CN210149541U - Unmanned aerial vehicle horn and connection fuselage - Google Patents
Unmanned aerial vehicle horn and connection fuselage Download PDFInfo
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- CN210149541U CN210149541U CN201920838652.0U CN201920838652U CN210149541U CN 210149541 U CN210149541 U CN 210149541U CN 201920838652 U CN201920838652 U CN 201920838652U CN 210149541 U CN210149541 U CN 210149541U
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- Prior art keywords
- unmanned aerial
- aerial vehicle
- horn
- fuselage
- accomodate
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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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
The utility model discloses an unmanned aerial vehicle horn and connecting fuselage, the unmanned aerial vehicle horn includes the horn body, horn body one end fixed connection frame, the horn body other end fixed connection limiting plate, frame inner wall fixed connection is provided with the motor storehouse of cavity, the motor storehouse sets up open-ended one end and passes through connecting piece connection cover plate, the hole has been seted up on the cover plate surface, the motor storehouse surface still fixed connection semiconductor refrigeration piece, semiconductor refrigeration piece cold junction contact motor storehouse surface, the unmanned aerial vehicle fuselage surface has been seted up and has been accomodate the groove, it is provided with the stopper to accomodate groove left and right sides symmetry, it still is provided with the mounting panel to accomodate the groove left and right sides, the spacing hole has been seted up on the mounting panel surface, the utility model discloses unmanned aerial vehicle can's unable carrying because of the size overlength of horn among the prior art, the not good problem of thermal diffusivity of, and can accomodate in the fuselage, be convenient for unmanned aerial vehicle's carrying.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially involves an unmanned aerial vehicle horn and connects fuselage.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by using a radio remote control device and a self-contained program control device, is a general name of unmanned aerial vehicles, and is originally applied to the military field. Along with the development and popularization of unmanned aerial vehicle technology, unmanned aerial vehicles have been widely applied to the fields of aerial photography, agriculture, forestry, surveying and mapping and the like.
Unmanned aerial vehicle includes the fuselage usually and outwards extends a plurality of horn from the fuselage, and the horn is kept away from and is set up one or more rotor blade on the end of fuselage, and this rotor blade's rotation can drive unmanned aerial vehicle flies, but, outwards extends the horn and rotor blade on it has increased unmanned aerial vehicle's volume, is unfavorable for portablely, and unmanned aerial vehicle drives rotor blade pivoted through the motor, and the motor can produce the heat at the pivoted in-process, if not in time stop flying, dispels the heat, can cause harm to unmanned aerial vehicle motor inside, makes it can't fly again, and this makes user's use experience not good, for this reason, the utility model discloses an unmanned aerial vehicle horn and connecting fuselage compares in prior art, and this unmanned aerial vehicle's horn can dispel the heat to the motor to can accomodate, portable.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to overcome prior art not enough, provide an unmanned aerial vehicle horn and connect fuselage to solve unmanned aerial vehicle among the prior art because the size overlength of horn can't carry, the not good technical problem of thermal diffusivity of motor, this unmanned aerial vehicle's horn can dispel the heat to the motor, and can accomodate, be convenient for unmanned aerial vehicle's carrying.
The utility model discloses a realize through following technical scheme: the utility model discloses an unmanned aerial vehicle horn, including the horn body, horn body one end fixed connection frame, horn body other end fixed connection limiting plate, frame inner wall fixed connection is provided with the motor storehouse of cavity, and the motor storehouse top is provided with the opening, and the motor storehouse sets up open-ended one end and passes through connecting piece connection cover plate, and the hole has been seted up on the cover plate surface, and the motor storehouse surface still fixed connection semiconductor refrigeration piece, semiconductor refrigeration piece cold junction contact motor storehouse surface;
the battery compartment has still been seted up on horn body surface, and battery compartment internally mounted has the battery, and the battery passes through wire electric connection semiconductor refrigeration piece, and the connection closing plate can be dismantled to the battery compartment.
This unmanned aerial vehicle wing during the use, the battery supplies power to the semiconductor refrigeration piece, semiconductor refrigeration piece one side is the cold junction, the another side is the hot junction, cold side and motor storehouse contact, the motor storehouse is made for the metal material that the heat conductivity is strong, install the motor in the motor storehouse, and make the inner wall contact in motor surface and motor storehouse, the mode that the semiconductor refrigeration piece passed through the heat transfer dispels the heat to the motor like this, to the hot junction of semiconductor refrigeration piece, unmanned aerial vehicle goes up the pivoted rotor blade and has certain radiating effect to the hot junction, unmanned aerial vehicle also has certain radiating effect at the in-process that removes.
Preferably, for the convenience of the use of the storage battery, the storage battery is provided with a power switch, a charging port is formed in the surface of the storage battery, a user can use the data line to supply power to the storage battery through the charging port, and the user can also control the power switch so as to control whether the storage battery supplies power to the semiconductor refrigeration piece.
Preferably, the surface of the sealing plate is provided with a notch corresponding to the charging port and the power switch.
Preferably, in order to realize the function of accomodating of horn body, the spout has been seted up to horn body front and back lateral wall symmetry.
