CN205654965U - Advance air control valve assembly - Google Patents
Advance air control valve assembly Download PDFInfo
- Publication number
- CN205654965U CN205654965U CN201620483359.3U CN201620483359U CN205654965U CN 205654965 U CN205654965 U CN 205654965U CN 201620483359 U CN201620483359 U CN 201620483359U CN 205654965 U CN205654965 U CN 205654965U
- Authority
- CN
- China
- Prior art keywords
- heat dissipation
- base
- control valve
- valve assembly
- connecting plate
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Landscapes
- Safety Valves (AREA)
Abstract
The utility model discloses an advance air control valve assembly, including the valve body shell, the connecting plate be equipped with the through -hole on the surface, the bottom left and right sides of connecting plate all is equipped with the forked tail slide bar, the top of connecting plate is equipped with the heat dissipation base, the upper surface left and right sides of heat dissipation base all is equipped with the dovetail, the upper surface central point of heat dissipation base puts the circumference and is equipped with the heat dissipation through -hole, the inboard of heat dissipation through -hole is equipped with the protection network, the inner chamber central point of heat dissipation base puts and is equipped with rotary device, be equipped with rotating vane on rotary device's the outer wall. This advance air control valve assembly through dovetail and forked tail slide bar sliding connection, can be in the same place the connecting plate with heat dissipation base sliding connection, drive the rotating vane rotation through rotary device and can produce wind, keeps watch through heat dissipation through -hole and through -hole and distributes away, can be for valve body shell heat dissipation cooling at the advance air control valve assembly during operation.
Description
Technical field
This utility model relates to engine charge control valve technical field, is specially a kind of air intake control valve total
Become.
Background technology
UAV is called for short unmanned plane, is to utilize radio robot and the programme-control dress provided for oneself
Put the most manned aircraft of manipulation, without driving cabin on machine, but automatic pilot, presetting apparatus are installed
Deng equipment, on ground, naval vessels or machine tool remote control station personnel are by the equipment such as radar, it is tracked,
Location, remote control, remote measurement and Digital Transmission, can take off as conventional airplane under wireless remotecontrol or use
Booster rocket launches, it is possible to is taken to by machine tool and throws in flight in the air, during recovery, can use and commonly fly
The mode automatic Landing that machine landing mission is the same, it is possible to reclaimed by remote control parachute or block, can be anti-
Cover use repeatedly, be widely used in aerial reconnaissance, monitor, communicate, antisubmarine, electronic interferences etc., according to nothing
The requirement of man-machine driving, this product uses motor and miniature gear draw box mechanism to drive opening of throttle body
Degree, the aperture of position sensor detection simultaneously, use closed loop control to ensure unmanned plane driving safety and steadily,
And current air intake control valve assembly can produce the heat of many in the course of the work, heat can not be timely
Distribute, valve shell can be caused awfully hot, and affect service behaviour, and air intake control valve can be damaged
Assembly.
Utility model content
The purpose of this utility model is to provide a kind of air intake control valve assembly, to solve above-mentioned background technology
The problem of middle proposition.
For achieving the above object, this utility model following technical scheme of offer: a kind of air intake control valve assembly,
Including valve shell, the top of described valve shell is provided with lid, and before and after described valve shell, both sides are divided
Not being provided with motor and position sensor, the bottom of described valve shell is provided with base, described base
Bottom is provided with connecting plate, and the surface of described connecting plate is provided with through hole, about the bottom of described connecting plate two
Side is equipped with dovetail slide bar, and the top of described connecting plate is provided with heat dissipation base, the upper table of described heat dissipation base
The left and right sides, face is equipped with dovetail groove, and described dovetail groove is connected with dovetail sliding bar, described heat dissipation base
Upper surface center circumference be provided with thermal vias, the inner side of described thermal vias is provided with protection network, institute
The lumen centers position stating heat dissipation base is provided with rotary apparatus, and the outer wall of described rotary apparatus is provided with rotation
Blade.
Preferably, the bottom of described heat dissipation base is provided with buffering plate, and described buffering plate includes sliding tray,
The inner chamber bottom of described sliding tray is provided with spring, and the top of described spring is provided with buffer table, described buffer table
Being slidably connected with sliding tray, the top of described buffer table is provided with rubber slab.
Preferably, the bottom of described buffering plate is provided with protection base plate.
Preferably, described valve shell is provided with sealing strip with the junction of lid.
Preferably, described connecting plate is provided with fixed plate with the junction of base.
