Power supply control system device of airborne artificial influence weather system

Abstract

The utility model provides a power supply control system device of an airborne artificial influence weather system in order to solve the problem that each subsystem of the airborne artificial influence weather system cannot be monitored and protected in the prior art. The power supply control system device comprises a general control switch, a general control circuit breaker, a contactor, a circuit breaker module and a toggle switch module. Wherein the circuit breakers of m subsystems of the circuit breaker module and the toggle switch module comprise toggle switches of m subsystems, and m is not less than 1. The airplane provided with the power supply control system device can automatically monitor and protect the power supply control of the human shadow subsystem without the operation of a flight crew, and can complete the monitoring and protection of the human shadow subsystem without any auxiliary equipment and facilities.

Description

Technical Field

[0001] The utility model relates to the technical field of power supply control and power supply protection, in particular to a power supply control system device for an airborne artificial weather modification system. Background Art

[0002] An airborne weather modification system is a comprehensive set of technical systems installed on aircraft for weather modification operations. The power control system manages, distributes, monitors, and protects the power supply to the onboard weather modification equipment. This reduces the impact of the weather modification system's load on the aircraft's power supply, thereby reducing crew workload and improving flight safety.

[0003] In the prior art, the King Air 360 airborne weather modification system lacks a power control system, and the various subsystems of the airborne weather modification system cannot be monitored and protected. The present invention aims to provide a power control device for the airborne weather modification system. Utility Model Content

[0004] The utility model aims to solve the problem in the prior art that various subsystems of an airborne artificial weather modification system cannot be monitored and protected, and provides a power supply control system device for the airborne artificial weather modification system.

[0005] The technical solution adopted in this utility model is:

[0006] A power supply control system device for an airborne weather modification system, comprising:

[0007] The master control switch is used to control the power input of the entire power control system device.

[0008] The master circuit breaker is used for overload protection of the load of the entire power control system device.

[0009] A contactor, one input end of which is connected to the output end of the master control circuit breaker, and the other input end of which is connected to the output end of the master control switch, is used to control the power supply input of the entire power control system device.

[0010] A circuit breaker module, wherein the input end of the circuit breaker module is connected to the output end of the contactor, and the circuit breaker module includes circuit breakers for m subsystems, which are used for overload protection of each subsystem of the weather modification system, where m is not less than 1.

[0011] A toggle switch module, wherein the m input terminals of the toggle switch module are connected to the corresponding m output terminals of the circuit breaker module, and the toggle switch module includes toggle switches of m subsystems, which are used to control the separate power supply input of each subsystem of the artificial weather modification system.

[0012] Furthermore, the circuit breaker module includes circuit breakers of 12 subsystems, which are:

[0013] The GVR circuit breaker is used to control overload protection of the GVR subsystem of the weather modification system without affecting other weather modification system subsystems connected to the power control system. GVR stands for Airborne Microwave Radiometer.

[0014] The KPR circuit breaker is used to control overload protection of the KPR subsystem of the weather modification system without affecting other weather modification system subsystems connected to the power control system. KPR stands for Airborne Ka-band Cloud Radar.

[0015] The CCN circuit breaker is used to control overload protection of the CCN subsystem of the weather modification system without affecting other weather modification subsystems connected to the power control system. CCN stands for Cloud Condensation Nuclei Analyzer.

[0016] The PCASP circuit breaker is used to control overload protection of the PCASP subsystem of the weather modification system without affecting other weather modification system subsystems connected to the power control system. PCASP stands for Passive Cavity Aerosol Sounder.

[0017] The CCP circuit breaker is used to control overload protection of the CCP subsystem of the weather modification system without affecting other weather modification system subsystems connected to the power control system. CCP stands for Cloud Combination Detector.

[0018] The PIP circuit breaker is used to control overload protection of the PIP subsystem of the weather modification system without affecting other weather modification system subsystems connected to the power control system. PIP stands for Precipitation Imaging System.

[0019] The AIMMS circuit breaker is used to control overload protection of the AIMMS subsystem of the weather modification system without affecting other weather modification subsystems connected to the power control system. AIMMS stands for Aircraft Integrated Meteorological Measurement System.

