CN213705782U - Aircraft based on real-time monitoring - Google Patents
Aircraft based on real-time monitoring Download PDFInfo
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- CN213705782U CN213705782U CN202022874448.XU CN202022874448U CN213705782U CN 213705782 U CN213705782 U CN 213705782U CN 202022874448 U CN202022874448 U CN 202022874448U CN 213705782 U CN213705782 U CN 213705782U
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- subassembly
- fixed mounting
- host computer
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- camera
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Abstract
The utility model relates to an aircraft technical field just discloses an aircraft based on real-time supervision, this aircraft based on real-time supervision, including the host computer subassembly, the top of host computer subassembly is provided with the pilot lamp, there is the connecting rod that fixed mounting is located the host computer subassembly bottom the bottom of pilot lamp, the one end fixed mounting of connecting rod has rotatory thick liquid subassembly, there is the battery that fixed mounting is located the host computer subassembly inside one side of rotatory thick liquid subassembly. This aircraft based on real-time supervision through the setting of battery, utilizes the battery to carry out the electric power storage to the camera to realize that the aircraft can real-time supervision's purpose, through the setting of camera subassembly, utilize the activity of installation pole to cup joint at the surface of second fixing bolt, can adjust the angle of camera, make the scope of control enlarge, through the setting of installation board subassembly, make things convenient for the staff to dismantle and install the camera.
Description
Technical Field
The utility model relates to an aircraft technical field specifically is an aircraft based on real-time supervision.
Background
The aircraft is the apparatus that flies in the atmosphere or the space outside the atmosphere, is made by the mankind, can fly off ground, fly in the space and controlled by the people in the atmosphere or the apparatus flight thing of space flight outside the atmosphere, and there is unmanned aircraft that passes through remote control at present to be called unmanned aerial vehicle, and current aircraft based on real-time supervision can not real-time supervision, can not adjust the angle of camera, consequently needs an urgent need for an aircraft based on real-time supervision.
Disclosure of Invention
Technical problem to be solved
Not enough to prior art, the utility model provides an aircraft based on real-time supervision possesses can real-time supervision, can adjust advantages such as the angle of camera, has solved not can real-time supervision, can not adjust the problem of the angle of camera.
(II) technical scheme
Can real-time supervision for realizing the aforesaid, can adjust the purpose of the angle of camera, the utility model provides a following technical scheme: the utility model provides an aircraft based on real-time supervision, includes the host computer subassembly, the top of host computer subassembly is provided with the pilot lamp, there is the connecting rod that fixed mounting is located the host computer subassembly bottom the bottom of pilot lamp, the one end fixed mounting of connecting rod has rotatory thick liquid subassembly, there is the battery that fixed mounting is located the inside of host computer subassembly one side of rotatory thick liquid subassembly, there is the mounting panel subassembly that demountable installation is located the host computer subassembly bottom one side of battery, the bottom fixed mounting of mounting panel subassembly has camera subassembly, there is the transport case subassembly that fixed mounting is located the host computer subassembly bottom one side of camera subassembly.
Preferably, the host assembly comprises a host, the heat dissipation holes are formed in the outer surface of the host, one side of each heat dissipation hole is provided with a floor pole fixedly installed at the bottom of the host, and a buffering column is fixedly installed at the bottom of each floor pole.
The model of host computer is UX5, and the quantity of louvre has a plurality of, and the surface at the host computer is seted up evenly respectively to a plurality of louvre, and the quantity of floor pole has a plurality of, and fixed mounting is in the bottom of host computer respectively, and the surface of bumping post is provided with the rubber sleeve.
Preferably, the bottom of pilot lamp has the rotatory thick liquid subassembly of fixed mounting position in host computer subassembly one side, the bottom fixed mounting of pilot lamp has the battery, the bottom of pilot lamp has the camera subassembly of fixed mounting position in host computer subassembly bottom.