Compared with prior art, the beneficial effects of the utility model are: this air intake control valve assembly, pass through
Dovetail groove and dovetail sliding bar connect, connecting plate can be slidably connected with heat dissipation base together with, logical
Cross rotary apparatus be rotated blade rotate can produce wind, being kept watch by thermal vias and through hole is given out
Go, can give to valve shell radiating and cooling when air intake control valve assembly works, prevent valve shell
The too high performance affecting work of temperature, is possible to prevent air intake control valve assembly due to overheated and damage simultaneously.
Accompanying drawing explanation
Fig. 1 is this utility model structural representation;
Fig. 2 is heat dissipation base structural representation of the present utility model;
Fig. 3 is heat dissipation base internal structure schematic diagram of the present utility model;
Fig. 4 is buffer unit structure schematic diagram of the present utility model.
In figure: 1, position sensor, 2, valve shell, 3, lid, 4, sealing strip, 5, stepping electricity
Machine, 6, dovetail slide bar, 7, dovetail groove, 8, heat dissipation base, 9, buffering plate, 901, sliding tray,
902, spring, 903, buffer table, 904, rubber slab, 10, fixed plate, 11, base, 12, connect
Plate, 13, protection network, 14, thermal vias, 15, rotating vane, 16, rotary apparatus, 17, protection
Base plate, 18, through hole.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, to the technology in this utility model embodiment
Scheme is clearly and completely described, it is clear that described embodiment is only this utility model one
Divide embodiment rather than whole embodiments.Based on the embodiment in this utility model, this area is common
The every other embodiment that technical staff is obtained under not making creative work premise, broadly falls into this
The scope of utility model protection.
Fig. 1-4, a kind of technical scheme of this utility model offer: a kind of air intake control valve assembly, bag are provided
Including valve shell 2, the top of described valve shell 2 is provided with lid 3, described valve shell 2 and lid 3
Junction be provided with sealing strip 4, valve shell 2 can be made tighter with the connection of lid 3 by sealing strip 4
Close, it is respectively provided on two sides with motor 5 and position sensor 1, described valve before and after described valve shell 2
The bottom of body case 2 is provided with base 11, and the bottom of described base 11 is provided with connecting plate 12, described connection
Plate 12 is provided with fixed plate 10 with the junction of base 11, by fixed plate 10 can make connecting plate 12 with
The connection of base 11 is more firm, and the surface of described connecting plate 12 is provided with through hole 18, described connecting plate 12
The left and right sides, bottom be equipped with dovetail slide bar 6, the top of described connecting plate 12 is provided with heat dissipation base 8,
The upper surface left and right sides of described heat dissipation base 8 is equipped with dovetail groove 7, described dovetail groove 7 and dovetail slide bar
6 are slidably connected, and the upper surface center circumference of described heat dissipation base 8 is provided with thermal vias 14, described
The inner side of thermal vias 14 is provided with protection network 13, and the lumen centers position of described heat dissipation base 8 is provided with rotation
Device 16, the outer wall of described rotary apparatus 16 is provided with rotating vane 15, the end of described heat dissipation base 8
End is provided with buffering plate 9, and described buffering plate 9 includes sliding tray 901, the inner chamber of described sliding tray 901
Bottom is provided with spring 902, and the top of described spring 902 is provided with buffer table 903, described buffer table 903 with
Sliding tray 901 is slidably connected, and the top of described buffer table 903 is provided with rubber slab 904, when unmanned plane accelerates
With when slowing down, the buffering impulsive force to air intake control valve that can be suitable by buffering plate 9, anti-stop loss
Bad, the bottom of described buffering plate 9 is provided with protection base plate 17, is possible to prevent buffering by protection base plate 17
Base 9 damages.
During use, it is slidably connected by dovetail groove 7 and dovetail slide bar 6, can be connecting plate 12 with scattered
Hot base 8 is slidably connected together, blade 15 is rotated by rotary apparatus 16 and rotates and can produce
Wind, is kept watch distributed by thermal vias 14 and through hole 18, can when air intake control valve assembly works
To give to valve shell 2 radiating and cooling, prevent the too high performance affecting work of temperature of valve shell 2,
It is possible to prevent air intake control valve assembly due to overheated and damage simultaneously.
Embodiment the most of the present utility model, for the ordinary skill people of this area
For Yuan, it is possible to understand that can be real to these in the case of without departing from principle of the present utility model and spirit
Executing example to carry out multiple change, revise, replace and modification, scope of the present utility model is by claims
And equivalent limits.
