CN104202028B - Safety switch for small aircraft - Google Patents

Safety switch for small aircraft Download PDF

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Publication number
CN104202028B
CN104202028B CN201410406890.6A CN201410406890A CN104202028B CN 104202028 B CN104202028 B CN 104202028B CN 201410406890 A CN201410406890 A CN 201410406890A CN 104202028 B CN104202028 B CN 104202028B
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China
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signal
pmos
resistance
motor
switch
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Expired - Fee Related
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CN201410406890.6A
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Chinese (zh)
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CN104202028A (en
Inventor
黄夏楠
林振智
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Zhejiang University ZJU
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Zhejiang University ZJU
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Priority to CN201410406890.6A priority Critical patent/CN104202028B/en
Publication of CN104202028A publication Critical patent/CN104202028A/en
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Publication of CN104202028B publication Critical patent/CN104202028B/en
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Abstract

The invention discloses a safety switch for a small aircraft. The safety switch for the small aircraft comprises a voltage-stabilizing module, a signal receiving module, a signal processing module, a switch, a remote controller and a battery, wherein the battery is used for supplying power for the signal receiving module and the signal processing module; the voltage-stabilizing module is respectively connected with the signal receiving module and the signal processing module; the remote controller is used for sending a signal to the signal receiving module through radio, the signal receiving module is connected with the signal processing module, the signal receiving module is used for receiving a remote-control index signal from the remote controller and sending the signal to the signal processing module; and the signal processing module is connected with the switch for controlling the on-off of the switch. The safety switch can be controlled at on or off state under PWM (pulse-width modulation) waves in different duty ratios. The safety switch is small in volume, light in mass, low in power consumption, strong in robustness and especially applied to fast turning off power supply when the small aircraft is out of operation so as to prevent the personal injury and property damage.