Preferably, in order to fix the position of the horn body, two thread hole groups are formed on the surfaces of the two sliding grooves, each thread hole group comprises a thread hole, and the number of the thread holes in each thread hole group is not less than one.
The utility model also provides an unmanned aerial vehicle fuselage for install foretell unmanned aerial vehicle horn.
Preferably, the surface of the unmanned aerial vehicle body is provided with at least one accommodating groove, the left side wall and the right side wall of each accommodating groove are symmetrically provided with limiting blocks, the left side and the right side of each accommodating groove are also provided with mounting plates, the surface of each mounting plate is provided with at least one limiting hole, and a bolt penetrates through the limiting holes;
to the fuselage of unmanned aerial vehicle horn and use this horn body, four horns of an unmanned aerial vehicle fuselage installation, the stopper slides and imbeds in the spout, the horn body can be accomodate in accomodating the groove, and fix the position of horn body through the bolt, bolted connection screw thread punch combination is provided with two screw thread punch combinations on the spout, a screw thread punch combination is used for carrying on spacingly to the position of horn body under the horn body state of accomodating, another screw thread punch combination is used for carrying on spacingly to the position of horn body under the state of extending.
The utility model discloses an unmanned aerial vehicle horn and connect fuselage compares with prior art: the unmanned aerial vehicle horn of the utility model has the function of radiating the motor, one side of the semiconductor refrigeration piece is a cold end and the other side is a hot end in the power-on state, the cold end of the semiconductor refrigeration piece is in contact with the motor bin, and the semiconductor refrigeration piece radiates the motor in a heat transfer mode; and secondly, the utility model discloses an unmanned aerial vehicle horn can be accomodate in the groove of accomodating of unmanned aerial vehicle fuselage to carry on spacingly through the bolt, this unmanned aerial vehicle's horn can dispel the heat to the motor, and can accomodate, the unmanned aerial vehicle's of being convenient for carries.
Drawings
Fig. 1 is an external view of an arm of an unmanned aerial vehicle in embodiment 1;
fig. 2 is an exploded view of the arm of the unmanned aerial vehicle in embodiment 1;
fig. 3 is a side view of the fuselage of the drone in embodiment 1;
FIG. 4 is a schematic view of the mounting plate;
fig. 5 is an appearance schematic diagram of the arm of the unmanned aerial vehicle in embodiment 2.
In the figure: 1. a limiting plate; 2. a thread hole group; 3. a horn body; 4. a chute; 5. a frame; 6. a motor compartment; 7. a cover plate; 8. a semiconductor refrigeration sheet; 9. a battery compartment; 10. a sealing plate; 11. a storage battery; 12. a notch; 13. a charging port; 102. a receiving groove; 103. a limiting block; 104. a bolt; 105. mounting a plate; 106. and a limiting hole.
Detailed Description
The embodiments of the present invention will be described in detail below, and the present embodiment is implemented on the premise of the technical solution of the present invention, and a detailed implementation manner and a specific operation process are given, but the scope of the present invention is not limited to the following embodiments.
Example 1
the surface of the machine arm body 3 is also provided with a battery compartment 9, a storage battery 11 is arranged in the battery compartment 9, the storage battery 11 is electrically connected with the semiconductor refrigerating sheet 8 through a conducting wire, one end of a sealing plate 10 is rotatably connected with one end of the battery compartment 9 through a hinge, and the other end of the sealing plate 10 is fixedly connected with the other end of the battery compartment 9 through a buckle;
the storage battery 11 is provided with a power switch, the surface of the storage battery 11 is provided with a charging port 13, a user can use a data line to supply power to the storage battery through the charging port 13, and the user can control whether the storage battery 11 supplies power to the semiconductor refrigeration sheet 8 or not by controlling the power switch, and the surface of the sealing plate 10 is provided with a notch 12 corresponding to the charging port 13 and the power switch;
the front side wall and the rear side wall of the machine arm body 3 are symmetrically provided with sliding chutes 4, the surfaces of the two sliding chutes 4 are provided with two threaded hole groups 2, each threaded hole group 2 comprises a threaded hole, and the number of the threaded holes in each threaded hole group 2 is not less than one;
as shown in fig. 3, the utility model also provides an unmanned aerial vehicle fuselage for installing the above-mentioned unmanned aerial vehicle horn, the surface of the unmanned aerial vehicle fuselage is provided with a storage groove 102, the number of the storage groove 102 is not less than one, the left and right side walls of the storage groove 102 are symmetrically provided with stoppers 103, and the left and right sides of the storage groove 102 are also provided with mounting plates 105;
as shown in fig. 4, the mounting plate 105 has at least one limiting hole 106 formed in the surface thereof, and the bolt 104 passes through the limiting hole 106.