The model of the indicating lamp is AD16-22DS, and the material of indicating lamp is ya keli, and ya keli has good temperature toleration, and also is difficult for damaging simultaneously, and the battery fixed mounting is in the inner chamber bottom of host computer, and the model of battery is 6-QAW-54 a.
Preferably, the rotating paddle component comprises a first motor, a heat dissipation plate is arranged on one side of the first motor, a first rotating paddle located at the top of the first motor is movably sleeved on one side of the heat dissipation plate, and a second rotating paddle is movably sleeved on the top of the first rotating paddle.
The number of the rotary paddle components is four, the first motor is specifically a rotary motor, the type of the first motor is Y132S1-2, the first motor is used for driving the first rotary paddle and the second rotary paddle to rotate, the number of the heat dissipation plates is two, and the type of the heat dissipation plates is PGZB600 x 400.
Preferably, the mounting panel subassembly includes the mounting panel, first fixing bolt has been cup jointed in the inside activity of mounting panel, there is the second motor that fixed mounting is located the mounting panel bottom one side of first fixing bolt, the rotary rod has been cup jointed in the bottom activity of second motor, the bottom fixed mounting of rotary rod has the mounting groove.
A plurality of first fixing bolts are sleeved in the mounting plate in a movable mode, the type of each first fixing bolt is M5, the material is 304 stainless steel, the second motor is specifically a rotating motor, the type of the second motor is Y132S1-2, the rotating rods are driven to rotate, and the mounting grooves are provided with a plurality of numbers.
Preferably, the camera subassembly includes the fixed plate, the inside activity of fixed plate has cup jointed second fixing bolt, the surface activity of second fixing bolt has cup jointed the installation pole, the bottom fixed mounting of installation pole has the camera, the surface of camera is provided with the safety cover.
The quantity of fixed plate has a plurality of, and a plurality of fixed plate fixed mounting is in the inside of mounting groove, and the model of second fixing bolt is M5, and the material is 304 stainless steel, and the model of camera is HI3559V200, and the model of safety cover is TBQS-1, plays the effect of protection camera.
Preferably, the tote box subassembly includes the tote frame, one side fixed mounting of tote frame has the installation piece, there is the transport case that sliding connection is located the inside of tote frame one side of installation piece, the inner wall of transport case bonds and has the guard plate, there is the handle that the setting is located transport case one side in one side of guard plate.
The carrying frame is fixedly installed at the bottom of the host machine through the two installation blocks, the carrying box is rectangular, the protection plate is made of sponge, the sponge has good shock resistance and protection performance, the carrying frame plays a role in protecting carried articles, and the handle is made of aluminum alloy.
Compared with the prior art, the utility model provides an aircraft based on real-time supervision possesses following beneficial effect:
1. this aircraft based on real-time supervision, through the setting of battery, utilize the battery to carry out the electric power storage to the camera, thereby realize that the aircraft can real-time supervision's purpose, through the setting of camera subassembly, utilize the installation pole activity to cup joint the surface at second fixing bolt, can adjust the angle of camera, make the scope of control enlarge, through the setting of installation panel subassembly, utilize mounting panel and first fixing bolt with camera demountable installation in the bottom of host computer, thereby make things convenient for the staff to dismantle and install the camera.
2. This aircraft based on real-time supervision through the setting of host computer subassembly, utilizes the buffering post can play the cushioning effect when the aircraft falls to the ground, avoids the host computer to receive wearing and tearing, can effectual extension aircraft's life to reduce resource cost through the setting of rotatory thick liquid subassembly, utilizes the heating panel can carry out the work of dispelling the heat to first motor, has solved rotatory thick liquid and has received the problem of damage because of the high temperature.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of the main frame assembly of the present invention;
FIG. 3 is a schematic structural view of the rotary paddle assembly of the present invention;
FIG. 4 is a schematic structural view of the mounting plate assembly of the present invention;
fig. 5 is a schematic structural view of the camera assembly of the present invention;
fig. 6 is a schematic view of the structure of the carrying box assembly of the present invention.