Description

Small aircraft safety switch
Technical field
The invention belongs to safety device, more particularly to a kind of small aircraft safety switch.
Background technology
Existing small aircraft adopts remote control control, when aircraft loses the control in remote control power, direction, does not have There are the means reliably cut off the electricity supply, so as to cause small aircraft to continue flight out of control, cause personnel's property to damage and lose. This phenomenon causes certain risk for the practical operation of small aircraft.
The content of the invention
In order to after overcoming small aircraft out of control cannot power-off control, so as to damnous risk, the present invention provides one Plant small aircraft safety switch.
The purpose of the present invention is achieved through the following technical solutions:A kind of small aircraft safety switch, including voltage stabilizing Module, signal receiving module, signal processing module, switch, remote control and battery, battery is to signal receiving module and signal processing Module for power supply;Voltage stabilizing module is connected with signal receiving module, signal processing module respectively;Remote control is connect to signal by radio Module sending signal is received, signal receiving module is connected with signal processing module, signal receiving module receives the remote control of remote control and refers to Show signal, and transmit a signal to signal processing module;Signal processing module is connected with switch, the break-make of controlling switch;It is described Signal processing module includes double D trigger U2, electric capacity C1, C6, C7, inductance L1, resistance R3, R4, adjustable potentiometer R2, lights two Pole pipe D2, audion Q1;Wherein, electric capacity C1 one end is connected with VCC, and the other end is connected to the ground;Electric capacity C6 one end and double D trigger The 1R ports of U2 are connected, and the other end is connected to the ground;Electric capacity C7 one end and inductance L1 and resistance R3, other end ground connection;Inductance L1 mono- End is connected with the 2Q ports of double D trigger, other end connection resistance R3 and electric capacity C7;One end connection inductance L1 of resistance R3, separately One end is connected with the base stage of audion Q1;Resistance R4 one end is connected with VCC, and the other end is connected with light emitting diode D2 anodes;Send out Optical diode D2 anodes are connected with resistance R4 one end, and the other end is connected with 2 ports of double D trigger;The base stage of audion Q1 connects Connecting resistance R3, colelctor electrode are connected with PMOS P-MOSFET of switch, the grid of PMOS P-MOSFET2, grounded emitter;Can 2 end of center contact of potentiometer R2 is adjusted to be connected with the 1Q ports of double D trigger with 1 end, 3 ends are connected with electric capacity C6 one end;Double D The remote control indication signal that the 1CLK ports of trigger receive, by low transition be high level when, electric capacity C6 pass through adjustable electric Position device R2 is started to charge up, and its two ends charging voltage reaches the time length of 5V(Threshold value)Determined by the resistance of adjustable potentiometer R2; When the dutycycle of remote control indication signal is less than the threshold value, audion Q1 is led by the 2Q ports output high level of double D trigger Logical, the collector potential of audion Q1 is identical with emitting stage current potential, to PMOS P-MOSFET and PMOS P- that switch The grid output low level of MOSFET2, the 2 ports output low level of double D trigger, light emitting diode D2 are lighted, and indicate switch In closure state;When the dutycycle of remote control indication signal is more than the threshold value, the 2Q ports output low level of double D trigger, Audion Q1 is turned off, audion Q1 is in high-impedance state, the grid to PMOS P-MOSFET and PMOS P-MOSFET2 of switch Pole does not export low level signal, and the 2 ports output high level of double D trigger, light emitting diode D2 are knocked out, and indicate switch in disconnected Open state.
The signal receiving module includes signal receiver P1, resistance R5;Wherein, resistance R5 one end and signal receiver P1 Signal port be connected, the other end is connected to the ground;The signal port of signal receiver P1 and the double D trigger of signal processing module 1CLK ports, 2D ports be connected;Positive pole is connected with VCC;Minus earth.
The Voltage stabilizing module includes 5V voltage stabilizing chips U1, resistance R1, electric capacity C2, C3, C4, C5, light emitting diode D1;Its In, electric capacity C2 is connected with the input port of 5V voltage stabilizing chips U1 with one end of C3, other end ground connection;One end of electric capacity C4 and C5 is equal It is connected with the output port of 5V voltage stabilizing chips U1, the other end is connected to the ground;Resistance R1 one end and the outfan of 5V voltage stabilizing chips U1 Mouth is connected, and the other end is connected with the anode of light emitting diode D1;The minus earth of light emitting diode D1;5V voltage stabilizing chips U1 it is defeated Inbound port is connected with positive source, and ground port is connected to the ground, output port output 5V voltages, supplies signal receiving module and signal Processing module.
