CN205730359U - A kind of aeromodelling airplane of band multifunctional detecting device - Google Patents
A kind of aeromodelling airplane of band multifunctional detecting device Download PDFInfo
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- CN205730359U CN205730359U CN201620413160.3U CN201620413160U CN205730359U CN 205730359 U CN205730359 U CN 205730359U CN 201620413160 U CN201620413160 U CN 201620413160U CN 205730359 U CN205730359 U CN 205730359U
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- detecting device
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- multifunctional detecting
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Abstract
The utility model discloses the aeromodelling airplane of a kind of band multifunctional detecting device, including main screw, operative body and tailplane, below described operative body, undercarriage is installed, described main screw is arranged on above operative body, described main screw is connected with operative body by fixing bar, in the middle part of described fixing bar, weight linear meter is installed, described tailplane is arranged on the right side of operative body, below described tailplane, power transmission shaft is installed, on the right side of described tailplane, vertical tail is installed, on the right side of described vertical tail, tail-rotor is installed, described tail-rotor is connected with tailplane by tail-rotor rotary shaft, described operative body lower inside is provided with power set, PLC ECU is installed on the right side of described power set, described operative body is electrically connected with power set and PLC ECU respectively.The aeromodelling airplane of this utility model band multifunctional detecting device, is provided with multifunctional detecting device, the property indices of detection aeromodelling airplane that can be intelligent.
Description
Technical field
This utility model relates to flight model plane field, the aeromodelling airplane of a kind of band multifunctional detecting device.
Background technology
null" model airplane is a kind of to overweight air to clear stipulaties in the rules of contest that International Aeronautical Federation formulates，There is size limitation，With or without electromotor，Remote-controlled can not be manned airborne vehicle，" aeromodelling airplane is general as manned aircraft，Main by wing、Empennage、Fuselage、Undercarriage and electromotor and control system six part form，Modern Aviation model sport is divided into free flight、Line is handled、Wireless remotecontrol、Emulation and the electronic big class of grade five，It is divided into again by power mode: piston engine、Jet engine、Rubber-band model aircraft and motorless model glider etc.，But existing aeromodelling airplane does not has the running parameter of some systems，For the duty under its different situations，We are not to be well aware of，Also cannot be carried out manipulation，Therefore，We are devoted to study and a kind of can detect aeromodelling airplane parameters under different situations，And the control parameters that energy is real-time.
Summary of the invention
The purpose of this utility model is to provide the aeromodelling airplane of a kind of band multifunctional detecting device, with the problem solving to propose in above-mentioned background technology.
nullFor achieving the above object，This utility model following technical scheme of offer: the aeromodelling airplane of a kind of band multifunctional detecting device，Including main screw、Operative body and tailplane，Below described operative body, undercarriage is installed，Described main screw is arranged on above operative body，Described main screw is connected with operative body by fixing bar，In the middle part of described fixing bar, weight linear meter is installed，Described main screw is connected with fixing bar by propeller axis，Described propeller axis side is provided with three main oar blades，And be uniformly distributed，Described main oar blade is connected with propeller axis by main oar rotary shaft，Described tailplane is arranged on the right side of operative body，Below described tailplane, power transmission shaft is installed，On the right side of described tailplane, vertical tail is installed，On the right side of described vertical tail, tail-rotor is installed，Described tail-rotor is connected with tailplane by tail-rotor rotary shaft，Described tail-rotor rotary shaft side is provided with two panels tail-rotor blade，And be uniformly distributed，Described operative body inner upper is provided with change speed gear box，Below described change speed gear box, motor is installed，On the right side of described motor, multifunctional detecting device is installed，Described operative body lower inside is provided with power set，PLC ECU is installed on the right side of described power set，Described operative body is electrically connected with power set and PLC ECU respectively，The outfan of described multifunctional detecting device is connected with the input of information transceiving device and information processor，The outfan of described information processor is connected with the input of PLC ECU，The outfan of described PLC ECU respectively with change speed gear box、Humidity controller is connected with the input of temperature controller.
Preferably, fix bar by cable-stayed type between described operative body and tailplane to be connected.
It is connected by two fixing devices between preferred described power transmission shaft and tailplane.
Preferably, the internal lower left of described operative body is provided with information processor, is provided with information transceiving device on the right side of described information processor.
Preferably, described multifunctional detecting device lower right is provided with humidity controller, is provided with temperature controller on the right side of described humidity controller.