[0020] The ZBT-LC-01 circuit breaker is used to control overload protection of the ZBT-LC-01R subsystem of the weather modification system without affecting other weather modification system subsystems connected to the power control system. ZBT-LC-01 stands for Cloud Particle Spectrometer.

[0021] The ZBT-LC-02 circuit breaker is used to control overload protection of the ZBT-LC-02 subsystem of the weather modification system without affecting other weather modification system subsystems connected to the power control system. The ZBT-LC-02 refers to the cloud particle imager.

[0022] The ZBT-LC-03 circuit breaker is used to control overload protection of the YGDS / C subsystem of the weather modification system without affecting other weather modification subsystems connected to the power control system. The ZBT-LC-03 stands for Precipitation Particle Imager.

[0023] The YGDS / C circuit breaker controls the power input from the power control system to the YGDS / C subsystem of the weather modification system. YGDS / C stands for Atmospheric Data Acquisition Pod.

[0024] The industrial computer circuit breaker is used to control overload protection of the industrial computer / display subsystem of the weather modification system without affecting other weather modification system subsystems connected to the power control system.

[0025] Furthermore, the toggle switch module includes 12 subsystem toggle switches, which are:

[0026] A GVR toggle switch, the input end of which is connected to the output end of the GVR circuit breaker, is used to control the power supply control system to input power to the GVR subsystem of the weather modification system.

[0027] A KPR toggle switch, the input end of which is connected to the output end of the KPR circuit breaker, is used to control the power supply control system to input power to the KPR subsystem of the weather modification system.

[0028] A CCN toggle switch, the input end of which is connected to the output end of the CCN circuit breaker, is used to control the power supply control system to input power to the CCN subsystem of the weather modification system.

[0029] A PCASP toggle switch, the input end of which is connected to the output end of the PCASP circuit breaker, is used to control the power supply control system to input power to the PCASP subsystem of the artificial weather modification system.

[0030] A CCP toggle switch, the input end of which is connected to the output end of the CCP circuit breaker, is used to control the power supply control system to input power to the CCP subsystem of the weather modification system.

[0031] A PIP toggle switch, the input end of which is connected to the output end of the PIP circuit breaker, is used to control the power supply control system to input power to the PIP subsystem of the artificial weather modification system.

[0032] An AIMMS toggle switch, the input end of which is connected to the output end of the AIMMS circuit breaker, is used to control the power supply control system to input power to the AIMMS subsystem of the weather modification system.

[0033] A ZBT-LC-01 toggle switch, the input end of which is connected to the output end of the ZBT-LC-01 circuit breaker, for controlling the power supply control system to input power to the ZBT-LC-01 subsystem of the weather modification system.

[0034] A ZBT-LC-02 toggle switch, the input end of which is connected to the output end of the ZBT-LC-02 circuit breaker, and is used to control the power supply control system to input power to the ZBT-LC-02 subsystem of the weather modification system.

[0035] A ZBT-LC-03 toggle switch, the input end of which is connected to the output end of the ZBT-LC-03 circuit breaker, is used to control the power supply control system to input power to the ZBT-LC-03 subsystem of the weather modification system.

[0036] A YGDS / C toggle switch, the input end of which is connected to the output end of the YGDS / C circuit breaker, is used to control the power supply control system to input power to the YGDS / C subsystem of the weather modification system.

[0037] The industrial computer switches the power switch, the input end of which is connected to the output end of the industrial computer circuit breaker, for controlling the power control system to input power to the industrial computer / display subsystem of the weather modification system.

[0038] Furthermore, the contactor is a normally open contactor. When the master control switch is pressed, the contactor is controlled to be turned on and the circuit is turned on; when the master control switch is lifted, the contactor is controlled to be turned off and the circuit is turned off.

[0039] Furthermore, the internal safety structure of the master control circuit breaker is a fuse.

[0040] Furthermore, the internal safety structure of the circuit breakers of all subsystems in the circuit breaker module is a fuse.

[0041] Furthermore, the master control switch is an aviation-specific toggle switch.

[0042] Further, the toggle switches of all subsystems in the toggle switch module are aviation-specific toggle switches.