The switch includes power supply wiring mouth P2, and PMOS P-MOSFET, PMOS P-MOSFET2, resistance R6, motor connect Line mouth Motor;Wherein, resistance R6 one end is connected with 1 port of power supply wiring mouth P2, the other end and PMOS P-MOSFET and The grid of PMOS P-MOSFET2 is connected;The current collection of the grid of PMOS P-MOSFET and the audion Q1 of signal processing module Extremely it is connected, drain electrode is connected with the positive pole of motor connection jaws Motor, and source electrode is connected with the positive pole of power supply wiring mouth P2;PMOS P- The grid of MOSFET2 is connected with the colelctor electrode of the audion Q1 of signal processing module, the positive pole of drain electrode and motor connection jaws Motor It is connected, source electrode is connected with the positive pole of power supply wiring mouth P2;The positive pole of power supply wiring mouth P2 is connected with positive source, negative pole with ground and Power cathode is connected;The positive pole of motor connection jaws Motor is connected with the positive pole of motor, and negative pole is connected with the negative pole of ground and motor; When the grid of PMOS P-MOSFET and PMOS P-MOSFET2 receives low level signal, their drain electrode and source electrode connect Logical so that the positive pole of power supply wiring mouth P2 is connected with the positive pole of motor connection jaws Motor, motor obtains the power supply of power supply and normal Work;When PMOS P-MOSFET and the grid of PMOS P-MOSFET2 are not received by low level signal or receive high electricity During ordinary mail, their drain electrode and source electrode disconnect so that the positive pole of power supply wiring mouth P2 is broken with the positive pole of motor connection jaws Motor Open, motor loses the power supply of power supply, quits work.
The invention has the beneficial effects as follows:Using the DC source of small aircraft, not only from having reached to small aircraft The break-make control of working power, provides working power to safety switch circuit also by 5V voltage stabilizing chips.
Simple structure, small volume are lightweight, may be mounted at any one place on small aircraft and do not affect weight The heart.
Can be in the difference according to small aircraft rotor quantity, DC source size, using varying number, the P- of model MOSFET is managed, with good robustness.
Description of the drawings
Fig. 1 is small aircraft safety switch construction schematic diagram;
Fig. 2 is the circuit diagram of signal processing module;
Fig. 3 is the circuit diagram of signal receiving module;
Fig. 4 is the circuit diagram of Voltage stabilizing module;
Fig. 5 is the circuit diagram of switch.
It is embodied as explanation
With reference to embodiments and its accompanying drawing is further described.
With reference to embodiments and its accompanying drawing is further described.
As shown in figure 1, small aircraft safety switch includes Voltage stabilizing module, signal receiving module, signal processing module, opens Pass, remote control and battery, battery are powered to signal receiving module and signal processing module;Voltage stabilizing module receives mould with signal respectively Block, signal processing module are connected, for stabilization signal receiver module, the voltage of signal processing module;Remote control passes through radio To signal receiving module sending signal, receive signal receiving module and be connected with signal processing module, signal receiving module receives distant The remote control indication signal of control device, and transmit a signal to signal processing module;Signal processing module is connected with switch, controlling switch Break-make.
As shown in Fig. 2 the signal processing module includes double D trigger U2, electric capacity C1, C6, C7, inductance L1, resistance R3, R4, adjustable potentiometer R2, light emitting diode D2, audion Q1;Wherein, electric capacity C1 one end is connected with VCC, the other end and ground phase Even;Electric capacity C6 one end is connected with the 1R ports of double D trigger U2, and the other end is connected to the ground;Electric capacity C7 one end and inductance L1 and electricity Resistance R3, other end ground connection;Inductance L1 one end is connected with the 2Q ports of double D trigger, other end connection resistance R3 and electric capacity C7;Electricity One end connection inductance L1 of resistance R3, the other end are connected with the base stage of audion Q1;Resistance R4 one end is connected with VCC, the other end with Light emitting diode D2 anodes are connected;Light emitting diode D2 anodes are connected with resistance R4 one end, 2 ends of the other end and double D trigger Mouth is connected;The base stage connection resistance R3 of audion Q1, colelctor electrode and PMOS P-MOSFET, PMOS P-MOSFET2 that switch Grid be connected, grounded emitter;1Q port phase of 2 end of center contact of adjustable potentiometer R2 with 1 end with double D trigger Even, 3 ends are connected with electric capacity C6 one end.The remote control indication signal that the 1CLK ports of double D trigger receive, by low transition be During high level, electric capacity C6 is started to charge up by adjustable potentiometer R2, and its two ends charging voltage reaches the time length of 5V by adjustable The resistance of potentiometer R2 determines that