Claims (5)
1. an air intake control valve assembly, including valve shell, it is characterised in that: described valve shell
Top is provided with lid, is respectively provided on two sides with motor and position sensor before and after described valve shell,
The bottom of described valve shell is provided with base, and the bottom of described base is provided with connecting plate, described connecting plate
Surface is provided with through hole, and the left and right sides, bottom of described connecting plate is equipped with dovetail slide bar, described connecting plate
Top be provided with heat dissipation base, the upper surface left and right sides of described heat dissipation base is equipped with dovetail groove, described
Dovetail groove is connected with dovetail sliding bar, and the upper surface center circumference of described heat dissipation base is provided with heat radiation
Through hole, the inner side of described thermal vias is provided with protection network, and the lumen centers position of described heat dissipation base is provided with
Rotary apparatus, the outer wall of described rotary apparatus is provided with rotating vane.
A kind of air intake control valve assembly the most according to claim 1, it is characterised in that: described heat radiation
The bottom of base is provided with buffering plate, and described buffering plate includes sliding tray, at the bottom of the inner chamber of described sliding tray
End is provided with spring, and the top of described spring is provided with buffer table, and described buffer table is slidably connected with sliding tray,
The top of described buffer table is provided with rubber slab.
A kind of air intake control valve assembly the most according to claim 2, it is characterised in that: described buffering
The bottom of base is provided with protection base plate.
A kind of air intake control valve assembly the most according to claim 1, it is characterised in that: described valve body
Shell is provided with sealing strip with the junction of lid.
A kind of air intake control valve assembly the most according to claim 1, it is characterised in that: described connection
Plate is provided with fixed plate with the junction of base.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201620483359.3U CN205654965U (en) | 2016-05-25 | 2016-05-25 | Advance air control valve assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201620483359.3U CN205654965U (en) | 2016-05-25 | 2016-05-25 | Advance air control valve assembly |
Publications (1)
Publication Number | Publication Date |
---|---|
CN205654965U true CN205654965U (en) | 2016-10-19 |
Family
ID=57405174
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201620483359.3U Expired - Fee Related CN205654965U (en) | 2016-05-25 | 2016-05-25 | Advance air control valve assembly |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN205654965U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110925472A (en) * | 2019-11-19 | 2020-03-27 | 张家港宏昌钢板有限公司 | Automatic blowdown device for heating furnace |
-
2016
- 2016-05-25 CN CN201620483359.3U patent/CN205654965U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110925472A (en) * | 2019-11-19 | 2020-03-27 | 张家港宏昌钢板有限公司 | Automatic blowdown device for heating furnace |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106428554B (en) | A kind of fixed-wing unmanned plane takes off and landing system and method | |
CN105756765B (en) | Unmanned vehicle engine cooling mechanism | |
RU2724006C1 (en) | Aircraft | |
CN204937514U (en) | A kind of unmanned plane with falling guard function | |
CN101332872A (en) | Multipurpose composite power unmanned air vehicle | |
CN108750101A (en) | A kind of super maneuver high speed compound unmanned rotary wing aircraft, assembly, assembly and disassembly methods | |
CN106275402B (en) | Detachable four paddles double-vane unmanned plane | |
CN106184741A (en) | A kind of flying wing type ducted fan VUAV | |
CN105129088B (en) | Spherical uniaxial rudder oriented intelligent aircraft | |
CN205654965U (en) | Advance air control valve assembly | |
CN204368432U (en) | A kind of can the animal-breeding rotary wind type unmanned plane of simultaneously spray disinfectant agent and liquid medicine | |
CN206243476U (en) | VTOL fixed-wing unmanned plane | |
CN108082400A (en) | Aerial photography aircraft airplane parking area waterborne | |
CN105035328B (en) | Hybrid-power flight vehicle | |
CN110316365A (en) | A kind of four axis unmanned plane of full-automatic fire-extinguishing | |
CN204078068U (en) | A kind of four-axle aircraft of overlength flying power | |
CN204368434U (en) | A kind of unmanned plane of band Dual Action camera of upper laying solar panel | |
CN206954510U (en) | It is a kind of can VTOL fixed-wing unmanned plane | |
CN207106925U (en) | A kind of unmanned plane camera fixing support | |
CN206092173U (en) | Orthostichous unmanned aerial vehicle engine | |
CN205652371U (en) | Unmanned aerial vehicle engine advances air control valve | |
CN207985228U (en) | A kind of novel unmanned plane of taking photo by plane | |
CN107512393A (en) | A kind of rapid vertical landing fixed-wing unmanned plane | |
CN209650571U (en) | The unmanned plane that can be used for replacing battery automatically independently rises and falls platform | |
CN201670359U (en) | Single-thrust-propeller disc-shaped unmanned aerial vehicle |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161019 Termination date: 20200525 |