[0043] The utility model discloses the beneficial effect is:

[0044] The aircraft that installed the power control device of airborne weather modification system of the utility model can automatically monitor and protect the power control of the weather modification system without the operation of the crew, and can complete the monitoring and protection of the weather modification system without any auxiliary equipment and facilities. When the subsystem is overloaded, the circuit breaker corresponding to the subsystem is automatically disconnected, cutting off the power supply to the corresponding system. When all subsystems are simultaneously overloaded, the master control circuit breaker is automatically disconnected, cutting off the power supply to the power control system, thereby protecting the power system of the aircraft. BRIEF DESCRIPTION OF DRAWINGS

[0045] In order to more clearly illustrate the technical solutions in the embodiments of the present application or the prior art, the drawings needed to be used in the embodiments or prior art description will be briefly introduced. Obviously, the drawings in the following description are only some embodiments of the present application, and other drawings can be obtained by those skilled in the art without creative labor.

[0046] Figure 1 The power control system device diagram. DETAILED DESCRIPTION

[0047] Weather modification system is a comprehensive technical system, which mainly refers to the collection of a complete set of equipment, technical methods and organizational management measures for artificially influencing the physical and chemical processes of local atmosphere through scientific and technological means, so as to make the weather phenomenon change in the direction expected by people. The purpose is to increase precipitation, prevent hail, eliminate fog, prevent frost, etc., so as to reduce the influence of meteorological disasters on human society and natural environment.

[0048] The power control of weather modification system is a new technology, which refers to the power control system to realize the separate power supply management control of each subsystem of weather modification system, and to realize the automatic monitoring and protection of the power supply of the entire power control system and each subsystem of weather modification system, so as to reduce the influence of weather modification system load on the aircraft power supply, thereby reducing the work load of the crew and improving the flight safety of the aircraft.

[0049] In the prior art, the aircraft lacks a power control system device, and the subsystems of the weather modification system cannot be monitored and protected.

[0050] The utility model aims to solve the problem in the prior art that various subsystems of an airborne artificial weather modification system cannot be monitored and protected, and provides a power supply control system device for the airborne artificial weather modification system.

[0051] The following disclosure provides embodiments for realizing different structures of the present invention, which are merely examples and are not intended to limit the present invention.

[0052] The following is combined with Figure 1 The schematic diagram of the power control system device is used to describe the embodiment of the utility model in detail.

[0053] A power supply control system device for an airborne weather modification system, comprising:

[0054] The master control switch is used to control the power input of the entire power control system device.

[0055] The master control circuit breaker is used for overload protection of the load of the entire power control system device. In this embodiment, the internal safety structure of the master control circuit breaker is a fuse.

[0056] A contactor, one input of which is connected to the output of the master control circuit breaker, and the other input of which is connected to the output of the master control switch, is used to control the power input of the entire power control system. In this embodiment, the contactor is a normally open contactor. When the master control switch is pressed, the contactor is controlled to conduct, thereby completing the circuit. When the master control switch is released, the contactor is controlled to open, thereby disconnecting the circuit.

[0057] A circuit breaker module, wherein the input of the circuit breaker module is connected to the output of the contactor. In this embodiment, the circuit breaker module includes circuit breakers for 12 subsystems, providing overload protection for each subsystem of the weather modification system. In this embodiment, the internal safety features of the circuit breakers for all subsystems in the circuit breaker module are fuses.

[0058] A toggle switch module, wherein the 12 input terminals of the toggle switch module are connected to the corresponding 12 output terminals of the circuit breaker module. The toggle switch module includes 12 subsystem toggle switches for controlling the individual power input of each subsystem of the artificial weather modification system.

[0059] The master control switch is an aviation-specific toggle switch, and the toggle switches of all subsystems in the toggle switch module are aviation-specific toggle switches.

[0060] Furthermore, the circuit breakers of the 12 subsystems of the circuit breaker module are respectively:

[0061] The GVR circuit breaker is used to control overload protection of the GVR subsystem of the weather modification system without affecting other weather modification system subsystems connected to the power control system. GVR stands for Airborne Microwave Radiometer.

