CN218334302U - Retractable installation structure for GPS antenna of unmanned aerial vehicle - Google Patents
Retractable installation structure for GPS antenna of unmanned aerial vehicle Download PDFInfo
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- CN218334302U CN218334302U CN202222971568.0U CN202222971568U CN218334302U CN 218334302 U CN218334302 U CN 218334302U CN 202222971568 U CN202222971568 U CN 202222971568U CN 218334302 U CN218334302 U CN 218334302U
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a retractable installation structure of an unmanned aerial vehicle GPS antenna, wherein an antenna structure is arranged at the top of a fixed structure; the fixing structure comprises a fixing base, a mounting groove, a communicating groove, an inserting rod, a rotating button, a signal transmitter, a fixing nail and a gasket, wherein the mounting groove is formed in the top of the fixing base, the communicating groove is formed in the outer side of the fixing base, the inserting rod is arranged in the communicating groove, the rotating button is arranged on the outer side of the inserting rod, the signal transmitter is arranged at the bottom of the fixing base, the fixing nail is arranged at each of four corners of the bottom of the fixing base, and the gasket is arranged around the fixing nail; the antenna structure comprises a mounting seat, a supporting seat, a connecting seat and a signal antenna, wherein the supporting seat is arranged at the top of the mounting seat, the connecting seat is arranged at the top of the supporting seat, the signal antenna is arranged at the top of the connecting seat, and the antenna structure is simple in structure, convenient to use and high in practicability.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle GPS antenna retractable mounting structure.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civilian applications. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industrial application are really just needed by the unmanned aerial vehicle; the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand the industrial application and develop the unmanned aerial vehicle technology.
Present unmanned aerial vehicle needs the GPS antenna to receive and controls the signal, and the antenna generally all is direct to be installed together with unmanned aerial vehicle, when not using, the in-process that unmanned aerial vehicle deposited leads to antenna bending or rupture very easily to the influence is to unmanned aerial vehicle's controlling, consequently needs an unmanned aerial vehicle GPS antenna can receive and release mounting structure in order to change above-mentioned technical defect.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle GPS antenna retractable mounting structure to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme:
a retractable installation structure of an unmanned aerial vehicle GPS antenna comprises a fixing structure and an antenna structure, wherein the antenna structure is arranged at the top of the fixing structure;
the fixing structure comprises a fixing base, a mounting groove, a communicating groove, an inserting rod, a rotating button, a signal transmitter, a fixing nail and a gasket, wherein the mounting groove is formed in the top of the fixing base, the communicating groove is formed in the outer side of the fixing base, the inserting rod is arranged in the communicating groove, the rotating button is arranged on the outer side of the inserting rod, the signal transmitter is arranged at the bottom of the fixing base, the fixing nail is arranged at each of four corners of the bottom of the fixing base, and the gasket is arranged around the fixing nail;
the antenna structure comprises an installation seat, a supporting seat, a connecting seat and a signal antenna, wherein the supporting seat is arranged at the top of the installation seat, the connecting seat is arranged at the top of the supporting seat, and the signal antenna is arranged at the top of the connecting seat.
As the utility model discloses preferred scheme, the inside of mounting groove is equipped with the signal reception mouth, be equipped with anodal magnet around the signal reception mouth.
As the utility model discloses preferred scheme, the inserting groove has been seted up in the outside of mount pad, the bottom of mount pad is equipped with the signal transmission mouth, be equipped with negative pole magnet around the signal transmission mouth.
As the utility model discloses preferred scheme, the mount pad is pegged graft in the inside of mounting groove, the connecting rod runs through the intercommunication groove, and pegs graft in the inside of inserting groove.
Through adopting above-mentioned technical scheme, can fix the mount pad in the mounting groove to through the principle that anodal magnet and negative pole magnet opposite poles attract, firmly fix the mount pad in the mounting groove, and run through the intercommunication groove through the connecting rod and insert the inserting groove, carry out the secondary to the mount pad and fix, use at unmanned aerial vehicle and accomplish the back, can be very convenient dismantle the mount pad from the mounting groove.
As the utility model discloses preferred scheme, cooperate the use between negative pole magnet and the anodal magnet, cooperate the use between signal transmission mouth and the signal receiving mouth.
As the utility model discloses preferred scheme, wireless connection between signal antenna, signalling mouth, signal reception mouth and the signal transmission ware.
