CN114229022A - Oscillating bar device of unmanned aerial vehicle nest wing - Google Patents
Oscillating bar device of unmanned aerial vehicle nest wing Download PDFInfo
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- CN114229022A CN114229022A CN202111484282.3A CN202111484282A CN114229022A CN 114229022 A CN114229022 A CN 114229022A CN 202111484282 A CN202111484282 A CN 202111484282A CN 114229022 A CN114229022 A CN 114229022A
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- 229910000831 Steel Inorganic materials 0.000 claims description 20
- 239000010959 steel Substances 0.000 claims description 20
- 238000003825 pressing Methods 0.000 claims description 10
- 230000000149 penetrating effect Effects 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims 1
- 239000002994 raw material Substances 0.000 claims 1
- 230000003028 elevating effect Effects 0.000 description 7
- 238000000034 method Methods 0.000 description 6
- 238000012986 modification Methods 0.000 description 5
- 230000004048 modification Effects 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- 230000009471 action Effects 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 238000013461 design Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000011161 development Methods 0.000 description 2
- 238000006467 substitution reaction Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000003086 colorant Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D25/00—Details of other kinds or types of rigid or semi-rigid containers
- B65D25/02—Internal fittings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D81/00—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents
- B65D81/02—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage
- B65D81/05—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage maintaining contents at spaced relation from package walls, or from other contents
- B65D81/07—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage maintaining contents at spaced relation from package walls, or from other contents using resilient suspension means
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D85/00—Containers, packaging elements or packages, specially adapted for particular articles or materials
- B65D85/68—Containers, packaging elements or packages, specially adapted for particular articles or materials for machines, engines or vehicles in assembled or dismantled form
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention discloses a swing rod device of an unmanned aerial vehicle nest wing, which comprises a nest assembly, wherein the nest assembly comprises a nest, a lifting platform and a swing rod, the lifting platform and the swing rod are arranged in the nest, the swing rod is matched with the lifting platform, and an unmanned aerial vehicle is arranged on the lifting platform. The swing rod is driven to rotate through the lifting platform, the wings of the unmanned aerial vehicle swing to a reasonable range, and the unmanned aerial vehicle is convenient to carry a nest.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle nests, in particular to a swing rod device of an unmanned aerial vehicle nest wing.
Background
In the prior art, after unmanned aerial vehicle descends to the platform, the pendulum of wing to the angle uncontrollable, lead to when closing the top hatch door, in order not to damage unmanned aerial vehicle, the biggest overall dimension of box inner chamber size must wrap up unmanned aerial vehicle to the minimum one side size of machine nest appearance all obtains reaching 1.8 meters. Because the size of opening a door of the current general elevator does not have 1.8 meters, if a machine nest needs to enter the elevator, the size of opening the door of the elevator needs to be improved or other carrying modes are adopted, so that the elevator is inconvenient.
Disclosure of Invention
This section is for the purpose of summarizing some aspects of embodiments of the invention and to briefly introduce some preferred embodiments, and in this section as well as in the abstract and the title of the invention of this application some simplifications or omissions may be made to avoid obscuring the purpose of this section, the abstract and the title of the invention, and such simplifications or omissions are not intended to limit the scope of the invention.
The present invention has been made keeping in mind the above problems occurring in the prior art and/or the problems occurring in the prior art.
Therefore, the invention aims to solve the technical problem that the patent can solve the problem that the size of a nest is reduced so as to be convenient for entering a common elevator and be convenient to carry under the condition that the unmanned aerial vehicle is not damaged.
In order to solve the technical problems, the invention provides the following technical scheme: the utility model provides a pendulum rod device of unmanned aerial vehicle nest wing includes the nest subassembly, the nest subassembly includes nest, elevating platform and pendulum rod, the elevating platform with the pendulum rod set up in inside the nest, the pendulum rod with the elevating platform cooperation, unmanned aerial vehicle arranges in on the elevating platform.
As an optimized scheme of the swing rod device of the unmanned aerial vehicle nest wing, the invention comprises the following steps: the pendulum rod includes half gear and the body of rod, the body of rod set up in half gear side, the pendulum rod is provided with two.
As an optimized scheme of the swing rod device of the unmanned aerial vehicle nest wing, the invention comprises the following steps: the machine nest comprises a box body groove, a downward pressing rebound block and a swinging groove, the box body groove is formed in the machine nest, the downward pressing rebound block and the swinging groove are formed in the inner side face of the box body groove, and the downward pressing rebound block and the swinging groove are symmetrically arranged along the box body groove.