Wherein: 1. a host component; 101. a host; 102. heat dissipation holes; 103. a floor pole; 104. a buffer column; 2. an indicator light; 3. a connecting rod; 4. a rotating paddle assembly; 401. a first motor; 402. a heat dissipation plate; 403. a first rotating paddle; 404. a second rotary paddle; 5. a storage battery; 6. mounting the plate assembly; 601. mounting a plate; 602. a first fixing bolt; 603. a second motor; 604. rotating the rod; 605. mounting grooves; 7. a camera assembly; 701. a fixing plate; 702. a second fixing bolt; 703. mounting a rod; 704. a camera; 705. a protective cover; 8. a tote assembly; 801. a carrying frame; 802. mounting blocks; 803. a tote box; 804. a protection plate; 805. a handle.
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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-6, an aircraft based on real-time monitoring comprises a host assembly 1, the host assembly 1 comprises a host 101, a heat dissipation hole 102 is formed in an outer surface of the host 101, a floor pole 103 fixedly installed at the bottom of the host 101 is arranged on one side of the heat dissipation hole 102, a buffer column 104 is fixedly installed at the bottom of the floor pole 103, an indicator light 2 is arranged at the top of the host assembly 1, a rotary paddle assembly 4 fixedly installed at one side of the host assembly 1 is arranged at the bottom of the indicator light 2, a storage battery 5 is fixedly installed at the bottom of the indicator light 2, a camera assembly 7 fixedly installed at the bottom of the host assembly 1 is arranged at the bottom of the indicator light 2, a connecting rod 3 fixedly installed at the bottom of the host assembly 1 is arranged at the bottom of the indicator light 2, a rotary paddle assembly 4 is fixedly installed at one end of the connecting rod 3, the rotary paddle assembly 4 comprises, one side of the heat dissipation plate 402 is movably sleeved with a first rotating paste 403 positioned at the top of a first motor 401, the top of the first rotating paste 403 is movably sleeved with a second rotating paste 404, one side of a rotating paste component 4 is fixedly provided with a storage battery 5 positioned in a host component 1, one side of the storage battery 5 is provided with a mounting plate component 6 detachably positioned at the bottom of the host component 1, the mounting plate component 6 comprises a mounting plate 601, the inside of the mounting plate 601 is movably sleeved with a first fixing bolt 602, one side of the first fixing bolt 602 is fixedly provided with a second motor 603 positioned at the bottom of the mounting plate 601, the bottom of the second motor 603 is movably sleeved with a rotating rod 604, the bottom of the rotating rod 604 is fixedly provided with a mounting groove 605, the bottom of the mounting plate component 6 is fixedly provided with a camera assembly 7, the camera assembly 7 comprises a fixing plate 701, the inside of the fixing plate 701, the installation rod 703 is sleeved on the outer surface of the second fixing bolt 702 in a movable mode, the camera 704 is fixedly installed at the bottom of the installation rod 703, the protective cover 705 is arranged on the outer surface of the camera 704, the carrying box assembly 8 fixedly installed at the bottom of the host assembly 1 is arranged on one side of the camera assembly 7, the carrying box assembly 8 comprises a carrying frame 801, an installation block 802 is fixedly installed on one side of the carrying frame 801, one side of the installation block 802 is provided with a carrying box 803 which is located inside the carrying frame 801 in a sliding connection mode, the protective plate 804 is bonded to the inner wall of the carrying box 803, and a handle 805 which is located on one side of the carrying box 803 is arranged on one side.
When using, generate electricity through battery 5 to host computer 101, utilize first motor 401 to drive first rotatory thick liquid 403 and the rotatory thick liquid 404 of second rotatory thick liquid rotatory to drive host computer 101 and take off, through the inside movable first fixing bolt 602 that cup joints of mounting panel 601, with rotary rod 604 demountable installation in the bottom of host computer 101, drive installation pole 703 through second motor 603 and rotate, thereby adjust the angle of camera 704, utilize transport box 803 of the inside sliding connection of transport frame 801, can carry the work to article.
