel center-periphery multi-rotor wing layout; (4) all be equipped with the aperture on integration frame board and the protection shield, can reduce the weight of integration frame board, improve the aerodynamic performance of integration frame board, can be for being used for installing the vertical stay connecting rod simultaneously.
Drawings
The present invention will be described in further detail with reference to the accompanying drawings and specific embodiments.
Fig. 1 is a schematic structural diagram of a prior art drone;
FIG. 2 is a schematic structural view of an integrated frame plate having four peripheral circles without rotor motor mounting members;
FIG. 3 is a schematic structural view of an integrated frame plate having four peripheral circles;
FIG. 4 is a schematic structural diagram of a first protection plate;
fig. 5 is a top view of an integrated plate-like laminated frame unmanned aerial vehicle with an integrated frame plate having four peripheral circles;
FIG. 6 is a schematic cross-sectional view of an integrated plate-like laminated airframe drone with one layer of rotor;
fig. 7 is a schematic cross-sectional view of an integrated plate-like laminated airframe drone with two layers of rotors;
fig. 8 is a schematic cross-sectional view of an integrated plate-like laminated airframe drone with four layers of rotors;
FIG. 9 is a schematic structural view of an integrated frame plate with six peripheral circles without rotor motor mounting members;
FIG. 10 is a schematic structural view of an integrated frame plate having six peripheral circles;
FIG. 11 is a schematic structural view of a second protection plate;
fig. 12 is a top view of an integrated plate-like laminated frame drone with an integrated frame plate having six peripheral circles;
figure 13 is a schematic structural view of eight integral frame plates with peripheral circles not provided with rotor motor mounting members;
FIG. 14 is a schematic structural view of an integrated frame plate with eight outer circles;
fig. 15 is a schematic structural view of a third protective plate;
fig. 16 is a top view of an integrated plate-like laminated frame drone with an integrated frame plate having eight outer perimeter circles;
figure 17 is a schematic structural view of an integrated frame plate having six peripheral circles with rotor motor mounting members in the center circle;
fig. 18 is a schematic structural view of an upper protection plate;
fig. 19 is a mechanism diagram of the lower protection plate;
fig. 20 is a top view of an integrated plate-like stacked rack drone having an integrated rack plate with six peripheral circles and a central circle with rotor motor mounting members;
fig. 21 is a side view of fig. 20.
In the figure, the reference numeral 1 is a rack center part, 2 is a horn, 3 is a rotor fixing part, 4 is a small hole, 5 is a peripheral circle, 6 is a central circle, 7 is an integrated frame plate without a rotor motor mounting member in the peripheral circle, 8 is an integrated frame plate, 9 is a rotor motor mounting member, 10 is a protection plate, 11 is a rotor, 12 is a control module, 13 is a vertical support connecting rod, 14 is a foot rest, 15 is a power supply, 16 is a load bin, 17 is an upper protection plate, and 18 is a lower protection plate.
Detailed Description
Example 1: integrated plate-shaped laminated rack unmanned aerial vehicle with single-layer rotor wing and integrated rack plate comprising four peripheral circles
As shown in fig. 2-3 and 5-6, an integrated plate-shaped laminated frame unmanned aerial vehicle comprises an integrated frame plate 7 (shown in fig. 2) and a second integrated frame plate 8 (shown in fig. 3), wherein the first integrated frame plate is not provided with a rotor motor mounting member at the periphery, the second integrated frame plate is not provided with a horn, the integrated frame plate comprises a central circle 6 and four peripheral circles 5, the peripheral circles 5 are connected to the periphery of the central circle 6, and the integrated frame plates at all layers are fixedly connected through vertical support connecting rods 13 (shown in fig. 6); and a rotor motor mounting member 9 is arranged in the peripheral circle 5 of the second-layer integrated frame plate 8, and a motor and a rotor 11 are mounted on the rotor motor mounting member 9. A power supply 15 and a control module 12 are arranged in the central circle 6; the foot rest 14 is located below the integrated plate-like laminated frame. Install four rotors 11 between integration frame plate, constitute four rotor unmanned aerial vehicle.
A plurality of small holes 4 are formed in the integrated frame plate, and the vertical support connecting rod 13 is installed through the small holes 4. The small holes 4 on the integrated frame plate can reduce the weight of the integrated frame plate, improve the aerodynamic performance of the integrated frame plate, and can be used for installing the vertical support connecting rods 13. The vertical support connecting rod 13 is a slender rod, and two ends of the rod are fixed on the integrated frame plate through screws. All the vertical support connecting rods 13 are the same in length, and the length thereof can be adjusted according to the height of the rotor and the rotor driving motor. The central circle 6 is provided with a supporting structure, is a central part of the rack and is used for installing an unmanned aerial vehicle battery, a control module, a waterproof device and the like; four peripheral rings 5, connected to the central ring 6, provide support and protection for the rotor 11. The rotor motor mounting structure 9 performs the same function as the rotor mount 3 at the end of the horn (shown in figure 1) of the prior art.