Compared with prior art, the beneficial effects of the utility model are: the aeromodelling airplane of this utility model band multifunctional detecting device, multifunctional detecting device is installed, the pressure to aeromodelling airplane of energy intelligence, ambient temperature, motor temperature, motor speed, the property indices such as main rotor system RPMs and air humidity detects, and change speed gear box is installed, humidity controller and temperature controller, can be to the motor speed of aeromodelling airplane, main rotor system RPMs, motor temperature and humidity are controlled, the indices of the detection aeromodelling airplane that multifunctional detecting device energy is real-time, and operation bench can be sent to by information transceiving device, system record these data, and process, draw the optimum Working of aeromodelling airplane, research further and improvement tool for aeromodelling airplane are of great significance.
Accompanying drawing explanation
Fig. 1 is the aeromodelling airplane structure chart of this utility model a kind of band multifunctional detecting device；
Fig. 2 is utility model works main structure chart；
Fig. 3 is this utility model electrical structure figure.
In figure: 1-main screw；2-fixes bar；3-operative body；4-undercarriage；5-cable-stayed type fixes bar；6-tailplane；7-power transmission shaft；8-fixing device；9-tail-rotor；10-tail-rotor rotary shaft；11-tail-rotor blade；12-vertical tail；13-main oar blade；14-weight linear meter；15-change speed gear box；16-motor；17-information transceiving device；18-information processor；19-propeller axis；20-main oar rotary shaft；21-multifunctional detecting device；22-humidity controller；23-temperature controller；24-PLC ECU；25-power set.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole embodiments.Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art are obtained under not making creative work premise, broadly fall into the scope of this utility model protection.
nullRefer to Fig. 1-3，A kind of embodiment that this utility model provides: the aeromodelling airplane of a kind of band multifunctional detecting device，Including main screw 1、Operative body 3 and tailplane 6，Undercarriage 4 is installed below operative body 3，Main screw 1 is arranged on above operative body 3，Main screw 1 is connected with operative body 3 by fixing bar 2，In the middle part of fixing bar 2, weight linear meter 14 is installed，Main screw 1 is connected with fixing bar 2 by propeller axis 19，Propeller axis 19 side is provided with three main oar blades 13，And be uniformly distributed，Main oar blade 13 is connected with propeller axis 19 by main oar rotary shaft 20，Tailplane 6 is arranged on the right side of operative body 3，Power transmission shaft 7 is installed below tailplane 6，Vertical tail 12 is installed on the right side of tailplane 6，Tail-rotor 9 is installed on the right side of vertical tail 12，Tail-rotor 9 is connected with tailplane 6 by tail-rotor rotary shaft 10，Tail-rotor rotary shaft 10 side is provided with two panels tail-rotor blade 11，And be uniformly distributed，Operative body 3 inner upper is provided with change speed gear box 15，Motor 16 is installed below change speed gear box 15，Multifunctional detecting device 21 is installed on the right side of motor 16，Operative body 3 lower inside is provided with power set 25，PLC ECU 24 is installed on the right side of power set 25，Operative body 3 is electrically connected with power set 25 and PLC ECU 24 respectively，The outfan of multifunctional detecting device 21 is connected with the input of information transceiving device 17 and information processor 18，The outfan of information processor 18 is connected with the input of PLC ECU 24，The outfan of PLC ECU 24 respectively with change speed gear box 15、Humidity controller 22 is connected with the input of temperature controller 23，Fix bar 5 by cable-stayed type between operative body 3 with tailplane 6 to be connected，It is connected by two fixing devices 8 between power transmission shaft 7 with tailplane 6，The internal lower left of operative body 3 is provided with information processor 18，Information transceiving device 17 is installed on the right side of information processor 18，Multifunctional detecting device 21 lower right is provided with humidity controller 22，Temperature controller 23 is installed on the right side of humidity controller 22.
nullSpecifically used mode: in utility model works，Control main screw 1 and the tail-rotor 9 of PLC ECU 24 energy intelligence rotate，Control aeromodelling airplane lifting and move horizontally，The direction of motion of aeromodelling airplane is controlled by controlling the incline direction of weight linear meter 14，Simultaneously，Multifunctional detecting device 21 can be to the pressure of aeromodelling airplane、Ambient temperature、Motor 16 temperature、Motor 16 rotating speed、The property indices such as main screw 1 rotating speed and air humidity detect，And the data of collection are transferred to information transceiving device 17 and information processor 18，After data are processed by information processor 18，Send an instruction to PLC ECU 24，PLC ECU 24 controls change speed gear box 15、Humidity controller 22 and temperature controller 23 are operated，Control the parameters of aeromodelling airplane.