As an optimized scheme of the swing rod device of the unmanned aerial vehicle nest wing, the invention comprises the following steps: and a swing rod is arranged in the swing groove, and the half gear is arranged in the swing groove and is rotationally connected with the swing rod.
As an optimized scheme of the swing rod device of the unmanned aerial vehicle nest wing, the invention comprises the following steps: the machine nest further comprises an upper resilience block, the upper resilience block is arranged on the inner side face of the box body groove, a lifting auxiliary block is arranged on the lifting platform, a rack is arranged on the lifting auxiliary block, and the rack is meshed with the half gear.
As an optimized scheme of the swing rod device of the unmanned aerial vehicle nest wing, the invention comprises the following steps: the machine nest assembly further comprises an upper cover, a side sliding block is arranged on the machine nest, and the upper cover is connected with the side sliding block.
As an optimized scheme of the swing rod device of the unmanned aerial vehicle nest wing, the invention comprises the following steps: the machine nest further comprises a plurality of handles, the handles are arranged on the side faces of the machine nest and provided with a plurality of clamping grooves, and the clamping grooves are symmetrically arranged along the central line of the machine nest.
As an optimized scheme of the swing rod device of the unmanned aerial vehicle nest wing, the invention comprises the following steps: the side surface sliding block comprises a sliding groove and a side surface limiting block, the sliding groove is arranged on the side surface of the side surface sliding block in a penetrating mode, and the side surface limiting block is arranged inside the sliding groove;
the side surface sliding block further comprises a first connecting rope hole and a square groove, the first connecting rope hole is formed in the upper end of the sliding groove and communicated with the box body groove, and the square groove is formed in the lower end of the side surface sliding block and communicated with the box body groove;
the side slider still includes second connecting rope hole and side movable pulley, the second connecting rope hole set up in the sliding tray lower extreme and with square groove communicates with each other, the side movable pulley set up in inside the square groove, the side movable pulley is provided with two.
As an optimized scheme of the swing rod device of the unmanned aerial vehicle nest wing, the invention comprises the following steps: the box body grooves are provided with two box body grooves symmetrically along the central line of the box body grooves, and box body pulleys are arranged in the box body grooves;
the lower end of the upper cover is provided with a clamping column, a sliding column is arranged on the clamping column, the sliding column is arranged in the sliding groove, and the clamping column is arranged in the clamping groove.
As an optimized scheme of the swing rod device of the unmanned aerial vehicle nest wing, the invention comprises the following steps: the lifting platform is provided with a plurality of lifting connecting blocks, and the lifting connecting blocks are connected with the sliding columns through steel wire ropes;
the elevating platform lower extreme still is provided with electronic flexible post, the lift of electronic flexible post control elevating platform, be provided with the spacing hole in center on the stopper of side.
The invention has the beneficial effects that: the swing rod is driven to rotate through the lifting platform, the wings of the unmanned aerial vehicle swing to a reasonable range, and the unmanned aerial vehicle is convenient to carry a nest.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without inventive exercise. Wherein:
fig. 1 is a schematic view of an assembly structure of a swing link device of an unmanned aerial vehicle airframe wing according to an embodiment of the present invention;
fig. 2 is a schematic structural diagram of a swing link device assembly of an unmanned aerial vehicle nest wing according to an embodiment of the present invention;
fig. 3 is a schematic view of a connection structure of a part of components in a swing link device of an unmanned aerial vehicle airframe wing according to an embodiment of the present invention;
fig. 4 is a schematic view of a connection cross-section structure of components in a swing link device of an unmanned aerial vehicle nest wing according to an embodiment of the present invention;
fig. 5 is a schematic cross-sectional view illustrating a part of components in a swing link device of an unmanned aerial vehicle airframe wing according to an embodiment of the present invention;
fig. 6 is a schematic structural view of a cross section of a drone nest in a pendulum device of a drone nest wing according to an embodiment of the present invention.
Detailed Description
In order to make the aforementioned objects, features and advantages of the present invention comprehensible, embodiments accompanied with figures are described in detail below.
In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, but the present invention may be practiced in other ways than those specifically described and will be readily apparent to those of ordinary skill in the art without departing from the spirit of the present invention, and therefore the present invention is not limited to the specific embodiments disclosed below.
Next, the present invention will be described in detail with reference to the drawings, wherein the cross-sectional views illustrating the structure of the device are not enlarged partially according to the general scale for convenience of illustration when describing the embodiments of the present invention, and the drawings are only examples, which should not limit the scope of the present invention. In addition, the three-dimensional dimensions of length, width and depth should be included in the actual fabrication.