Example 2: integrated plate-shaped laminated rack unmanned aerial vehicle with integrated rack plate with double rotor wings and four peripheral circles
As shown in fig. 2-5 and 7, an integrated plate-shaped laminated frame unmanned aerial vehicle comprises an integrated frame plate 7 (shown in fig. 2) with a first layer of peripheral circles not provided with a rotor motor mounting member, a second layer of integrated frame plate 8 (shown in fig. 3) and a protection plate 10 (shown in fig. 4), wherein no horn is provided, the integrated frame plate comprises a central circle 6 and four peripheral circles 5, the peripheral circles 5 are connected around the central circle 6, a rotor motor mounting member 9 is provided in the peripheral circle 5 of the second layer of integrated frame plate 8, and a motor and a rotor 11 are mounted on the rotor motor mounting member 9; the protection plate 10 comprises four arcs corresponding to the peripheral circles 5; the integrated frame plates of the layers and the second integrated frame plate 8 and the protective plate 10 of the second layer are fixedly connected through vertical support connecting rods 13 (as shown in fig. 7). A power supply 15 and a control module 12 are arranged in the central circle 6; the foot rest 14 is located below the integrated plate-like laminated frame. Four rotors 11 are installed between two-layer integration frame plate, and four rotors 11 are installed between second floor integration frame plate 8 and protection shield 10, constitute two-layer eight rotor unmanned aerial vehicle.
All be equipped with a plurality of apertures 4 on integrated frame board and the protection shield 10, vertical braces connecting rod 13 installs through aperture 4. The small holes 4 can reduce the weight of the integrated frame plate, improve the aerodynamic performance of the integrated frame plate, and can be used for installing the vertical support connecting rods 13. The vertical support connecting rod 13 is a slender rod, and two ends of the rod are fixed on the integrated frame plate and the protective plate 10 through screws. All the vertical support connecting rods 13 are the same in length, and the length thereof can be adjusted according to the height of the rotor and the rotor driving motor. The central circle 6 is provided with a supporting structure, is a central part of the rack and is used for installing an unmanned aerial vehicle battery, a control module, a waterproof device and the like; four peripheral rings 5, connected to the central ring 6, provide support and protection for the rotor 11. The rotor motor mounting structure 9 performs the same function as the rotor mount 3 at the end of the horn (shown in figure 1) of the prior art.
Example 3: integrated plate-shaped laminated rack unmanned aerial vehicle with four peripheral circles on integrated rack plate of four-layer rotor wing
As shown in fig. 2-5 and 8, an integrated plate-shaped laminated frame unmanned aerial vehicle comprises an integrated frame plate 7 (shown in fig. 2) with a first layer of periphery circle not provided with a rotor motor mounting member, a second layer of integrated frame plate 8 (shown in fig. 3), a third layer of integrated frame plate 8 (shown in fig. 3) and two layers of protection plates 10 (shown in fig. 4). The first layer of protection plate 10 is located between the second layer of integrated frame plate 8 and the third layer of integrated frame plate 8, the second layer of protection plate 10 is located below the third layer of integrated frame plate 8 (as shown in fig. 8), and has no horn, the integrated frame plate includes a central circle 6 and four peripheral circles 5, the peripheral circles 5 are connected around the central circle 6, the rotor motor mounting member 9 is arranged in the peripheral circles 5 of the second layer of integrated frame plate 8 and the third layer of integrated frame plate 8, and the motor and the rotor 11 are mounted on the rotor motor mounting member 9; the protection plate 10 comprises four arcs corresponding to the peripheral circles 5; the integrated frame plates or the protective plates of each layer are connected and fixed through vertical support connecting rods 13 (as shown in fig. 8). A power supply 15 and a control module 12 are arranged in the central circle 6; the foot rest 14 is located below the integrated plate-like laminated frame. Four rotors 11 are installed between integrated frame plate 7 and the second floor integration frame plate 8 that first floor periphery circle does not be equipped with rotor motor installation component, installs four rotors 11 between second floor integration frame plate 8 and first floor protection shield 10, installs four rotors 11 between first floor protection shield 10 and third floor integration frame plate 8, installs four rotors 11 between third floor integration frame plate 8 and second floor protection shield 10, constitutes four layers of sixteen rotor unmanned aerial vehicle.