It is obvious to a person skilled in the art that this utility model is not limited to the details of above-mentioned one exemplary embodiment, and in the case of without departing substantially from spirit or essential attributes of the present utility model, it is possible to realize this utility model in other specific forms.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and be nonrestrictive, scope of the present utility model is limited by claims rather than described above, it is intended that all changes fallen in the implication of equivalency and scope of claim included in this utility model.Should not be considered as limiting involved claim by any reference in claim.
Claims (5)
- null1. the aeromodelling airplane of a band multifunctional detecting device，Including main screw (1)、Operative body (3) and tailplane (6)，It is characterized in that: described operative body (3) lower section is provided with undercarriage (4)，Described main screw (1) is arranged on operative body (3) top，Described main screw (1) is connected with operative body (3) by fixing bar (2)，Described fixing bar (2) middle part is provided with weight linear meter (14)，Described main screw (1) is connected with fixing bar (2) by propeller axis (19)，Described propeller axis (19) side is provided with three main oar blades (13)，And be uniformly distributed，Described main oar blade (13) is connected with propeller axis (19) by main oar rotary shaft (20)，Described tailplane (6) is arranged on operative body (3) right side，Described tailplane (6) lower section is provided with power transmission shaft (7)，Described tailplane (6) right side is provided with vertical tail (12)，Described vertical tail (12) right side is provided with tail-rotor (9)，Described tail-rotor (9) is connected with tailplane (6) by tail-rotor rotary shaft (10)，Described tail-rotor rotary shaft (10) side is provided with two panels tail-rotor blade (11)，And be uniformly distributed，Described operative body (3) inner upper is provided with change speed gear box (15)，Described change speed gear box (15) lower section is provided with motor (16)，Described motor (16) right side is provided with multifunctional detecting device (21)，Described operative body (3) lower inside is provided with power set (25)，Described power set (25) right side is provided with PLC ECU (24)，Described operative body (3) is electrically connected with power set (25) and PLC ECU (24) respectively，The outfan of described multifunctional detecting device (21) is connected with the input of information transceiving device (17) and information processor (18)，The outfan of described information processor (18) is connected with the input of PLC ECU (24)，The outfan of described PLC ECU (24) respectively with change speed gear box (15)、Humidity controller (22) is connected with the input of temperature controller (23).
- The aeromodelling airplane of a kind of band multifunctional detecting device the most according to claim 1, it is characterised in that: fix bar (5) by cable-stayed type between described operative body (3) with tailplane (6) and be connected.
- The aeromodelling airplane of a kind of band multifunctional detecting device the most according to claim 1, it is characterised in that: it is connected by two fixing devices (8) between described power transmission shaft (7) with tailplane (6).
- The aeromodelling airplane of a kind of band multifunctional detecting device the most according to claim 1, it is characterized in that: the internal lower left of described operative body (3) is provided with information processor (18), described information processor (18) right side is provided with information transceiving device (17).
- The aeromodelling airplane of a kind of band multifunctional detecting device the most according to claim 1, it is characterized in that: described multifunctional detecting device (21) lower right is provided with humidity controller (22), described humidity controller (22) right side is provided with temperature controller (23).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620413160.3U CN205730359U (en) | 2016-05-09 | 2016-05-09 | A kind of aeromodelling airplane of band multifunctional detecting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620413160.3U CN205730359U (en) | 2016-05-09 | 2016-05-09 | A kind of aeromodelling airplane of band multifunctional detecting device |
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| Publication Number | Publication Date |
|---|---|
| CN205730359U true CN205730359U (en) | 2016-11-30 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620413160.3U Expired - Fee Related CN205730359U (en) | 2016-05-09 | 2016-05-09 | A kind of aeromodelling airplane of band multifunctional detecting device |
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| CN (1) | CN205730359U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108696301A (en) * | 2017-03-31 | 2018-10-23 | 迪尔航空航天有限公司 | Transmitting device and aircraft for the transmission data in aircraft |
-
2016
- 2016-05-09 CN CN201620413160.3U patent/CN205730359U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108696301A (en) * | 2017-03-31 | 2018-10-23 | 迪尔航空航天有限公司 | Transmitting device and aircraft for the transmission data in aircraft |
| CN108696301B (en) * | 2017-03-31 | 2021-09-28 | 迪尔航空航天有限公司 | Transmission device for transmitting data in an aircraft, and aircraft |
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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: 20161130 Termination date: 20170509 |