Further, reference herein to "one embodiment" or "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one implementation of the invention. The appearances of the phrase "in one embodiment" in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments.
Example 1
Referring to fig. 1 to 4, the present embodiment provides a swing link device for a wing of an unmanned aerial vehicle nest, including a nest assembly 100, the nest assembly 100 includes a nest 101, a lifting platform 103 and a swing link 106, the lifting platform 103 and the swing link 106 are disposed inside the nest 101, the swing link 106 is matched with the lifting platform 103, and an unmanned aerial vehicle 107 is disposed on the lifting platform 103.
The swing link 106 includes a half gear 106a and two rods 106b, the rods 106b are disposed on the side of the half gear 106a, and the two swing links 106 are disposed.
The nest 101 comprises a box body groove 101a, a lower pressing rebound block 101e and a swinging groove 101f, wherein the box body groove 101a is arranged on the nest 101, the lower pressing rebound block 101e and the swinging groove 101f are arranged on the inner side surface of the box body groove 101a, and the lower pressing rebound block 101e and the swinging groove 101f are symmetrically arranged in two along the box body groove 101 a.
The lower pressing rebound block 101e is provided with a spring fixedly connected with the bottom of the box body groove 101 a.
A swing rod 101f-1 is arranged in the swing groove 101f, a half gear 106a is arranged in the swing groove 101f and is connected with the swing rod 101f-1 in a rotating mode, and a connecting hole is formed in the half gear 106 a.
The nest 101 further comprises an upper rebound block 101g, the upper rebound block 101g is arranged on the inner side surface of the box body groove 101a, the lifting platform 103 is provided with a lifting auxiliary block 103c, the lifting auxiliary block 103c is provided with a rack 103c-1, and the rack 103c-1 is meshed with the half gear 106 a.
The upper rebound block 101g is provided with a spring which is fixedly connected with a convex block at the side of the machine nest 101.
The lower end of the lifting platform 103 is also provided with an electric telescopic column 103b, and the electric telescopic column 103b controls the lifting of the lifting platform 103.
When the lifting platform is used, the electric telescopic column 103b is started, the lifting platform 103 is lifted, the rack 103c-1 is meshed with the half gear 106a in the lifting process to drive the swing rod 106 to rotate downwards to extrude the push-down resilient block 101e, the swing rod 106 cannot rotate downwards all the time and only rotates to a certain angle as shown in fig. 4, the electric telescopic column 103b is closed after the lifting platform 103 is lifted to a certain position, and the swing rod 106 is restored to the horizontal state under the action of the push-down resilient block 101 e.
The unmanned aerial vehicle 107 stops on the lifting platform 103 after finishing working, at the moment, wings of the unmanned aerial vehicle 107 are in a random state, the rack 103c-1 and the half gear 106a are meshed to drive the swing rod 106 to rotate upwards in the descending process of the lifting platform 103, the swing rod 106 touches the wings and pushes the wings slowly in the upwards rotating process, the wings are swung to a proper position, the swing rod 106 squeezes the upper rebound block 101g at the moment, and therefore the wings cannot touch the nest 101 to damage the unmanned aerial vehicle in the descending process of the lifting platform 103.
After the unmanned aerial vehicle descends to a certain position, the rack 103c-1 is not meshed with the half gear 106a, and the swing rod 106 is restored to the horizontal state under the action of the upper rebound block 101g and the lower rebound block 101e, so that the problem that the size of the machine nest 101 is small under the state that the unmanned aerial vehicle is not damaged is solved, and the requirements of entering an elevator and carrying are met.
Example 2
Referring to fig. 1 to 6, a second embodiment of the present invention is provided, which is based on the previous embodiment, and this embodiment provides an implementation of a pendulum device for a drone airframe wing.
The nest assembly 100 comprises a nest 101, an upper cover 102 and a lifting platform 103, wherein a side sliding block 101c is arranged on the nest 101, the upper cover 102 is connected with the side sliding block 101c, and the lifting platform 103 is arranged inside the nest 101 and connected with the upper cover 102.
Two side sliders 101c are symmetrically arranged along the center line of the machine nest 101, and two upper covers 102 are arranged.
The nest 101 comprises a box body groove 101a and handles 101b, the box body groove 101a is arranged on the nest 101, the handles 101b are arranged on the side faces of the nest 101, and the handles 101b are provided with four handles which are convenient to lift and move the whole nest.