All be equipped with a plurality of apertures 4 on integrated frame board and the protection shield 10, vertical braces connecting rod 13 installs through aperture 4. The small holes 4 can reduce the weight of the integrated frame plate, improve the aerodynamic performance of the integrated frame plate, and can be used for installing the vertical support connecting rods 13. The vertical support connecting rod 13 is a slender rod, and two ends of the rod are fixed on the integrated frame plate and the protective plate 10 through screws. All the vertical support connecting rods 13 are the same in length, and the length thereof can be adjusted according to the height of the rotor and the rotor driving motor. The central circle 6 is provided with a supporting structure, is a central part of the rack and is used for installing an unmanned aerial vehicle battery, a control module, a waterproof device and the like; four peripheral rings 5, connected to the central ring 6, provide support and protection for the rotor 11. The rotor motor mounting structure 9 performs the same function as the rotor mount 3 at the end of the horn (shown in figure 1) of the prior art.
Example 4: integrated plate-shaped laminated rack unmanned aerial vehicle with single-layer rotor wing and integrated rack plate containing six peripheral circles
As shown in fig. 6, 9-10 and 12, an integrated plate-shaped laminated frame unmanned aerial vehicle comprises an integrated frame plate 7 (shown in fig. 9) and a second integrated frame plate 8 (shown in fig. 10), wherein the first integrated frame plate is not provided with a rotor motor mounting member at the periphery, the second integrated frame plate is not provided with a horn, the integrated frame plate comprises a central circle 6 and six peripheral circles 5, the peripheral circles 5 are connected to the periphery of the central circle 6, and the integrated frame plates at all layers are fixedly connected through a vertical support connecting rod 13 (shown in fig. 6); and a rotor motor mounting member 9 is arranged in the peripheral circle 5 of the second-layer integrated frame plate 8, and a motor and a rotor are mounted on the rotor motor mounting member 9. A power supply 15 and a control module 12 are arranged in the central circle 6; the foot rest 14 is located below the integrated plate-like laminated frame. Six rotors 11 are installed between the integrated frame plate to form a six-rotor unmanned aerial vehicle.
A plurality of small holes 4 are formed in the integrated frame plate, and the vertical support connecting rod 13 is installed through the small holes 4. The small holes 4 on the integrated frame plate can reduce the weight of the integrated frame plate, improve the aerodynamic performance of the integrated frame plate, and can be used for installing the vertical support connecting rods 13. The vertical support connecting rod 13 is a slender rod, and two ends of the rod are fixed on the integrated frame plate through screws. All the vertical support connecting rods 13 are the same in length, and the length thereof can be adjusted according to the height of the rotor and the rotor driving motor. The central circle 6 is provided with a supporting structure, is a central part of the rack and is used for installing an unmanned aerial vehicle battery, a control module, a waterproof device and the like; six peripheral rings 5, connected to the central ring 6, provide support and protection for the rotor 11. The rotor motor mounting structure 9 performs the same function as the rotor mount 3 at the end of the horn (shown in figure 1) of the prior art.
Example 5: integrated plate-shaped laminated rack unmanned aerial vehicle with integrated rack plate with double rotor wings and six peripheral circles
As shown in fig. 7 and 9-12, an integrated plate-shaped laminated frame unmanned aerial vehicle comprises an integrated frame plate 7 (shown in fig. 9) with a first layer of peripheral circles not provided with a rotor motor mounting member, a second layer of integrated frame plate 8 (shown in fig. 10) and a protection plate 10 (shown in fig. 11), wherein no horn is provided, the integrated frame plate comprises a central circle 6 and six peripheral circles 5, the peripheral circles 5 are connected around the central circle 6, the rotor motor mounting member 9 is arranged in the peripheral circle 5 of the second layer of integrated frame plate 8, and a motor and a rotor 11 are mounted on the rotor motor mounting member 9; the protective plate 10 comprises six circular arcs corresponding to the peripheral circles 5; the integrated frame plates of the layers and the second integrated frame plate 8 and the protective plate 10 of the second layer are fixedly connected through vertical support connecting rods 13 (as shown in fig. 7). A power supply 15 and a control module 12 are arranged in the central circle 6; the foot rest 14 is located below the integrated plate-like laminated frame. Six rotor wings 11 are installed between two-layer integrated frame plate, six rotor wings 11 are installed between second layer integrated frame plate 8 and protection shield 10, constitute two-layer twelve-rotor unmanned aerial vehicle.
All be equipped with a plurality of apertures 4 on integrated frame board and the protection shield 10, vertical braces connecting rod 13 installs through aperture 4. The small holes 4 can reduce the weight of the integrated frame plate, improve the aerodynamic performance of the integrated frame plate, and can be used for installing the vertical support connecting rods 13. The vertical support connecting rod 13 is a slender rod, and two ends of the rod are fixed on the integrated frame plate and the protective plate 10 through screws. All the vertical support connecting rods 13 are the same in length, and the length thereof can be adjusted according to the height of the rotor and the rotor driving motor. The central circle 6 is provided with a supporting structure, is a central part of the rack and is used for installing an unmanned aerial vehicle battery, a control module, a waterproof device and the like; six peripheral rings 5, connected to the central ring 6, provide support and protection for the rotor 11. The rotor motor mounting structure 9 performs the same function as the rotor mount 3 at the end of the horn (shown in figure 1) of the prior art.
Example 6: integrated plate-shaped laminated rack unmanned aerial vehicle with four layers of rotor wings and integrated rack plate containing six peripheral circles
As shown in fig. 8-12, an integrated plate-shaped laminated frame unmanned aerial vehicle comprises an integrated frame plate 7 (shown in fig. 9) with a first layer of periphery circle not provided with a rotor motor mounting member, a second layer of integrated frame plate 8 (shown in fig. 10), a third layer of integrated frame plate 8 (shown in fig. 10) and two layers of protection plates 10 (shown in fig. 11). The first layer of protection plate 10 is located between the second layer of integrated frame plate 8 and the third layer of integrated frame plate 8, the second layer of protection plate 10 is located below the third layer of integrated frame plate 8 (as shown in fig. 8), and has no horn, the integrated frame plate comprises a central circle 6 and six peripheral circles 5, the peripheral circles 5 are connected around the central circle 6, a rotor motor mounting member 9 is arranged in the peripheral circles 5 of the second layer of integrated frame plate 8 and the third layer of integrated frame plate 8, and a motor and a rotor 11 are mounted on the rotor motor mounting member 9; the protective plate 10 comprises six circular arcs corresponding to the peripheral circles 5; the integrated frame plates or the protective plates of each layer are connected and fixed through vertical support connecting rods 13 (as shown in fig. 8). A power supply 15 and a control module 12 are arranged in the central circle 6; the foot rest 14 is located below the integrated plate-like laminated frame. Six rotors 11 are installed between the integrated frame plate 7 and the second layer integrated frame plate 8 of first layer periphery circle that is not equipped with rotor motor installation component, and six rotors 11 are installed between second layer integrated frame plate 8 and first layer protection shield 10, and six rotors 11 are installed between first layer protection shield 10 and third layer integrated frame plate 8, and six rotors 11 are installed between third layer integrated frame plate 8 and second layer protection shield 10, constitute four layers of twenty-four rotor unmanned aerial vehicle.
All be equipped with a plurality of apertures 4 on integrated frame board and the protection shield 10, vertical braces connecting rod 13 installs through aperture 4. The small holes 4 can reduce the weight of the integrated frame plate, improve the aerodynamic performance of the integrated frame plate, and can be used for installing the vertical support connecting rods 13. The vertical support connecting rod 13 is a slender rod, and two ends of the rod are fixed on the integrated frame plate and the protective plate 10 through screws. All the vertical support connecting rods 13 are the same in length, and the length thereof can be adjusted according to the height of the rotor and the rotor driving motor. The central circle 6 is provided with a supporting structure, is a central part of the rack and is used for installing an unmanned aerial vehicle battery, a control module, a waterproof device and the like; six peripheral rings 5, connected to the central ring 6, provide support and protection for the rotor 11. The rotor motor mounting structure 9 performs the same function as the rotor mount 3 at the end of the horn (shown in figure 1) of the prior art.
Example 7: integrated plate-shaped laminated rack unmanned aerial vehicle with single-layer rotor wing and integrated rack plate containing eight peripheral circles
As shown in fig. 6, 13-14 and 16, an integrated plate-shaped laminated frame unmanned aerial vehicle comprises an integrated frame plate 7 (as shown in fig. 13) and a second integrated frame plate 8 (as shown in fig. 14), wherein the first integrated frame plate is not provided with a rotor motor mounting member at the periphery, the second integrated frame plate is not provided with a horn, the integrated frame plate comprises a central circle 6 and eight peripheral circles 5, the peripheral circles 5 are connected to the periphery of the central circle 6, and the integrated frame plates at all layers are fixedly connected through a vertical support connecting rod 13 (as shown in fig. 6); and a rotor motor mounting member 9 is arranged in the peripheral circle 5 of the second-layer integrated frame plate 8, and a motor and a rotor are mounted on the rotor motor mounting member 9. A power supply 15 and a control module 12 are arranged in the central circle 6; the foot rest 14 is located below the integrated plate-like laminated frame. Install eight rotors 11 between integration frame plate, constitute eight rotor unmanned aerial vehicle.
A plurality of small holes 4 are formed in the integrated frame plate, and the vertical support connecting rod 13 is installed through the small holes 4. The small holes 4 on the integrated frame plate can reduce the weight of the integrated frame plate, improve the aerodynamic performance of the integrated frame plate, and can be used for installing the vertical support connecting rods 13. The vertical support connecting rod 13 is a slender rod, and two ends of the rod are fixed on the integrated frame plate through screws. All the vertical support connecting rods 13 are the same in length, and the length thereof can be adjusted according to the height of the rotor and the rotor driving motor. The central circle 6 is provided with a supporting structure, is a central part of the rack and is used for installing an unmanned aerial vehicle battery, a control module, a waterproof device and the like; eight outer circles 5, connected to the central circle 6, provide support and protection for the rotor 11. The rotor motor mounting structure 9 performs the same function as the rotor mount 3 at the end of the horn (shown in figure 1) of the prior art.