Through adopting above-mentioned technical scheme, can pass through the transmission of signal transmission mouth with signal antenna received signal to from the signal reception mouth receipt, with signal transmission to signal transmission ware in, thereby transmit control signal for unmanned aerial vehicle through signal transmission ware.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model discloses in, through the design of mount pad, can fix the mount pad in the mounting groove to through the principle that positive magnet and negative pole magnet opposite sex attracted, firmly fix the mount pad in the mounting groove, and run through the intercommunication groove through the connecting rod and insert the inserting groove, carry out the secondary to the mount pad and fix, use at unmanned aerial vehicle and accomplish the back, can be very convenient dismantle the mount pad from the mounting groove.
2. The utility model discloses in, through signal transmission ware's design, can pass through the signal transmission mouth transmission with signal antenna received signal to receive from the signal receiving mouth, with signal transmission to signal transmission ware in, thereby pass through signal transmission ware and give unmanned aerial vehicle with control signal transmission.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a bottom view of the fixing base of the present invention;
fig. 3 is a top view of the fixing base of the present invention.
Fig. 4 is the overall structure schematic diagram of the mounting seat of the present invention.
In the figure: 1-fixed structure, 11-fixed base, 12-mounting groove, 121-positive magnet, 122-signal receiving opening, 13-rotating button, 14-plug rod, 15-communicating groove, 16-fixing nail, 17-signal transmitter, 18-gasket, 2-antenna structure, 21-mounting seat, 211-negative magnet, 212-plug groove, 213-signal transmitting opening, 22-supporting seat, 23-connecting seat and 24-signal antenna.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below in conjunction with the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, rather than all embodiments, and all other embodiments obtained by a person of ordinary skill in the art without creative work belong to the scope of the present invention based on the embodiments of the present invention.
To facilitate understanding of the invention, several embodiments of the invention will be described below with reference to the accompanying drawings, but the invention can be implemented in many different forms and is not limited to the embodiments described herein, but rather these embodiments are provided to make the disclosure more thorough and comprehensive.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present, that when an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present, and that the terms "vertical", "horizontal", "left", "right" and the like are used herein for descriptive purposes only.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs, and the terms used herein in the specification of the present invention are for the purpose of describing particular embodiments only and are not intended to limit the present invention, and the term "and/or" as used herein includes any and all combinations of one or more of the associated listed items.
Referring to fig. 1-3, the present invention provides a technical solution:
a retractable installation structure of an unmanned aerial vehicle GPS antenna comprises a fixed structure 1 and an antenna structure 2, wherein the antenna structure 2 is arranged at the top of the fixed structure 1;
the fixing structure 1 comprises a fixing base 11, a mounting groove 12, a communicating groove 15, an inserting rod 14, a rotating button 13, a signal transmitter 17, a fixing nail 16 and a gasket 18, wherein the mounting groove 12 is formed in the top of the fixing base 11, the communicating groove 15 is formed in the outer side of the fixing base 11, the inserting rod 14 is arranged in the communicating groove 15, the rotating button 13 is arranged on the outer side of the inserting rod 14, the signal transmitter 17 is arranged at the bottom of the fixing base 11, the fixing nails 16 are arranged at four corners of the bottom of the fixing base 11, and the gasket 18 is arranged around the fixing nail 16;
In an embodiment, referring to fig. 1 and 3, a signal receiving opening 122 is disposed inside the mounting groove 12, and a positive magnet 121 is disposed around the signal receiving opening 122.
In an embodiment, referring to fig. 1 and 4, an insertion groove 212 is formed on an outer side of the mounting base 21, a signal emitting opening 213 is formed at a bottom of the mounting base 21, and a negative magnet 211 is disposed around the signal emitting opening 213.
Embodiment, please refer to fig. 1 and 4, mount pad 21 is pegged graft in the inside of mounting groove 12, the connecting rod runs through the intercommunication groove 15, and peg graft in the inside of inserting groove 212, through the design of mount pad 21, can fix mount pad 21 in mounting groove 12, and through the principle that anodal magnet 121 and negative pole magnet 211 opposite poles attract, firmly fix mount pad 21 in mounting groove 12, and run through intercommunication groove 15 and insert in inserting groove 212 through the connecting rod, carry out the secondary fixation to mount pad 21, after unmanned aerial vehicle uses the completion, can be very convenient dismantle mount pad 21 from mounting groove 12.
In an embodiment, referring to fig. 1, 3 and 4, the negative magnet 211 and the positive magnet 121 are used cooperatively, and the signal transmitting opening 213 and the signal receiving opening 122 are used cooperatively.