[0062] The KPR circuit breaker is used to control overload protection of the KPR subsystem of the weather modification system without affecting other weather modification system subsystems connected to the power control system. KPR stands for Airborne Ka-band Cloud Radar.

[0063] The CCN circuit breaker is used to control overload protection of the CCN subsystem of the weather modification system without affecting other weather modification subsystems connected to the power control system. CCN stands for Cloud Condensation Nuclei Analyzer.

[0064] The PCASP circuit breaker is used to control overload protection of the PCASP subsystem of the weather modification system without affecting other weather modification system subsystems connected to the power control system. PCASP stands for Passive Cavity Aerosol Sounder.

[0065] The CCP circuit breaker is used to control overload protection of the CCP subsystem of the weather modification system without affecting other weather modification system subsystems connected to the power control system. CCP stands for Cloud Combination Detector.

[0066] The PIP circuit breaker is used to control overload protection of the PIP subsystem of the weather modification system without affecting other weather modification system subsystems connected to the power control system. PIP stands for Precipitation Imaging System.

[0067] The AIMMS circuit breaker is used to control overload protection of the AIMMS subsystem of the weather modification system without affecting other weather modification subsystems connected to the power control system. AIMMS stands for Aircraft Integrated Meteorological Measurement System.

[0068] The ZBT-LC-01 circuit breaker is used to control overload protection of the ZBT-LC-01R subsystem of the weather modification system without affecting other weather modification system subsystems connected to the power control system. ZBT-LC-01 stands for Cloud Particle Spectrometer.

[0069] The ZBT-LC-02 circuit breaker is used to control overload protection of the ZBT-LC-02 subsystem of the weather modification system without affecting other weather modification system subsystems connected to the power control system. The ZBT-LC-02 refers to the cloud particle imager.

[0070] ZBT-LC-03 circuit breaker for controlling the YGDS / C subsystem overload protection of the weather modification system without affecting other weather modification system subsystems connected to the power control system. Wherein ZBT-LC-03 means precipitation particle imager.

[0071] YGDS / C circuit breaker for controlling the YGDS / C system overload protection of the weather modification system without affecting other weather modification system subsystems connected to the power control system. Wherein YGDS / C means atmospheric data gathering pod.

[0072] Industrial computer circuit breaker for controlling the industrial computer / display subsystem overload protection of the weather modification system without affecting other weather modification system subsystems connected to the power control system.

[0073] Further, the 12 subsystems of the toggle switch module are respectively:

[0074] GVR toggle switch, the input end of the GVR toggle switch is connected with the output end of the GVR circuit breaker, for controlling the power control system to input power to the GVR subsystem of the weather modification system.

[0075] KPR toggle switch, the input end of the KPR toggle switch is connected with the output end of the KPR circuit breaker, for controlling the power control system to input power to the KPR subsystem of the weather modification system.

[0076] CCN toggle switch, the input end of the CCN toggle switch is connected with the output end of the CCN circuit breaker, for controlling the power control system to input power to the CCN subsystem of the weather modification system.

[0077] PCASP toggle switch, the input end of the PCASP toggle switch is connected with the output end of the PCASP circuit breaker, for controlling the power control system to input power to the PCASP subsystem of the weather modification system.

[0078] CCP toggle switch, the input end of the CCP toggle switch is connected with the output end of the CCP circuit breaker, for controlling the power control system to input power to the CCP subsystem of the weather modification system.

[0079] PIP toggle switch, the input end of the PIP toggle switch is connected with the output end of the PIP circuit breaker, for controlling the power control system to input power to the PIP subsystem of the weather modification system.

[0080] An AIMMS toggle switch, the input end of which is connected to the output end of the AIMMS circuit breaker, is used to control the power supply control system to input power to the AIMMS subsystem of the weather modification system.

[0081] A ZBT-LC-01 toggle switch, the input end of which is connected to the output end of the ZBT-LC-01 circuit breaker, for controlling the power supply control system to input power to the ZBT-LC-01 subsystem of the weather modification system.

[0082] A ZBT-LC-02 toggle switch, the input end of which is connected to the output end of the ZBT-LC-02 circuit breaker, and is used to control the power supply control system to input power to the ZBT-LC-02 subsystem of the weather modification system.

