CN210971556U - Engine temperature regulating device and unmanned aerial vehicle with same - Google Patents
Engine temperature regulating device and unmanned aerial vehicle with same Download PDFInfo
- Publication number
- CN210971556U CN210971556U CN201921311717.2U CN201921311717U CN210971556U CN 210971556 U CN210971556 U CN 210971556U CN 201921311717 U CN201921311717 U CN 201921311717U CN 210971556 U CN210971556 U CN 210971556U
- Authority
- CN
- China
- Prior art keywords
- engine
- engine temperature
- inlet channel
- control device
- temperature control
- 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.)
- Active
Links
Images
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses an engine temperature regulating device and have its unmanned aerial vehicle, engine temperature regulating device include the fuselage, and the fuselage both sides all are provided with inlet channel, and inlet channel is located the engine front end, and inlet channel and the inside intercommunication of fuselage, inlet channel include the passageway board and rotate the main deep bead of being connected with the passageway board, and both ends are provided with upper and lower deep bead respectively about the main deep bead. This engine temperature regulating device can utilize the inlet channel to admit air and cool off the engine, need not additionally to dispose cooling system, simultaneously, utilizes relative passageway board pivoted main deep bead nimble control intake to control engine temperature avoids the engine temperature too high or low excessively, and the unmanned aerial vehicle who has this engine temperature regulating device then can fully cool off the advantage, improves the unmanned aerial vehicle performance.
Description
Technical Field
The utility model belongs to the technical field of the aircraft technique and specifically relates to an engine temperature regulating device and have its unmanned aerial vehicle is related to.
Background
Compared with the traditional gasoline engine, the heavy oil engine has the advantages of good durability, stronger load capacity, high cost performance, high safety and the like.
Due to the operating characteristics of heavy oil engines, the operating temperature thereof needs to be controlled within a specific range. If the working temperature of the engine is lower than the specified temperature range of the engine, the heavy oil is insufficiently combusted, and the working efficiency of the engine is reduced; if the working temperature of the engine is higher than the designated temperature range, the engine piston and the cylinder are excessively tightly matched, the inner wall of the cylinder is strained, and the service life of the engine is shortened.
SUMMERY OF THE UTILITY MODEL
To the above problem, the utility model provides an engine temperature regulating device and have its unmanned aerial vehicle, it can utilize the air current control engine temperature.
The utility model discloses a solve the technical scheme that its technical problem adopted and be:
the utility model provides an engine temperature regulating device, includes the fuselage, and the fuselage both sides all are provided with inlet channel, and inlet channel is located the engine front end, and inlet channel and the inside intercommunication of fuselage, inlet channel include the passageway board and rotate the main deep bead of being connected with the passageway board, and both ends are provided with upper and lower deep bead respectively about the main deep bead.
According to the utility model discloses an engine temperature regulating device of first aspect, go up the deep bead and the equal level setting of deep bead down, it is closed when main deep bead, main deep bead and passageway board smooth transition.
According to the utility model discloses an engine temperature regulating device of first aspect, the passageway board extends towards the inboard slant of fuselage along the course.
According to the utility model discloses an engine temperature regulating device of first aspect, the passageway board passes through the hinge and articulates with main wind shield.
According to the utility model discloses an aspect an engine temperature regulating device, the passageway inboard is provided with the mount pad, is provided with drive arrangement on the mount pad, and drive arrangement includes the steering wheel, is connected with first dwang on the steering wheel output, and first dwang articulates there is the second dwang, and the second dwang is articulated with the hinge.
According to the utility model discloses an engine temperature regulating device of first aspect, be the bulb between first dwang and the second dwang and connect, be the bulb between second dwang and the hinge and connect.
According to the utility model discloses an engine temperature regulating device, the steering wheel both sides are provided with the connecting plate, and the connecting plate passes through the right angle installation piece to be installed on the mount pad.
According to the utility model discloses the second aspect an unmanned aerial vehicle, include the utility model discloses the first aspect arbitrary engine temperature regulating device.
The utility model has the advantages that: the engine temperature control device can cool the engine by utilizing the air inlet of the air inlet channel without additionally configuring a cooling system. Simultaneously, utilize relative channel board pivoted main deep bead to control the intake in a flexible way to control engine temperature, avoid engine temperature too high or low excessively, and the unmanned aerial vehicle that has this engine temperature regulating device then can fully cool off the advantage, improve the unmanned aerial vehicle performance.