the time is referred to as threshold value.When the dutycycle of remote control indication signal is less than the threshold value, double D triggerings The 2Q ports output high level of device, audion Q1 is turned on, and the collector potential of audion Q1 is identical with emitting stage current potential, split PMOS P-MOSFET of pass exports low level with the grid of PMOS P-MOSFET2, and 2 ports of double D trigger export low electricity Flat, light emitting diode D2 is lighted, and indicates switch in closure state;When the dutycycle of remote control indication signal is more than the threshold value, The 2Q ports output low level of double D trigger, audion Q1 is turned off, and audion Q1 is in high-impedance state, to the PMOS for switching P-MOSFET does not export low level signal with the grid of PMOS P-MOSFET2, and the 2 ports output high level of double D trigger is sent out Optical diode D2 is knocked out, and indicates that switch is off.
As shown in figure 3, the signal receiving module includes signal receiver P1, resistance R5;Wherein, resistance R5 one end and letter The signal port of number receptor P1 is connected, and the other end is connected to the ground;The signal port and signal processing module of signal receiver P1 The 1CLK ports of double D trigger, 2D ports are connected;Positive pole is connected with VCC;Minus earth.The module is powered by VCC, electricity Resistance R5 plays a part of stable remote control indication signal level, and the remote control indication signal that the module output is received is to signal processing mould Block.
As shown in figure 4, the Voltage stabilizing module includes 5V voltage stabilizing chips U1, resistance R1, electric capacity C2, C3, C4, C5 light two Pole pipe D1;Wherein, electric capacity C2 is connected with the input port of 5V voltage stabilizing chips U1 with one end of C3, other end ground connection;Electric capacity C4 with One end of C5 is connected with the output port of 5V voltage stabilizing chips U1, and the other end is connected to the ground;Resistance R1 one end and 5V voltage stabilizing chips The output port of U1 is connected, and the other end is connected with the anode of light emitting diode D1;The minus earth of light emitting diode D1;5V voltage stabilizings The input port of chip U1 is connected with positive source, and ground port is connected to the ground, output port output 5V voltages, that is, VCC, is supplied To signal receiving module and signal processing module, as its running voltage, light emitting diode D1 is lighted, and represents that Voltage stabilizing module is normal Work.
As shown in figure 5, the switch includes power supply wiring mouth P2, PMOS P-MOSFET, PMOS P-MOSFET2, electricity Resistance R6, motor connection jaws Motor;Wherein, resistance R6 one end is connected with 1 port of power supply wiring mouth P2, the other end and PMOS P-MOSFET is connected with the grid of PMOS P-MOSFET2;The grid of PMOS P-MOSFET and three poles of signal processing module The colelctor electrode of pipe Q1 is connected, and drain electrode is connected with the positive pole of motor connection jaws Motor, the positive pole phase of source electrode and power supply wiring mouth P2 Even;The grid of PMOS P-MOSFET2 is connected with the colelctor electrode of the audion Q1 of signal processing module, is drained and motor connection jaws The positive pole of Motor is connected, and source electrode is connected with the positive pole of power supply wiring mouth P2;The positive pole of power supply wiring mouth P2 and positive source phase Even, negative pole is connected with ground and power cathode;The positive pole of motor connection jaws Motor is connected with the positive pole of motor, negative pole with ground and electricity The negative pole of machine is connected.When the grid of PMOS P-MOSFET and PMOS P-MOSFET2 receives low level signal, they Drain electrode is connected with source electrode so that the positive pole of power supply wiring mouth P2 is connected with the positive pole of motor connection jaws Motor, and motor obtains power supply Power supply and normal work;When PMOS P-MOSFET is not received by low level signal with the grid of PMOS P-MOSFET2 Or when receiving high level signal, their drain electrode and source electrode disconnect so that the positive pole of power supply wiring mouth P2 and motor connection jaws The positive pole of Motor disconnects, and motor loses the power supply of power supply, quits work.
The remote control is model airplane remote controller, including X2610 models, the 8CH models of JR companies, the SD- of SANWA companies 10G models, 6EXHP models of FUTABA companies etc..
Using front, by remote control with signal receiving module to frequency so that safety switch can be entered by radio with remote control Row communication;
Signal receiving module receives the remote control indication signal of small aircraft remote control(PWM ripples), and by signal(PWM ripples) Send signal processing module to;Signal processing module is according to the PWM ripple dutycycles for receiving, controlling switch break-make;Fly when small-sized When row device is in the hole(To thrust into), the gear on adjusting remote device so that PWM ripples dutycycle is less than threshold value, switch is disconnected, Power supply of the power supply to aircraft is completely cut through, small aircraft falls, prevented injury of the aircraft to personnel etc..