[0083] A ZBT-LC-03 toggle switch, the input end of which is connected to the output end of the ZBT-LC-03 circuit breaker, is used to control the power supply control system to input power to the ZBT-LC-03 subsystem of the weather modification system.

[0084] A YGDS / C toggle switch, the input end of which is connected to the output end of the YGDS / C circuit breaker, is used to control the power supply control system to input power to the YGDS / C subsystem of the weather modification system.

[0085] The industrial computer switches the power switch, the input end of which is connected to the output end of the industrial computer circuit breaker, for controlling the power control system to input power to the industrial computer / display subsystem of the weather modification system.

[0086] This embodiment adds an external aircraft power system and 12 weather modification subsystems to the complete power control system. These subsystems are: GVR, KPR, CCN, PCASP, CCP, PIP, AIMMS, ZBT-LC-01, ZBT-LC-02, ZBT-LC-03, and YGDS / C.

[0087] The aircraft power system uses the existing power supply on the aircraft to provide a 28V voltage for the power control system device of the present invention. The solution of this embodiment is to combine the existing power supply on the aircraft with the power control system device technology of the present invention.

[0088] GVR subsystem, the input end of the GVR subsystem is connected to the output end of the GVR toggle switch.

[0089] KPR subsystem, the input end of the KPR subsystem is connected to the output end of the KPR toggle switch.

[0090] CCN subsystem, the input end of the CCN subsystem is connected to the output end of the CCN toggle switch.

[0091] PCASP subsystem, the input end of the PCASP subsystem is connected to the output end of the PCASP toggle switch.

[0092] CCP subsystem, the input end of the CCP subsystem is connected to the output end of the CCP toggle switch.

[0093] PIP subsystem, the input end of the PIP subsystem is connected to the output end of the PIP toggle switch.

[0094] AIMMS subsystem, the input end of the AIMMS subsystem is connected to the output end of the AIMMS toggle switch.

[0095] ZBT-LC-01 subsystem, the input end of the ZBT-LC-01 subsystem is connected to the output end of the ZBT-LC-01 toggle switch.

[0096] ZBT-LC-02 subsystem, the input end of the ZBT-LC-02 subsystem is connected to the output end of the ZBT-LC-02 toggle switch.

[0097] ZBT-LC-03 subsystem, the input end of the ZBT-LC-03 subsystem is connected to the output end of the ZBT-LC-03 toggle switch.

[0098] YGDS / C subsystem, the input end of the YGDS / C subsystem is connected to the output end of the YGDS / C toggle switch.

[0099] Industrial computer / display, the input end of the industrial computer / display is connected to the output end of the industrial computer toggle switch.

[0100] In this embodiment, the master control switch and contactor obtain a 28V voltage from the aircraft power system, the master control circuit breaker provides overload protection for the entire power control system device, and the circuit breaker module's circuit breaker provides overload protection for each subsystem of the artificial weather modification system. The toggle switch of the toggle switch module then controls the distribution of voltage to each subsystem added to the artificial weather modification system. The voltage distributed to each subsystem added to the artificial weather modification system is uniformly 28V.

[0101] The contactor obtains 28V voltage from the aircraft power system, and the master control switch controls the on and off of the contactor, thereby controlling the aircraft's 28V power supply to provide 28V voltage to the entire power control system device.

[0102] The master circuit breaker monitors the cumulative load current of the aircraft's 28V power supply. The master circuit breaker has a fuse as a safety feature. When the current exceeds the limit, the fuse blows, tripping the master circuit breaker and breaking the circuit.

[0103] The circuit breakers for all subsystems in the circuit breaker module monitor the load current of the 28V power supply for each subsystem of the aircraft power control system. All subsystem circuit breakers in the circuit breaker module have internal fuses as safety features. When the current is too high, the fuse blows, the master control circuit breaker opens, and the circuit is disconnected.

[0104] Aircraft equipped with the power control device for an airborne weather modification system can automatically monitor and protect the power control of the weather modification system without crew intervention, eliminating the need for any auxiliary equipment or facilities. When a subsystem overloads, the corresponding subsystem's circuit breaker automatically trips, cutting off power to the corresponding system. When all subsystems are simultaneously overloaded, the master control circuit breaker automatically trips, shutting off power to the aircraft's power control system, thereby protecting the aircraft's power system.