The side of the nest 101 is further provided with a plurality of engaging grooves 101d, and the engaging grooves 101d are symmetrically arranged along the nest 101.
The side surface sliding block 101c comprises a sliding groove 101c-1 and a side surface limiting block 101c-2, the sliding groove 101c-1 is arranged on the side surface of the side surface sliding block 101c in a penetrating mode, and the side surface limiting block 101c-2 is arranged inside the sliding groove 101 c-1.
The side surface slide block 101c further includes a first connecting rope hole 101c-3, and the first connecting rope hole 101c-3 is provided at the upper end of the slide groove 101c-1 and communicates with the case body groove 101 a.
The box groove 101a is provided with two box grooves 101a-1, the two box grooves 101a-1 are symmetrically arranged along the central line of the box groove 101a, the box groove 101a-1 is internally provided with a box pulley 101a-2, and the box pulley 101a-2 is convenient for the sliding of the steel wire rope 104.
The lower end of the upper cover 102 is provided with a clamping column 102a, the clamping column 102a is provided with a sliding column 102b, the sliding column 102b is arranged in the sliding groove 101c-1, and the clamping column 102a is arranged in the clamping groove 101 d.
The lifting platform 103 is provided with a plurality of lifting connecting blocks 103a, the lifting connecting blocks 103a are fixedly connected with the sliding column 102b through a steel wire rope 104, and two lifting connecting blocks 103a are respectively arranged on the upper surface and the lower surface of the lifting platform 103.
The lower end of the lifting platform 103 is also provided with an electric telescopic column 103b, the electric telescopic column 103b controls the lifting of the lifting platform 103, a central limiting hole 101c-21 is arranged on the side limiting block 101c-2, a spring is also arranged on the side limiting block 101c-2, and the other end of the spring is fixedly connected with the sliding groove 101 c-1.
The handle 101b is provided with a stopper 101b-1 for limiting the position of the upper cover 102 when the upper cover 102 slides on the side slider 101c, thereby ensuring the normal movement of the upper cover 102 in the sliding groove 101 c-1.
The sliding groove 101c-1 is provided with a curved groove 101c-11 near the upper end of the nest 101, and the sliding column 102b can turn over the upper cover 102 to cover the box body groove 101a when moving in the curved groove 101 c-11.
When the unmanned aerial vehicle nest 101 is not opened for use, the two upper covers 102 are positioned above the nest 101 to seal the nest 101, the sliding columns 102b in the sliding grooves 101c-1 extrude the side limiting blocks 101c-2, one ends of the steel wire ropes 104 penetrate through the central limiting holes 101c-21 to be fixedly connected with the sliding columns 102b, and the other ends of the steel wire ropes are fixedly connected with the lifting connecting blocks 103a to provide tension for the sliding columns 102 b.
When the nest 101 is opened, the electric telescopic column 103b is started to slowly rise, the sliding column 102b is gradually reduced by the tensile force of the steel wire rope 104, the sliding column 102b slowly moves in the sliding groove 101c-1 under the action of the side limiting block 101c-2, finally slowly slides to the bottom of the sliding groove 101c-1 under the limitation of the shielding block 101b-1, and at the moment, the electric telescopic column 103b extends to the highest point, and the unmanned aerial vehicle is started.
The machine nest 101 is closed, the electric telescopic column 103b is started to slowly descend, the sliding column 102b slowly ascends in the sliding groove 101c-1 under the pulling force of the steel wire rope 104, the steel wire rope 104 drives the box body pulley 101a-2 to slide on the box body pulley 101a-2 to reduce friction, and finally the original closed state is recovered.
This device is through the mode of mutual linkage, can open and close quick-witted nest 101 upper cover 102 in the lift unmanned aerial vehicle elevating platform 103, realizes long-range unmanned control in the use, has ensured the demand of unmanned aerial vehicle's work under the various harsh environment.
Example 3
Referring to fig. 1 to 6, the present invention provides three embodiments of an unmanned aerial vehicle airframe wing swing link device based on the previous embodiment.
The side slider 101c further includes a square groove 101c-4, and the square groove 101c-4 is provided at the lower end of the side slider 101c and communicates with the case groove 101 a.
The side sliding block 101c further comprises a second connecting rope hole 101c-5 and two side sliding wheels 101c-6, the second connecting rope hole 101c-5 is arranged at the lower end of the sliding groove 101c-1 and communicated with the square groove 101c-4, the side sliding wheels 101c-6 are arranged inside the square groove 101c-4, and the number of the side sliding wheels 101c-6 is two.