Claims (3)

1. a kind of small aircraft safety switch, it is characterised in that including Voltage stabilizing module, signal receiving module, signal processing mould Block, switch, remote control and battery, battery are powered to signal receiving module and signal processing module;Voltage stabilizing module respectively with signal Receiver module, signal processing module are connected;Remote control is by radio to signal receiving module sending signal, signal receiving module It is connected with signal processing module, signal receiving module receives the remote control indication signal of remote control, and transmits a signal at signal Reason module;Signal processing module is connected with switch, the break-make of controlling switch;The signal processing module includes double D trigger U2, Electric capacity C1, C6, C7, inductance L1, resistance R3, R4, adjustable potentiometer R2, light emitting diode D2, audion Q1;Wherein, electric capacity C1 One end is connected with VCC, and the other end is connected to the ground;Electric capacity C6 one end is connected with the 1R ports of double D trigger U2, the other end and ground phase Even;Electric capacity C7 one end is connected with inductance L1 and resistance R3, other end ground connection;The 2Q ports phase of inductance L1 one end and double D trigger Even, other end connection resistance R3 and electric capacity C7;One end connection inductance L1 of resistance R3, the base stage phase of the other end and audion Q1 Even;Resistance R4 one end is connected with VCC, and the other end is connected with light emitting diode D2 anodes;Light emitting diode D2 anodes and resistance R4 One end is connected, and the other end is connected with 2 ports of double D trigger;The base stage connection resistance R3 of audion Q1, colelctor electrode and switch PMOS P-MOSFET, the grid of PMOS P-MOSFET2 are connected, grounded emitter;2 end of center contact of adjustable potentiometer R2 It is connected with the 1Q ports of double D trigger with 1 end, 3 ends are connected with electric capacity C6 one end;
The switch includes power supply wiring mouth P2, PMOS P-MOSFET, PMOS P-MOSFET2, resistance R6, motor connection jaws Motor;Wherein, resistance R6 one end is connected with 1 port of power supply wiring mouth P2, the other end and PMOS P-MOSFET and PMOS The grid of P-MOSFET2 is connected;The grid of PMOS P-MOSFET is connected with the colelctor electrode of the audion Q1 of signal processing module, Drain electrode is connected with the positive pole of motor connection jaws Motor, and source electrode is connected with the positive pole of power supply wiring mouth P2;PMOS P-MOSFET2 Grid be connected with the colelctor electrode of the audion Q1 of signal processing module, drain electrode be connected with the positive pole of motor connection jaws Motor, source Pole is connected with the positive pole of power supply wiring mouth P2;The positive pole of power supply wiring mouth P2 is connected with positive source, minus earth;Motor wiring The mouth positive pole of Motor is connected with the positive pole of motor, minus earth;
The remote control indication signal that the 1CLK ports of double D trigger receive, by low transition be high level when, electric capacity C6 passes through Adjustable potentiometer R2 is started to charge up, and its two ends charging voltage reaches the time length of 5V and determined by the resistance of adjustable potentiometer R2; When the dutycycle of remote control indication signal is less than the time length in short-term, the 2Q ports output high level of double D trigger, by audion Q1 Conducting, the collector potential of audion Q1 are identical with emitting stage current potential, to PMOS P-MOSFET and PMOS P- that switch The grid output low level of MOSFET2, the 2 ports output low level of double D trigger, light emitting diode D2 are lighted, and indicate switch In closure state;When the grid of PMOS P-MOSFET and PMOS P-MOSFET2 receives low level signal, they Drain electrode is connected with source electrode so that the positive pole of power supply wiring mouth P2 is connected with the positive pole of motor connection jaws Motor, and motor obtains power supply Power supply and normal work;When the dutycycle of remote control indication signal is more than the time length in short-term, the 2Q ports output of double D trigger Low level, audion Q1 is turned off, and audion Q1 is in high-impedance state, to PMOS P-MOSFET and PMOS P- that switch The grid of MOSFET2 does not export low level signal, and the 2 ports output high level of double D trigger, light emitting diode D2 are knocked out, referred to Show that switch is off;When PMOS P-MOSFET is not received by low level letter with the grid of PMOS P-MOSFET2 Number or when receiving high level signal, their drain electrode and source electrode disconnect so that the positive pole of power supply wiring mouth P2 and motor wiring The positive pole of mouth Motor disconnects, and motor loses the power supply of power supply, quits work.
2. a kind of small aircraft safety switch according to claim 1, it is characterised in that the signal receiving module bag Include signal receiver P1, resistance R5;Wherein, resistance R5 one end is connected with the signal port of signal receiver P1, the other end with ground It is connected;The 1CLK ports of the signal port of signal receiver P1 and the double D trigger of signal processing module, 2D ports are connected, just Pole is connected with VCC, minus earth.
3. a kind of small aircraft safety switch according to claim 1, it is characterised in that the Voltage stabilizing module includes 5V Voltage stabilizing chip U1, resistance R1, electric capacity C2, C3, C4, C5, light emitting diode D1;Wherein, one end of electric capacity C2 and C3 is steady with 5V The input port of pressure chip U1 is connected, other end ground connection;Output port phase of the one end of electric capacity C4 and C5 with 5V voltage stabilizing chips U1 Even, the other end is connected to the ground;Resistance R1 one end is connected with the output port of 5V voltage stabilizing chips U1, the other end and light emitting diode D1 Anode be connected;The minus earth of light emitting diode D1;The input port of 5V voltage stabilizing chips U1 is connected with positive source, ground port It is connected to the ground, output port output 5V voltages supply signal receiving module and signal processing module.
CN201410406890.6A 2014-08-19 2014-08-19 Safety switch for small aircraft Expired - Fee Related CN104202028B (en)

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Application Number Priority Date Filing Date Title
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Application Number Priority Date Filing Date Title
CN201410406890.6A CN104202028B (en) 2014-08-19 2014-08-19 Safety switch for small aircraft

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CN104202028B true CN104202028B (en) 2017-04-12

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Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105116799A (en) * 2015-08-06 2015-12-02 北京韦加航通科技有限责任公司 Remote control switch and control method
CN106961267B (en) * 2017-05-09 2023-05-30 四川巧夺天工信息安全智能设备有限公司 Anti-misoperation anti-interference switching circuit

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2376141Y (en) * 1999-02-04 2000-04-26 张忠 General infrared remote-control switch
CN203014993U (en) * 2012-11-27 2013-06-19 深圳市睿碒科技有限公司 Switching circuit controlling power source of television signal receiving circuit

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005020363A (en) * 2003-06-26 2005-01-20 Matsushita Electric Ind Co Ltd Pulse width modulation driving device

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2376141Y (en) * 1999-02-04 2000-04-26 张忠 General infrared remote-control switch
CN203014993U (en) * 2012-11-27 2013-06-19 深圳市睿碒科技有限公司 Switching circuit controlling power source of television signal receiving circuit

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