Example 8: integrated plate-shaped laminated rack unmanned aerial vehicle with integrated rack plate with double rotor wings and eight peripheral circles
As shown in fig. 7 and 13-16, an integrated plate-shaped laminated frame unmanned aerial vehicle comprises an integrated frame plate 7 (shown in fig. 13) with a first layer of peripheral circles not provided with a rotor motor mounting member, a second layer of integrated frame plate 8 (shown in fig. 14) and a protection plate 10 (shown in fig. 15), wherein no horn is provided, the integrated frame plate comprises a central circle 6 and eight peripheral circles 5, the peripheral circles 5 are connected around the central circle 6, a rotor motor mounting member 9 is arranged in the peripheral circle 5 of the second layer of integrated frame plate 8, and a motor and a rotor 11 are mounted on the rotor motor mounting member 9; the protection plate 10 comprises eight arcs corresponding to the peripheral circles 5; the integrated frame plates of the layers and the second integrated frame plate 8 and the protective plate 10 of the second layer are fixedly connected through vertical support connecting rods 13 (as shown in fig. 7). A power supply 15 and a control module 12 are arranged in the central circle 6; the foot rest 14 is located below the integrated plate-like laminated frame. Eight rotors 11 are installed between two-layer integration frame plate, install eight rotors 11 between second floor integration frame plate 8 and protection shield 10, constitute two-layer sixteen rotor unmanned aerial vehicle.
All be equipped with a plurality of apertures 4 on integrated frame board and the protection shield 10, vertical braces connecting rod 13 installs through aperture 4. The small holes 4 can reduce the weight of the integrated frame plate, improve the aerodynamic performance of the integrated frame plate, and can be used for installing the vertical support connecting rods 13. The vertical support connecting rod 13 is a slender rod, and two ends of the rod are fixed on the integrated frame plate and the protective plate 10 through screws. All the vertical support connecting rods 13 are the same in length, and the length thereof can be adjusted according to the height of the rotor and the rotor driving motor. The central circle 6 is provided with a supporting structure, is a central part of the rack and is used for installing an unmanned aerial vehicle battery, a control module, a waterproof device and the like; eight outer circles 5, connected to the central circle 6, provide support and protection for the rotor 11. The rotor motor mounting structure 9 performs the same function as the rotor mount 3 at the end of the horn (shown in figure 1) of the prior art.
Example 9: integrated plate-shaped laminated rack unmanned aerial vehicle with four layers of rotor wings and integrated rack plate containing eight peripheral circles
As shown in fig. 8 and 13-16, an integrated plate-shaped laminated frame unmanned aerial vehicle comprises an integrated frame plate 7 (shown in fig. 13) with a first layer of periphery circle not provided with a rotor motor mounting member, a second layer of integrated frame plate 8 (shown in fig. 14), a third layer of integrated frame plate 8 (shown in fig. 14) and two layers of protection plates 10 (shown in fig. 15). The first layer of protection plate 10 is located between the second layer of integrated frame plate 8 and the third layer of integrated frame plate 8, the second layer of protection plate 10 is located below the third layer of integrated frame plate 8 (as shown in fig. 8), and has no horn, the integrated frame plate comprises a central circle 6 and eight peripheral circles 5, the peripheral circles 5 are connected around the central circle 6, a rotor motor mounting member 9 is arranged in the peripheral circles 5 of the second layer of integrated frame plate 8 and the third layer of integrated frame plate 8, and a motor and a rotor 11 are mounted on the rotor motor mounting member 9; the protection plate 10 comprises eight arcs corresponding to the peripheral circles 5; the integrated frame plates or the protective plates of each layer are connected and fixed through vertical support connecting rods 13 (as shown in fig. 8). A power supply 15 and a control module 12 are arranged in the central circle 6; the foot rest 14 is located below the integrated plate-like laminated frame. Eight rotors 11 are installed between integrated frame plate 7 and the second floor integration frame plate 8 that first floor periphery circle does not be equipped with rotor motor installation component, installs eight rotors 11 between second floor integration frame plate 8 and first floor protection shield 10, installs eight rotors 11 between first floor protection shield 10 and third floor integration frame plate 8, installs eight rotors 11 between third floor integration frame plate 8 and second floor protection shield 10, constitutes four layers of thirty two rotor unmanned aerial vehicle.