The lifting platform 103 is provided with a plurality of lifting connecting blocks 103a, the lifting connecting blocks 103a are fixedly connected with the sliding column 102b through a steel wire rope 104, and two lifting connecting blocks 103a are respectively arranged on the upper surface and the lower surface of the lifting platform 103.
The lifting connecting block 103a positioned at the lower end of the lifting platform 103 is fixedly connected with one end of a second steel wire rope 105, the other end of the second steel wire rope 105 and the sliding column 102b penetrate through the square groove 101c-4 and the second connecting rope hole 101c-5 to be fixedly connected with the sliding column 102b, and the second steel wire rope 105 is attached to the two side sliding wheels 101c-6 in the square groove 101c-4, so that the friction force generated when the second steel wire rope 105 moves is reduced.
When the machine nest 101 is opened to start the electric telescopic column 103b to slowly rise, the sliding column 102b is gradually reduced by the tensile force of the steel wire rope 104 and gradually increased by the tensile force of the second steel wire rope 105, the sliding column 102b slowly moves in the sliding groove 101c-1 under the action of the side limiting block 101c-2 and the second steel wire rope 105, and finally slowly slides to the bottom of the sliding groove 101c-1 under the limitation of the shielding block 101b-1, at the moment, the electric telescopic column 103b extends out of the highest point, and the unmanned aerial vehicle is started.
The machine nest 101 is closed, the electric telescopic column 103b is started to slowly descend, the sliding column 102b slowly ascends in the sliding groove 101c-1 under the pulling force of the steel wire rope 104, the second steel wire rope 105 does not generate force on the sliding column 102b at the moment, the steel wire rope 104 drives the box body pulley 101a-2 to slide on the box body pulley 101a-2 to reduce friction, and finally the machine nest 101 is restored to the original closed state.
It is important to note that the construction and arrangement of the present application as shown in the various exemplary embodiments is illustrative only. Although only a few embodiments have been described in detail in this disclosure, those skilled in the art who review this disclosure will readily appreciate that many modifications are possible (e.g., variations in sizes, dimensions, structures, shapes and proportions of the various elements, values of parameters (e.g., temperatures, pressures, etc.), mounting arrangements, use of materials, colors, orientations, etc.) without materially departing from the novel teachings and advantages of the subject matter recited in this application. For example, elements shown as integrally formed may be constructed of multiple parts or elements, the position of elements may be reversed or otherwise varied, and the nature or number of discrete elements or positions may be altered or varied. Accordingly, all such modifications are intended to be included within the scope of this invention. The order or sequence of any process or method steps may be varied or re-sequenced according to alternative embodiments. In the claims, any means-plus-function clause is intended to cover the structures described herein as performing the recited function and not only structural equivalents but also equivalent structures. Other substitutions, modifications, changes and omissions may be made in the design, operating conditions and arrangement of the exemplary embodiments without departing from the scope of the present inventions. Therefore, the present invention is not limited to a particular embodiment, but extends to various modifications that nevertheless fall within the scope of the appended claims.
Moreover, in an effort to provide a concise description of the exemplary embodiments, all features of an actual implementation may not be described (i.e., those unrelated to the presently contemplated best mode of carrying out the invention, or those unrelated to enabling the invention).
It should be appreciated that in the development of any such actual implementation, as in any engineering or design project, numerous implementation-specific decisions may be made. Such a development effort might be complex and time consuming, but would nevertheless be a routine undertaking of design, fabrication, and manufacture for those of ordinary skill having the benefit of this disclosure, without undue experimentation.
It should be noted that the above-mentioned embodiments are only for illustrating the technical solutions of the present invention and not for limiting, and although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that modifications or equivalent substitutions may be made on the technical solutions of the present invention without departing from the spirit and scope of the technical solutions of the present invention, which should be covered by the claims of the present invention.
Claims (10)
1. The utility model provides a pendulum rod device of unmanned aerial vehicle machine nest wing which characterized in that: comprises the steps of (a) preparing a mixture of a plurality of raw materials,
the nest assembly (100) comprises a nest (101), a lifting platform (103) and a swing rod (106), wherein the lifting platform (103) and the swing rod (106) are arranged inside the nest (101), the swing rod (106) is matched with the lifting platform (103), and an unmanned aerial vehicle (107) is arranged on the lifting platform (103).