The embodiment discloses an unmanned aerial vehicle horn and a connecting body, when an unmanned aerial vehicle wing is used, a storage battery 11 supplies power to a semiconductor refrigeration sheet 8, one surface of the semiconductor refrigeration sheet 8 is a cold end, the other surface of the semiconductor refrigeration sheet is a hot end, the cold end is in contact with a motor cabin 6, the motor cabin 6 is made of a metal material with strong heat conductivity, a motor is arranged in the motor cabin 6, and the surface of the motor is in contact with the inner wall of the motor cabin 6, so that the semiconductor refrigeration sheet 8 radiates the heat of the motor in a heat transfer mode, for the hot end of the semiconductor refrigeration sheet, a rotary wing blade rotating on the unmanned aerial vehicle has a certain radiating effect on the hot end, the unmanned aerial vehicle also has a certain radiating effect in the moving process, for the unmanned aerial vehicle body, four horn are arranged on one unmanned aerial vehicle body, a limiting block 103 is embedded in a sliding groove 4 in a, and fix the position of horn body 3 through bolt 104, bolt 104 connects thread hole group 2, be provided with two thread hole groups 2 on the spout 4, a thread hole group 2 is used for carrying on spacingly to the position of horn body 3 under the state is accomodate to horn body 3, another thread hole group 2 is used for spacing the position of horn body 3 under the state is extended, this unmanned aerial vehicle's horn can dispel the heat to the motor to can accomodate, unmanned aerial vehicle's of being convenient for carries.
Example 2
the surface of the arm body 3 is also provided with a battery compartment 9, a storage battery 11 is arranged in the battery compartment 9, and the storage battery 11 is electrically connected with the semiconductor refrigerating sheet 8 through a conducting wire;
The embodiment 2 is different from the embodiment 1 in that a plurality of through holes (not labeled in the figure) are formed in the surface of the sealing plate 10, a cylinder (not labeled in the figure) with a threaded hole is arranged at the corner of the inner wall of the battery compartment 9, the sealing plate 10 is mounted on the arm body 3 through screws to seal the battery compartment 6, and the screws penetrate through the through holes in the sealing plate 10 to be connected with the cylinder with the threaded hole.
Claims (7)
1. An unmanned aerial vehicle horn comprises a horn body (3) and is characterized in that one end of the horn body (3) is fixedly connected with a frame (5), the other end of the horn body (3) is fixedly connected with a limiting plate (1), the inner wall of the frame (5) is fixedly connected with a motor bin (6) provided with a cavity, the top of the motor bin (6) is provided with an opening, one end of the motor bin (6) provided with the opening is connected with a cover plate (7) through a connecting piece, a hole is formed in the surface of the cover plate (7), the outer surface of the motor bin (6) is also fixedly connected with a semiconductor refrigerating sheet (8), and the cold end of the semiconductor refrigerating sheet (8) is in contact with the outer surface of the motor bin (;
the mechanical arm is characterized in that a battery compartment (9) is further formed in the surface of the mechanical arm body (3), a storage battery (11) is arranged inside the battery compartment (9), the storage battery (11) is electrically connected with the semiconductor refrigeration piece (8) through a wire, and the battery compartment (9) is detachably connected with the sealing plate (10).
2. An unmanned aerial vehicle arm as claimed in claim 1, wherein the battery (11) itself is provided with a power switch and the battery (11) surface is provided with a charging port (13).
3. The unmanned aerial vehicle horn of claim 2, wherein the sealing plate (10) surface is notched (12) in positions corresponding to the charging port (13) and the power switch.
4. The unmanned aerial vehicle horn of claim 1, characterized in that, the lateral wall symmetry has seted up spout (4) around horn body (3).
5. An unmanned aerial vehicle horn according to claim 4, wherein two screw hole groups (2) are formed on the surfaces of the two sliding grooves (4), the screw hole groups (2) comprise screw holes, and the number of the screw holes of the screw hole groups (2) is not less than one.
6. An unmanned aerial vehicle fuselage, characterized in that, the unmanned aerial vehicle fuselage installs the unmanned aerial vehicle horn of any one of claims 1 ~ 5.
7. The unmanned aerial vehicle fuselage of claim 6, characterized in that the unmanned aerial vehicle fuselage surface has been seted up and has been accomodate groove (102), the number of accomodating groove (102) is no less than one, it is provided with stopper (103) to accomodate groove (102) bilateral wall symmetry, it still is provided with mounting panel (105) to accomodate groove (102) left and right sides, spacing hole (106) have been seted up on mounting panel (105) surface, the number of spacing hole (106) is no less than one, and bolt (104) pass spacing hole (106).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920838652.0U CN210149541U (en) | 2019-06-05 | 2019-06-05 | Unmanned aerial vehicle horn and connection fuselage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920838652.0U CN210149541U (en) | 2019-06-05 | 2019-06-05 | Unmanned aerial vehicle horn and connection fuselage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210149541U true CN210149541U (en) | 2020-03-17 |
Family
ID=69761819
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920838652.0U Expired - Fee Related CN210149541U (en) | 2019-06-05 | 2019-06-05 | Unmanned aerial vehicle horn and connection fuselage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210149541U (en) |
-
2019
- 2019-06-05 CN CN201920838652.0U patent/CN210149541U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200317 Termination date: 20210605 |
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| CF01 | Termination of patent right due to non-payment of annual fee |