All be equipped with a plurality of apertures 4 on integrated frame board and the protection shield 10, vertical braces connecting rod 13 installs through aperture 4. The small holes 4 can reduce the weight of the integrated frame plate, improve the aerodynamic performance of the integrated frame plate, and can be used for installing the vertical support connecting rods 13. The vertical support connecting rod 13 is a slender rod, and two ends of the rod are fixed on the integrated frame plate and the protective plate 10 through screws. All the vertical support connecting rods 13 are the same in length, and the length thereof can be adjusted according to the height of the rotor and the rotor driving motor. The central circle 6 is provided with a supporting structure, is a central part of the rack and is used for installing an unmanned aerial vehicle battery, a control module, a waterproof device and the like; eight outer circles 5, connected to the central circle 6, provide support and protection for the rotor 11. The rotor motor mounting structure 9 performs the same function as the rotor mount 3 at the end of the horn (shown in figure 1) of the prior art.
Example 10: integrated frame plate unmanned aerial vehicle containing six peripheral circles and provided with rotor motor installation members in central circle
As shown in fig. 17-21, an integral platy laminated frame unmanned aerial vehicle comprises an upper protective plate 17, an integral frame plate 8 and a lower protective plate 18, and is free of a horn. The integrated frame plate 8 (as shown in fig. 17) comprises a central circle 6 and six peripheral circles 5, the peripheral circles 5 are connected to the periphery of the central circle 6, the diameter of the central circle 6 is larger than that of the peripheral circles 5, rotor motor installation members 9 are arranged in the central circle 6 and the peripheral circles 5, a motor and a rotor 11 are installed on the rotor motor installation members 9, the rotor in the central circle 6 is a central rotor, and the diameter of the rotor is 1.5-3 times that of the rotor in the peripheral circles 5; the central rotor wings are in a pair and are arranged in an up-and-down symmetrical mode; the upper protection plate 17 (as shown in fig. 18) is in a circle structure corresponding to the central circle 6; the lower protection plate 18 (as shown in fig. 19) is in a circular arc structure corresponding to the outer circumference circle 5; the upper protection plate 17, the integrated frame plate 8 and the lower protection plate 18 are fixedly connected through a vertical support connecting rod 13 (as shown in fig. 21); the foot rest 14 is positioned below the integrated plate-shaped laminated frame; a load compartment 16 is integrated in the foot rest 14, and the control module 12 and power supply 15 are located within the load compartment 16. Install two central rotors on center circle 6 install a rotor in six periphery circles 5 respectively, constitute eight rotor unmanned aerial vehicle.
All be equipped with aperture 4 on upper shield 17, the integrated frame board 8 and the lower fender 18, vertical braces connecting rod 13 installs through aperture 4. The small holes 4 can reduce the weight of the integrated frame plate, improve the aerodynamic performance of the integrated frame plate, and can be used for installing the vertical support connecting rods 13. The vertical support connecting rod 13 is a slender rod, and two ends of the rod are fixed on the integrated frame plate and the upper and lower protection plates through screws. All the vertical support connecting rods 13 are the same in length, and the length thereof can be adjusted according to the height of the rotor and the rotor driving motor. Six peripheral rings 5, connected to the central ring 6, provide support and protection for the rotor 11. The rotor motor mounting structure 9 performs the same function as the rotor mount 3 at the end of the horn (shown in figure 1) of the prior art.
The above embodiments are not intended to be exhaustive or to limit the invention to other embodiments, and the above embodiments are intended to illustrate the invention and not to limit the scope of the invention, and all applications that can be modified from the invention are within the scope of the invention.
Claims (15)
1. An integrated plate-shaped laminated rack unmanned aerial vehicle is characterized in that the integrated plate-shaped laminated rack comprises at least two layers of integrated rack plates, each integrated rack plate comprises a central circle and an outer circle, the outer circles are connected to the periphery of the central circle, and the integrated rack plates of all layers are connected and fixed through vertical support connecting rods; a rotor motor mounting component is arranged in the peripheral circle, and a motor and a rotor are mounted on the rotor motor mounting component; a power supply and control module is arranged in the central circle; the foot rest is positioned below the integrated plate-shaped laminated frame.
2. The integrated plate-like laminated frame unmanned aerial vehicle of claim 1, wherein a peripheral circle of the topmost integrated frame plate is free of rotor motor mounting members.
3. The integrated plate-shaped laminated rack unmanned aerial vehicle according to claim 1 or 2, wherein the integrated rack plate is provided with a small hole, and the vertical support connecting rod is installed through the small hole.
4. The integral panel-like laminated rack unmanned aerial vehicle of claim 3, wherein the integral panel-like laminate comprises two integral frame plates, each of the upper and lower integral frame plates comprising a center circle and four outer circles, to form a quad-rotor unmanned aerial vehicle.