Drawings
In order to more clearly illustrate the technical solution in the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly described below. Obviously, the described figures are only some embodiments of the invention, not all embodiments, and other designs and figures can be obtained by those skilled in the art without inventive effort, based on these figures:
FIG. 1 is a first schematic structural diagram of a preferred embodiment of the present invention;
FIG. 2 is a second schematic structural diagram of the preferred embodiment of the present invention;
FIG. 3 is a first schematic structural view of the intake passage and the driving device according to the preferred embodiment of the present invention;
fig. 4 is a schematic structural diagram of an intake passage and a driving device according to a preferred embodiment of the present invention.
Detailed Description
The conception, the specific structure, and the technical effects produced by the present invention will be clearly and completely described below in conjunction with the embodiments and the accompanying drawings to fully understand the objects, the features, and the effects of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, and not all embodiments, and other embodiments obtained by those skilled in the art without inventive labor based on the embodiments of the present invention all belong to the protection scope of the present invention.
Referring to fig. 1 to 4, an engine temperature control device includes a body 100, air inlet channels 200 are disposed on both sides of the body 100, the air inlet channels 200 are located at the front end of an engine, the air inlet channels 200 are communicated with the interior of the body 100, the air inlet channels 200 include a channel plate 210 and a main wind shield 220 rotatably connected with the channel plate 210, an upper wind shield 230 is disposed at the upper end of the main wind shield 220, and a lower wind shield 240 is disposed at the lower end of the main wind shield 220.
Referring to fig. 3 and 4, the upper wind deflector 230 and the lower wind deflector 240 are horizontally disposed, and when the main wind deflector 220 is closed, the main wind deflector 220 and the channel plate 210 smoothly transition, and the main wind deflector 220 and the channel plate 210 form a complete channel wall surface.
Referring to fig. 1, the tunnel plate 210 extends diagonally toward the inside of the body 100 in a heading direction. Referring to fig. 3 and 4, the channel plate 210 is hinged to the main wind guard 220 by a hinge 300. The inboard mount pad 400 that is provided with of passageway board 210, be provided with drive arrangement 500 on the mount pad 400, drive arrangement 500 includes steering wheel 510, is connected with first dwang 520 on the steering wheel 510 output, and first dwang 520 articulates there is second dwang 530, and second dwang 530 articulates with hinge 300. Preferably, the first rotating rod 520 and the second rotating rod 530 are connected by a ball, and the second rotating rod 530 and the hinge 300 are connected by a ball.
Referring to fig. 3 and 4, the steering engine 510 is provided with connecting plates 540 at both sides thereof, and the connecting plates 540 are mounted on the mounting base 400 through right-angle mounting blocks 550.
When the main wind shield 220 is closed, the main wind shield 220 and the channel plate 210 are in smooth transition, the main wind shield 220 and the channel plate 210 form a complete channel wall surface, and the air inflow is small at the moment and is used for preventing the temperature of the engine from being too low; when the main wind shield 220 is rotated toward the inside of the body 100 by the driving device 500, the communication area of the intake passage 200 and the body 100 is increased, and the amount of intake air is increased for preventing the engine temperature from being excessively high.
The utility model discloses an unmanned aerial vehicle, preferably tail pushing-type unmanned aerial vehicle, this unmanned aerial vehicle includes the engine temperature regulating device in this embodiment. The unmanned aerial vehicle utilizes an engine temperature control device to control the temperature of an engine, in particular a heavy oil engine.
The above embodiments are further described in the above aspects of the present invention, but it should not be understood that the scope of the above subject matter of the present invention is limited to the above embodiments, and all the technologies realized based on the above aspects belong to the scope of the present invention.
Claims (8)
1. An engine temperature control device is characterized in that: including fuselage (100), fuselage (100) both sides all are provided with inlet channel (200), and inlet channel (200) are located the engine front end, and inlet channel (200) and fuselage (100) inside intercommunication, inlet channel (200) include passageway board (210) and main deep bead (220) of being connected with passageway board (210) rotation, and both ends are provided with upper and lower deep bead (230, 240) respectively about main deep bead (220).
2. The temperature control device of the engine according to claim 1, wherein: the upper wind shield plate (230) and the lower wind shield plate (240) are both horizontally arranged, and when the main wind shield plate (220) is closed, the main wind shield plate (220) and the channel plate (210) are in smooth transition.
3. An engine temperature control device according to claim 1 or 2, characterized in that: the channel plate (210) extends obliquely towards the inner side of the fuselage (100) along the heading direction.