In an embodiment, referring to fig. 1 to 4, the signal antenna 24, the signal transmitting port 213, the signal receiving port 122 and the signal transmitter 17 are wirelessly connected, and by the design of the signal transmitter 17, a signal received by the signal antenna 24 can be transmitted through the signal transmitting port 213, received from the signal receiving port 122, and transmitted to the signal transmitter 17, so that a control signal is transmitted to the unmanned aerial vehicle through the signal transmitter 17.
The utility model discloses work flow: during the use, fix unable adjustment base 11 and unmanned aerial vehicle together through staple 16, gasket 18 can effectually prevent that unmanned aerial vehicle's shell from receiving too big pressure and leading to breaking, fix mount pad 21 in mounting groove 12, and through the principle that positive magnet 121 and negative magnet 211 opposite poles attract, firmly fix mount pad 21 in mounting groove 12, and run through intercommunication groove 15 through the connecting rod and insert in inserting groove 212, carry out the secondary to mount pad 21 and fix, the signal that signal antenna 24 received passes through the transmission of signal transmission mouth 213, and receive from signal receiving port 122, with signal transmission to signal transmitter 17 in, thereby pass through signal transmitter 17 and give unmanned aerial vehicle control signal transmission, after unmanned aerial vehicle uses the completion, dismantle mount pad 21 from mounting groove 12, this device simple structure, convenient to use and practicality are higher.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an unmanned aerial vehicle GPS antenna retractable mounting structure, includes fixed knot structure (1) and antenna structure (2), its characterized in that: the top of the fixed structure (1) is provided with an antenna structure (2);
the fixing structure (1) comprises a fixing base (11), a mounting groove (12), a communicating groove (15), an inserting rod (14), a rotating button (13), a signal transmitter (17), a fixing nail (16) and a gasket (18), wherein the mounting groove (12) is formed in the top of the fixing base (11), the communicating groove (15) is formed in the outer side of the fixing base (11), the inserting rod (14) is arranged in the communicating groove (15), the rotating button (13) is arranged on the outer side of the inserting rod (14), the signal transmitter (17) is arranged at the bottom of the fixing base (11), the fixing nail (16) is arranged at each of four corners of the bottom of the fixing base (11), and the gasket (18) is arranged around the fixing nail (16);
antenna structure (2) are including mount pad (21), supporting seat (22), connecting seat (23) and signal antenna (24), the top of mount pad (21) is equipped with supporting seat (22), the top of supporting seat (22) is equipped with connecting seat (23), the top of connecting seat (23) is equipped with signal antenna (24).
2. The retractable installation structure of unmanned aerial vehicle GPS antenna of claim 1, characterized in that: the mounting groove (12) is internally provided with a signal receiving opening (122), and the periphery of the signal receiving opening (122) is provided with a positive magnet (121).
3. The retractable installation structure of unmanned aerial vehicle GPS antenna of claim 1, characterized in that: the outer side of the mounting seat (21) is provided with a plug-in groove (212), the bottom of the mounting seat (21) is provided with a signal emitting opening (213), and the periphery of the signal emitting opening (213) is provided with a negative magnet (211).
4. The retractable mounting structure of unmanned aerial vehicle GPS antenna according to claim 1, characterized in that: the mounting seat (21) is inserted in the mounting groove (12), and the connecting rod penetrates through the communicating groove (15) and is inserted in the insertion groove (212).
5. The retractable installation structure of unmanned aerial vehicle GPS antenna of claim 3, characterized in that: the negative magnet (211) and the positive magnet (121) are matched for use, and the signal transmitting port (213) and the signal receiving port (122) are matched for use.
6. The retractable mounting structure of unmanned aerial vehicle GPS antenna according to claim 1, characterized in that: the signal antenna (24), the signal transmitting port (213), the signal receiving port (122) and the signal transmitter (17) are in wireless connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222971568.0U CN218334302U (en) | 2022-11-07 | 2022-11-07 | Retractable installation structure for GPS antenna of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222971568.0U CN218334302U (en) | 2022-11-07 | 2022-11-07 | Retractable installation structure for GPS antenna of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218334302U true CN218334302U (en) | 2023-01-17 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222971568.0U Active CN218334302U (en) | 2022-11-07 | 2022-11-07 | Retractable installation structure for GPS antenna of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218334302U (en) |
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2022
- 2022-11-07 CN CN202222971568.0U patent/CN218334302U/en active Active
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