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 (7)
1. An aircraft based on real-time monitoring, comprising a main machine component (1), characterized in that: the top of host computer subassembly (1) is provided with pilot lamp (2), there is connecting rod (3) that fixed mounting is located host computer subassembly (1) bottom the bottom of pilot lamp (2), the one end fixed mounting of connecting rod (3) has rotatory thick liquid subassembly (4), there is battery (5) that fixed mounting is located host computer subassembly (1) inside one side of rotatory thick liquid subassembly (4), there is mounting panel subassembly (6) that demountable installation is located host computer subassembly (1) bottom one side of battery (5), the bottom fixed mounting of mounting panel subassembly (6) has camera subassembly (7), there is transport case subassembly (8) that fixed mounting is located host computer subassembly (1) bottom one side of camera subassembly (7).
2. The real-time monitoring based aircraft according to claim 1, wherein: host computer subassembly (1) includes host computer (101), louvre (102) have been seted up to the surface of host computer (101), there is floor pole (103) that fixed mounting is located host computer (101) bottom one side of louvre (102), the bottom fixed mounting of floor pole (103) has cushion post (104).
3. The real-time monitoring based aircraft according to claim 1, wherein: the bottom of pilot lamp (2) has the rotatory thick liquid subassembly (4) that fixed mounting is located host computer subassembly (1) one side, the bottom fixed mounting of pilot lamp (2) has battery (5), the bottom of pilot lamp (2) has camera subassembly (7) that fixed mounting is located host computer subassembly (1) bottom.
4. The real-time monitoring based aircraft according to claim 1, wherein: rotatory thick liquid subassembly (4) include first motor (401), one side of first motor (401) is provided with heating panel (402), one side of heating panel (402) has the activity to cup joint first rotatory thick liquid (403) that are located first motor (401) top, the top activity of first rotatory thick liquid (403) is cup jointed the rotatory thick liquid of second (404).
5. The real-time monitoring based aircraft according to claim 1, wherein: mounting panel subassembly (6) are including mounting panel (601), first fixing bolt (602) have been cup jointed in the inside activity of mounting panel (601), there is second motor (603) that fixed mounting is located mounting panel (601) bottom one side of first fixing bolt (602), the bottom activity of second motor (603) has been cup jointed rotary rod (604), the bottom fixed mounting of rotary rod (604) has mounting groove (605).
6. The real-time monitoring based aircraft according to claim 1, wherein: camera subassembly (7) are including fixed plate (701), second fixing bolt (702) have been cup jointed in the inside activity of fixed plate (701), installation pole (703) have been cup jointed in the surface activity of second fixing bolt (702), the bottom fixed mounting of installation pole (703) has camera (704), the surface of camera (704) is provided with safety cover (705).
7. The real-time monitoring based aircraft according to claim 1, wherein: the tote box subassembly (8) is including tote box (801), one side fixed mounting of tote box (801) has installation piece (802), there is inside tote box (803) of sliding connection position in tote box (801) one side of installation piece (802), the inner wall of tote box (803) bonds and has guard plate (804), there is handle (805) that the setting is located tote box (803) one side in one side of guard plate (804).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022874448.XU CN213705782U (en) | 2020-12-04 | 2020-12-04 | Aircraft based on real-time monitoring |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022874448.XU CN213705782U (en) | 2020-12-04 | 2020-12-04 | Aircraft based on real-time monitoring |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213705782U true CN213705782U (en) | 2021-07-16 |
Family
ID=76786302
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022874448.XU Expired - Fee Related CN213705782U (en) | 2020-12-04 | 2020-12-04 | Aircraft based on real-time monitoring |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213705782U (en) |
-
2020
- 2020-12-04 CN CN202022874448.XU patent/CN213705782U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210716 Termination date: 20211204 |
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| CF01 | Termination of patent right due to non-payment of annual fee |