2. The pendulum device of an unmanned aerial vehicle nest wing of claim 1, characterized in that: the swing rod (106) comprises a half gear (106a) and a rod body (106b), the rod body (106b) is arranged on the side face of the half gear (106a), and the number of the swing rods (106) is two.
3. The pendulum device of an unmanned aerial vehicle nest wing of claim 2, characterized in that: the machine nest (101) comprises a box body groove (101a), a downward pressing rebound block (101e) and a swinging groove (101f), the box body groove (101a) is formed in the machine nest (101), the downward pressing rebound block (101e) and the swinging groove (101f) are formed in the inner side face of the box body groove (101a), and the downward pressing rebound block (101e) and the swinging groove (101f) are symmetrically arranged along the box body groove (101 a).
4. The pendulum device of unmanned aerial vehicle nest wing of claim 3, characterized in that: a swing rod (101f-1) is arranged in the swing groove (101f), and the half gear (106a) is arranged in the swing groove (101f) and is rotationally connected with the swing rod (101 f-1).
5. The pendulum device of unmanned aerial vehicle nest wing of claim 4, characterized in that: the nest (101) further comprises an upper rebound block (101g), the upper rebound block (101g) is arranged on the inner side face of the box body groove (101a), a lifting auxiliary block (103c) is arranged on the lifting platform (103), a rack (103c-1) is arranged on the lifting auxiliary block (103c), and the rack (103c-1) is meshed with the half gear (106 a).
6. The device of claim 4 or 5, wherein: the nest assembly (100) further comprises an upper cover (102), a side sliding block (101c) is arranged on the nest (101), and the upper cover (102) is connected with the side sliding block (101 c).
7. The pendulum device of an unmanned aerial vehicle nest wing of claim 6, characterized in that: the nest (101) further comprises a handle (101b), the handle (101b) is arranged on the side face of the nest (101), the handle (101b) is provided with a plurality of clamping grooves (101d), and the clamping grooves (101d) are symmetrically arranged along the central line of the nest (101).
8. The pendulum device of an unmanned aerial vehicle nest wing of claim 7, characterized in that: the side surface sliding block (101c) comprises a sliding groove (101c-1) and a side surface limiting block (101c-2), the sliding groove (101c-1) is arranged on the side surface of the side surface sliding block (101c) in a penetrating mode, and the side surface limiting block (101c-2) is arranged inside the sliding groove (101 c-1);
the side sliding block (101c) further comprises a first connecting rope hole (101c-3) and a square groove (101c-4), the first connecting rope hole (101c-3) is arranged at the upper end of the sliding groove (101c-1) and communicated with the box body groove (101a), and the square groove (101c-4) is arranged at the lower end of the side sliding block (101c) and communicated with the box body groove (101 a);
the side sliding block (101c) further comprises a second connecting rope hole (101c-5) and two side sliding wheels (101c-6), the second connecting rope hole (101c-5) is formed in the lower end of the sliding groove (101c-1) and communicated with the square groove (101c-4), the side sliding wheels (101c-6) are arranged inside the square groove (101c-4), and the number of the side sliding wheels (101c-6) is two.
9. The pendulum device of an unmanned aerial vehicle nest wing of claim 8, wherein: two box grooves (101a-1) are arranged on the box groove (101a), the two box grooves (101a-1) are symmetrically arranged along the central line of the box groove (101a), and box pulleys (101a-2) are arranged in the box grooves (101 a-1);
the lower end of the upper cover (102) is provided with a clamping column (102a), the clamping column (102a) is provided with a sliding column (102b), the sliding column (102b) is arranged in the sliding groove (101c-1), and the clamping column (102a) is arranged in the clamping groove (101 d).
10. The pendulum device of an unmanned aerial vehicle nest wing of claim 9, wherein: a plurality of lifting connecting blocks (103a) are arranged on the lifting platform (103), and the lifting connecting blocks (103a) are connected with the sliding column (102b) through a steel wire rope (104);
the lower end of the lifting platform (103) is further provided with an electric telescopic column (103b), the electric telescopic column (103b) controls the lifting of the lifting platform (103), and a central limiting hole (101c-21) is formed in the side limiting block (101 c-2).
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Denomination of invention: A swinging rod device for swinging wings inside a drone nest Effective date of registration: 20231222 Granted publication date: 20230630 Pledgee: Societe Generale Bank Limited by Share Ltd. Guangzhou branch Pledgor: Guangzhou saihaoda Intelligent Technology Co.,Ltd. Registration number: Y2023980073611 |
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