5. The integrated plate-shaped laminated rack unmanned aerial vehicle as claimed in claim 4, wherein a layer of protective plate is further arranged below the two layers of integrated rack plates; the protection plate comprises four circular arcs corresponding to the peripheral circles; a small hole is formed in the arc, and the vertical support connecting rod is installed through the small hole; four rotors are installed between two-layer integrated frame plate, four rotors are installed between lower floor integrated frame plate and protection shield, constitute two-layer eight rotor unmanned aerial vehicle.
6. The integral panel-like laminated rack unmanned aerial vehicle of claim 3, wherein the integral panel-like laminate comprises three integral frame panels, a first layer of protective panel is disposed between the second and third integral frame panels, and a second layer of protective panel is disposed below the third integral frame panel; each layer of integrated frame plate comprises a central circle and four peripheral circles; each layer of protection plate comprises four arcs corresponding to the peripheral circles; a small hole is formed in the arc, and the vertical support connecting rod is installed through the small hole; four rotors are respectively installed between the first layer of integrated frame plate and the second layer of integrated frame plate, between the second layer of integrated frame plate and the first layer of protection plate, between the first layer of protection plate and the third layer of integrated frame plate, and between the third layer of integrated frame plate and the second layer of protection plate, so that the four-layer sixteen-rotor unmanned aerial vehicle is formed.
7. The integral panel-like laminated rack unmanned aerial vehicle of claim 3, wherein the integral panel-like laminate comprises two layers of integral frame plates, each of the upper and lower layers of integral frame plates comprising one central circle and six peripheral circles, constituting a six-rotor unmanned aerial vehicle.
8. The integrated plate-shaped laminated rack unmanned aerial vehicle as claimed in claim 7, wherein a layer of protective plate is further arranged below the two layers of integrated rack plates; the protection plate comprises six circular arcs corresponding to the peripheral circles; a small hole is formed in the arc, and the vertical support connecting rod is installed through the small hole; six rotors are installed between the two layers of integrated frame plates, six rotors are installed between the lower layer of integrated frame plate and the protection plate, and the two layers of twelve-rotor unmanned aerial vehicles are formed.
9. The integral panel-like laminated rack unmanned aerial vehicle of claim 3, wherein the integral panel-like laminate comprises three integral frame panels, a first layer of protective panel is disposed between the second and third integral frame panels, and a second layer of protective panel is disposed below the third integral frame panel; each layer of integrated frame plate comprises a central circle and six peripheral circles; each layer of protection plate comprises six circular arcs corresponding to the peripheral circles; a small hole is formed in the arc, and the vertical support connecting rod is installed through the small hole; six rotors are respectively installed between the first layer of integrated frame plate and the second layer of integrated frame plate, between the second layer of integrated frame plate and the first layer of protection plate, between the first layer of protection plate and the third layer of integrated frame plate and between the third layer of integrated frame plate and the second layer of protection plate, so that the four-layer twenty-four rotor unmanned aerial vehicle is formed.
10. The integral panel-like laminated rack unmanned aerial vehicle of claim 3, wherein the integral panel-like laminate comprises two layers of integral frame plates, and each of the upper and lower layers of integral frame plates comprises one central circle and eight peripheral circles, thereby forming an eight-rotor unmanned aerial vehicle.
11. The integrated plate-shaped laminated rack unmanned aerial vehicle of claim 10, wherein a layer of protective plate is further arranged below the two layers of integrated rack plates; the protection plate comprises eight circular arcs corresponding to the peripheral circles; a small hole is formed in the arc, and the vertical support connecting rod is installed through the small hole; install eight rotors between two-layer integration frame plate, install eight rotors between lower floor integration frame plate and protection shield, constitute two-layer sixteen rotor unmanned aerial vehicle.
12. The integral panel-like laminated rack unmanned aerial vehicle of claim 3, wherein the integral panel-like laminate comprises three integral frame panels, a first layer of protective panel is disposed between the second and third integral frame panels, and a second layer of protective panel is disposed below the third integral frame panel; each layer of integrated frame plate comprises a central circle and eight peripheral circles; each layer of protection plate comprises eight arcs corresponding to the peripheral circles; a small hole is formed in the arc, and the vertical support connecting rod is installed through the small hole; eight rotors are respectively installed between the first layer of integrated frame plate and the second layer of integrated frame plate, between the second layer of integrated frame plate and the first layer of protection plate, between the first layer of protection plate and the third layer of integrated frame plate, and between the third layer of integrated frame plate and the second layer of protection plate, so that the four-layer thirty-two rotor unmanned aerial vehicle is formed.