4. The temperature control device of the engine according to claim 1, wherein: the channel plate (210) is hinged to the main wind deflector (220) by means of a hinge (300).
5. The temperature control device of an engine according to claim 1 or 4, wherein: the inner side of the channel plate (210) is provided with a mounting seat (400), the mounting seat (400) is provided with a driving device (500), the driving device (500) comprises a steering engine (510), the output end of the steering engine (510) is connected with a first rotating rod (520), the first rotating rod (520) is hinged to a second rotating rod (530), and the second rotating rod (530) is hinged to a hinge (300).
6. The temperature control device of the engine according to claim 5, wherein: be the bulb between first dwang (520) and the second dwang (530) and connect, be the bulb between second dwang (530) and hinge (300) and connect.
7. The temperature control device of the engine according to claim 5, wherein: connecting plates (540) are arranged on two sides of the steering engine (510), and the connecting plates (540) are installed on the installation seat (400) through right-angle installation blocks (550).
8. An unmanned aerial vehicle, its characterized in that: comprising an engine temperature control device as claimed in any one of claims 1 to 7.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921311717.2U CN210971556U (en) | 2019-08-13 | 2019-08-13 | Engine temperature regulating device and unmanned aerial vehicle with same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921311717.2U CN210971556U (en) | 2019-08-13 | 2019-08-13 | Engine temperature regulating device and unmanned aerial vehicle with same |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210971556U true CN210971556U (en) | 2020-07-10 |
Family
ID=71414807
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921311717.2U Active CN210971556U (en) | 2019-08-13 | 2019-08-13 | Engine temperature regulating device and unmanned aerial vehicle with same |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210971556U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113464262A (en) * | 2021-06-30 | 2021-10-01 | 航天时代飞鸿技术有限公司 | Temperature control device and control method of aviation piston engine for unmanned aerial vehicle |
| CN113513399A (en) * | 2021-05-26 | 2021-10-19 | 珠海天晴航空航天科技有限公司 | Aircraft engine and heat dissipation control method thereof |
-
2019
- 2019-08-13 CN CN201921311717.2U patent/CN210971556U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113513399A (en) * | 2021-05-26 | 2021-10-19 | 珠海天晴航空航天科技有限公司 | Aircraft engine and heat dissipation control method thereof |
| CN113464262A (en) * | 2021-06-30 | 2021-10-01 | 航天时代飞鸿技术有限公司 | Temperature control device and control method of aviation piston engine for unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN202935216U (en) | Fracturing pump vehicle driven by turbine engine | |
| CN210971556U (en) | Engine temperature regulating device and unmanned aerial vehicle with same | |
| CN202926404U (en) | Fracturing unit driven by turbine engine | |
| CN211617900U (en) | Truck dome | |
| CN202247770U (en) | Snow blowing device and snow remover | |
| CN205589317U (en) | Foldable additional rear of a vehicle | |
| CN107091231B (en) | A kind of air conditioning for automobiles Spiralism type motor compressor | |
| US9624818B2 (en) | Cooling apparatus of bus | |
| CN206781527U (en) | Air-inlet grille for automobile | |
| CN109159902B (en) | Drainage mechanism for air inlet of unmanned aerial vehicle engine | |
| CN109250003A (en) | The method of automobile and operation air guide device with double air guide devices | |
| SE542537C2 (en) | Vehicle air duct, air duct assembly, vehicle and method for controlling a vehicle air duct | |
| CN210882369U (en) | Automobile tail wing capable of reducing wind resistance | |
| CN210437283U (en) | Rotary type automobile active diffuser | |
| CN108301947B (en) | Automobile engine intake pipe supercharging device suitable for high and low speeds | |
| CN212220579U (en) | Fixed wing unmanned aerial vehicle for oil field inspection and special mechanism | |
| CN204402714U (en) | A kind of intake duct base assembly | |
| EP3792163B1 (en) | Revolvable active diffuser for vehicle | |
| CN208753409U (en) | A kind of visitor's Vehicular battery cabinet forced radiator | |
| CN113998126B (en) | Piston engine air cooling device for folding unmanned aerial vehicle | |
| CN204533391U (en) | The engine assembly of compound variable speed | |
| CN220809589U (en) | Multifunctional truck air guide sleeve with adjustable angle | |
| CN204749846U (en) | Novel drive shaft guide plate device | |
| CN204729600U (en) | Compact engine assembly | |
| CN219529454U (en) | Steering power-assisted oil cylinder and vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |