CN209938956U - Conveniently dismantle wing-connected unmanned aerial vehicle of solar energy electroplax - Google Patents

Conveniently dismantle wing-connected unmanned aerial vehicle of solar energy electroplax Download PDF

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Publication number
CN209938956U
CN209938956U CN201920749409.1U CN201920749409U CN209938956U CN 209938956 U CN209938956 U CN 209938956U CN 201920749409 U CN201920749409 U CN 201920749409U CN 209938956 U CN209938956 U CN 209938956U
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China
Prior art keywords
wing
solar
aerial vehicle
unmanned aerial
electric
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Application number
CN201920749409.1U
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Chinese (zh)
Inventor
刘德山
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Wing Wing Flying (tianjin) Technology Co Ltd
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Wing Wing Flying (tianjin) Technology Co Ltd
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Priority to CN201920749409.1U priority Critical patent/CN209938956U/en
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Abstract

The utility model discloses a conveniently dismantle wing-connected unmanned aerial vehicle of solar energy electroplax, including the wing, the middle part of wing is provided with solar panel room, solar panel room includes the hypoplastron, upper plate and curb plate, there is the curb plate at the both ends of hypoplastron through electronic hinged joint, the middle part of hypoplastron is fixed with first electric putter through the screw level, first electric putter's both ends have second electric putter's one end through screw vertical fixation, second electric putter's the other end has the one end of dead lever through screw vertical fixation, the other end welded fastening of dead lever has the mounting panel, the top of mounting panel is fixed with solar cell panel through the screw, thereby can make solar cell panel can carry out simple and easy fixed, thereby can carry out convenient dismouting.

Description

Conveniently dismantle wing-connected unmanned aerial vehicle of solar energy electroplax
Technical Field
The utility model relates to an unmanned aerial vehicle's solar cell panel's dismouting technical field especially relates to a conveniently dismantle even wing unmanned aerial vehicle of solar energy electroplax.
Background
The solar cell panel on traditional even wing unmanned aerial vehicle all is fixed mounting on unmanned aerial vehicle wing or fuselage always, because prevent solar cell panel and break away from in the flight, solar cell panel all with wing, fuselage fixed very firm to make solar cell panel carry out the difficulty very of dismouting.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that has the solar cell panel dismouting difficulty on the unmanned aerial vehicle among the prior art, and the convenient company's of dismantling solar energy electroplax wing unmanned aerial vehicle who proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides a conveniently dismantle wing-connected unmanned aerial vehicle of solar energy electroplax, includes the wing, the middle part of wing is provided with solar panel room, and solar panel room includes hypoplastron, upper plate and curb plate, there is the curb plate at the both ends of hypoplastron through electronic hinged joint, and the middle part of hypoplastron is fixed with first electric putter through the screw level, and first electric putter's both ends have second electric putter's one end through screw vertical fixation, and second electric putter's the other end has the one end of dead lever through screw vertical fixation, and the other end welded fastening of dead lever has the mounting panel, and the top of mounting panel has solar cell panel through the screw fixation.
Preferably, the adjacent ends of the two first electric push rods in the middle of the lower plate are horizontally fixed through screws.
Preferably, the electric hinge is DJXD, and the rotation angle of the electric hinge is larger than 270 degrees.
Preferably, the solar cell panel is connected with the input end of the storage battery through a wire, and the storage battery is fixed inside the wing through a screw.
Preferably, the output end of the storage battery is connected with the first electric push rod and the second electric push rod through conducting wires.
The utility model has the advantages that:
1. the utility model discloses an arrange solar cell panel in the inside of wing to avoid solar cell panel and flight air current contact, thereby can make solar cell panel can carry out simple and easy fixed, thereby can carry out convenient dismouting.
2. The utility model discloses a first push rod motor extends toward the outside, stretches out solar cell panel room back completely when solar cell panel, and second push rod motor up extends, and second push rod motor drives the dead lever and up extends, then first push rod motor is retrieved to the inboard for solar cell panel is located the higher authority of upper plate, and solar cell panel can carry out the light energy electricity generation this moment, thereby can be normal realization solar cell panel charge.
To sum up, the utility model discloses only need carry out simple and easy installation with solar cell panel and fix and can satisfy flight and solar cell panel charging requirement, thereby can carry out the convenient dismouting of solar cell panel.
Drawings
Fig. 1 is a schematic structural view of a wing-connected unmanned aerial vehicle convenient for detaching a solar panel according to the present invention;
fig. 2 is a schematic structural view of a folded solar cell panel of the wing-connected unmanned aerial vehicle convenient for detaching the solar cell panel according to the present invention;
fig. 3 is the utility model provides a conveniently dismantle solar energy electroplax's even wing unmanned aerial vehicle's solar cell panel during operation schematic structure.
In the figure: the solar energy power generation system comprises 1 wing, 2 solar panel chambers, 3 solar panels, 4 mounting plates, 5 fixing rods, 6 second electric push rods, 7 first electric push rods, 8 storage batteries, 21 lower plates, 22 upper plates and 23 side plates.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
Referring to fig. 1-3, a wing-connected unmanned aerial vehicle convenient for detaching a solar panel comprises a wing 1, a solar panel chamber 2 is arranged in the middle of the wing 1, the solar panel chamber 2 comprises a lower plate 21, an upper plate 22 and side plates 23, the two ends of the lower plate 21 are connected with the side plates 23 through electric hinges, the electric hinges are DJXD in type, the rotation angle of the electric hinges is larger than 270 degrees, a first electric push rod 7 is horizontally fixed in the middle of the lower plate 21 through screws, one ends of the two adjacent first electric push rods 7 in the middle of the lower plate 21 are horizontally fixed through screws, one end of a second electric push rod 6 is vertically fixed at the two ends of the first electric push rod 7 through screws, one end of a fixing rod 5 is vertically fixed at the other end of the second electric push rod 6 through screws, a mounting plate 4 is welded and fixed at the other end of the fixing rod 5, a solar panel 3 is fixed at the, solar cell panel 3 passes through the wire and is connected with battery 8's input, and battery 8 passes through the fix with screw in the inside of wing 1, and battery 8's output passes through the wire and connects with first electric putter 7, second electric putter 6.
In this embodiment, unmanned aerial vehicle is when flying, and 3 shrink of solar cell panel are in solar cell panel room 2 to make solar cell panel 3 etc. do not influence unmanned aerial vehicle's flight, and unmanned aerial vehicle when flying, solar cell panel 3 is located the inside of wing 1, make flight in-process solar cell panel 3 not with the air current contact, consequently solar cell panel 3 can only fix through screw and mounting panel 4, thereby can realize very convenient dismouting of carrying on.
When unmanned aerial vehicle is in idle state, curb plate 23 is opened toward both sides through electronic hinge, electronic hinge is also supplied power by battery 8, make curb plate 23 both sides rotatory bottom to hypoplastron 21, then first push rod motor 7 extends toward the outside, stretch out solar cell panel room 2 back completely when solar cell panel 3, second push rod motor 6 extends up, second push rod motor 6 drives dead lever 5 and extends up, the bottom up to dead lever 5 flushes with the top of upper plate 22, first push rod motor 7 is retrieved to the inboard this moment, both ends up to upper plate 22 are close to first electric putter 6, and make solar cell panel 3 be located the higher authority of upper plate 22, solar cell panel 3 can carry out light energy power generation this moment, thereby realization solar cell panel's that can be normal charge.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims (5)

1. The utility model provides a conveniently dismantle wing-connected unmanned aerial vehicle of solar energy electroplax, includes wing (1), its characterized in that, the middle part of wing (1) is provided with solar panel room (2), and solar panel room (2) include hypoplastron (21), upper plate (22) and curb plate (23), there are curb plate (23) at the both ends of hypoplastron (21) through electronic hinged joint, and the middle part of hypoplastron (21) is fixed with first electric putter (7) through the screw level, and the both ends of first electric putter (7) are fixed with the one end of second electric putter (6) through the screw vertical fixation, and the other end of second electric putter (6) is fixed with the one end of dead lever (5) through the screw vertical fixation, and the other end welded fixation of dead lever (5) has mounting panel (4), and the top of mounting panel (4) is fixed with solar cell panel (3) through the screw.
2. The wing-connected unmanned aerial vehicle convenient for disassembling the solar electric board as claimed in claim 1, wherein one end of the lower board (21) adjacent to the two first electric push rods (7) is horizontally fixed by screws.
3. The wing-connected unmanned aerial vehicle for conveniently disassembling the solar electric board as claimed in claim 1, wherein the electric hinge is DJXD type, and the rotation angle of the electric hinge is larger than 270 °.
4. The wing-connected unmanned aerial vehicle convenient for disassembling the solar panel as claimed in claim 1, wherein the solar panel (3) is connected with the input end of the storage battery (8) through a wire, and the storage battery (8) is fixed inside the wing (1) through a screw.
5. The wing-connected unmanned aerial vehicle convenient for disassembling the solar electric board as claimed in claim 4, wherein the output end of the storage battery (8) is connected with the first electric push rod (7) and the second electric push rod (6) through wires.
CN201920749409.1U 2019-05-23 2019-05-23 Conveniently dismantle wing-connected unmanned aerial vehicle of solar energy electroplax Active CN209938956U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920749409.1U CN209938956U (en) 2019-05-23 2019-05-23 Conveniently dismantle wing-connected unmanned aerial vehicle of solar energy electroplax

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920749409.1U CN209938956U (en) 2019-05-23 2019-05-23 Conveniently dismantle wing-connected unmanned aerial vehicle of solar energy electroplax

Publications (1)

Publication Number Publication Date
CN209938956U true CN209938956U (en) 2020-01-14

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920749409.1U Active CN209938956U (en) 2019-05-23 2019-05-23 Conveniently dismantle wing-connected unmanned aerial vehicle of solar energy electroplax

Country Status (1)

Country Link
CN (1) CN209938956U (en)

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