13. An integrated plate-shaped laminated rack unmanned aerial vehicle is characterized in that the integrated plate-shaped laminated rack comprises an upper protection plate, an integrated rack plate and a lower protection plate, the integrated rack plate comprises a central circle and a peripheral circle, the peripheral circle is connected to the periphery of the central circle, the diameter of the central circle is larger than that of the peripheral circle, rotor motor installation members are arranged in the central circle and the peripheral circle, a motor and a rotor are installed on the rotor motor installation members, and the rotor in the central circle is a central rotor and the diameter of the rotor is larger than that of the rotor in the peripheral circle; the central rotor wings are in a pair and are arranged in an up-and-down symmetrical mode; the upper protective plate is in a circle structure corresponding to the central circle; the lower protective plate is of an arc structure corresponding to the peripheral circle; the upper protection plate, the integrated frame plate and the lower protection plate are fixedly connected through a vertical support connecting rod; the foot rest is positioned below the integrated platy stacked rack; the load bin is integrated in the foot rest, and the control module and the power supply are located in the load bin.
14. The integrated plate-like laminated frame unmanned aerial vehicle of claim 13, wherein the upper protective plate, the integrated frame plate and the lower protective plate are provided with small holes, and the vertical support connecting rod is installed through the small holes.
15. The integral panel-like laminated airframe drone of claim 14, wherein said integral airframe plate includes a center circle on which two center rotors are mounted and six outer circles in which one rotor is mounted, respectively, constituting an eight-rotor drone.
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Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103625640A (en) * | 2013-10-25 | 2014-03-12 | 南京航空航天大学 | Multi-rotor unmanned aerial vehicle |
| CN204197292U (en) * | 2014-08-07 | 2015-03-11 | 金卫红 | A kind of Multi-axis aircraft |
| WO2015135951A1 (en) * | 2014-03-12 | 2015-09-17 | G.A.M. Progetti Di Guzzardi Andrea E Guffanti Marco Snc | Rotating-wing drone, with intrinsically protective and accident prevention supporting structure |
| WO2015177376A1 (en) * | 2014-05-23 | 2015-11-26 | Airmovie S.R.L.S. | Mechanical structure for a multirotor unmanned aerial vehicle |
| CN106184733A (en) * | 2016-09-20 | 2016-12-07 | 上海交通大学附属中学闵行分校 | A kind of three-dimensional aircraft |
| CN106428540A (en) * | 2016-11-29 | 2017-02-22 | 四川特飞科技股份有限公司 | Combination duct aircraft, flight control system and method thereof |
| CN106585965A (en) * | 2016-12-30 | 2017-04-26 | 苏州曾智沃德智能科技有限公司 | Unmanned aerial vehicle used for highway surveying |
| CN108248852A (en) * | 2018-02-26 | 2018-07-06 | 天津中德应用技术大学 | Exerciser is passed through in unmanned plane racing |
| CN108263600A (en) * | 2016-12-30 | 2018-07-10 | 深圳光启空间技术有限公司 | Aircraft |
| CN108839792A (en) * | 2018-04-24 | 2018-11-20 | 江苏理工学院 | A kind of multi-rotor unmanned aerial vehicle |
| KR20200099233A (en) * | 2019-02-13 | 2020-08-24 | (주)이지시스템 | multi-copter type unmanned aerial vehicle using engine |
-
2021
- 2021-02-18 CN CN202110190453.5A patent/CN112874753A/en active Pending
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103625640A (en) * | 2013-10-25 | 2014-03-12 | 南京航空航天大学 | Multi-rotor unmanned aerial vehicle |
| WO2015135951A1 (en) * | 2014-03-12 | 2015-09-17 | G.A.M. Progetti Di Guzzardi Andrea E Guffanti Marco Snc | Rotating-wing drone, with intrinsically protective and accident prevention supporting structure |
| WO2015177376A1 (en) * | 2014-05-23 | 2015-11-26 | Airmovie S.R.L.S. | Mechanical structure for a multirotor unmanned aerial vehicle |
| CN204197292U (en) * | 2014-08-07 | 2015-03-11 | 金卫红 | A kind of Multi-axis aircraft |
| CN106184733A (en) * | 2016-09-20 | 2016-12-07 | 上海交通大学附属中学闵行分校 | A kind of three-dimensional aircraft |
| CN106428540A (en) * | 2016-11-29 | 2017-02-22 | 四川特飞科技股份有限公司 | Combination duct aircraft, flight control system and method thereof |
| CN106585965A (en) * | 2016-12-30 | 2017-04-26 | 苏州曾智沃德智能科技有限公司 | Unmanned aerial vehicle used for highway surveying |
| CN108263600A (en) * | 2016-12-30 | 2018-07-10 | 深圳光启空间技术有限公司 | Aircraft |
| CN108248852A (en) * | 2018-02-26 | 2018-07-06 | 天津中德应用技术大学 | Exerciser is passed through in unmanned plane racing |
| CN108839792A (en) * | 2018-04-24 | 2018-11-20 | 江苏理工学院 | A kind of multi-rotor unmanned aerial vehicle |
| KR20200099233A (en) * | 2019-02-13 | 2020-08-24 | (주)이지시스템 | multi-copter type unmanned aerial vehicle using engine |
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