[0105] Finally, it should be noted that the above are merely preferred embodiments of the present invention and are not intended to limit the present invention. Those skilled in the art will readily appreciate that the present invention is susceptible to various modifications and variations. The embodiments and features of the embodiments of this application may be combined arbitrarily without conflict. Any modifications, equivalent substitutions, and improvements made within the spirit and principles of the present invention are intended to be within the scope of protection of the present invention.

Claims

1. A power supply control system device for an airborne weather modification system, characterized in that: include: The master control switch is used to control the power input of the entire power control system device; Master control circuit breaker, used for overload protection of the load of the entire power control system device; A contactor, one input end of the contactor is connected to the output end of the master control circuit breaker, and the other input end is connected to the output end of the master control switch, for controlling the power supply input of the entire power control system device; a circuit breaker module, wherein the input end of the circuit breaker module is connected to the output end of the contactor, and the circuit breaker module includes circuit breakers for m subsystems, and is used for overload protection of each subsystem of the weather modification system; wherein m is not less than 1; A toggle switch module, wherein the m input terminals of the toggle switch module are connected to the corresponding m output terminals of the circuit breaker module, and the toggle switch module includes toggle switches of m subsystems, which are used to control the separate power supply input of each subsystem of the artificial weather modification system.

2. The power control system device for an airborne weather modification system according to claim 1, characterized in that: The circuit breaker module includes circuit breakers for 12 subsystems, which are: GVR circuit breaker, used to control overload protection of the GVR subsystem of the weather modification system; KPR circuit breaker, used to control overload protection of the KPR subsystem of the weather modification system; CCN circuit breaker, used to control overload protection of the CCN subsystem of the weather modification system; PCASP circuit breaker, used to control overload protection of the PCASP subsystem of the weather modification system; CCP circuit breaker, used to control overload protection of the CCP subsystem of the weather modification system; PIP circuit breaker, used to control overload protection of the PIP subsystem of the weather modification system; AIMMS circuit breakers, used for overload protection of the AIMMS subsystem that controls the weather modification system; The ZBT-LC-01 circuit breaker is used to control overload protection of the ZBT-LC-01R subsystem of the weather modification system; ZBT-LC-02 circuit breaker, used to control overload protection of the ZBT-LC-02 subsystem of the weather modification system; ZBT-LC-03 circuit breaker, used for overload protection of the YGDS / C subsystem controlling the weather modification system; YGDS / C circuit breakers are used for overload protection of the industrial computer / display subsystem that controls the weather modification system.

3. The power control system device for an airborne weather modification system according to claim 2, characterized in that: The toggle switch module includes 12 subsystem toggle switches, which are: a GVR toggle switch, wherein the input end of the GVR toggle switch is connected to the output end of the GVR circuit breaker and is used to control the power supply control system to input power to the GVR subsystem of the weather modification system; a KPR toggle switch, wherein the input end of the KPR toggle switch is connected to the output end of the KPR circuit breaker and is used to control the power supply control system to input power to the KPR subsystem of the weather modification system; a CCN toggle switch, wherein the input end of the CCN toggle switch is connected to the output end of the CCN circuit breaker and is used to control the power supply control system to input power to the CCN subsystem of the weather modification system; a PCASP toggle switch, wherein an input end of the PCASP toggle switch is connected to an output end of the PCASP circuit breaker and is used to control the power supply control system to input power to the PCASP subsystem of the weather modification system; a CCP toggle switch, wherein the input end of the CCP toggle switch is connected to the output end of the CCP circuit breaker and is used to control the power supply control system to input power to the CCP subsystem of the weather modification system; a PIP toggle switch, wherein the input end of the PIP toggle switch is connected to the output end of the PIP circuit breaker and is used to control the power supply control system to input power to the PIP subsystem of the weather modification system; an AIMMS toggle switch, wherein an input end of the AIMMS toggle switch is connected to an output end of the AIMMS circuit breaker and is used to control the power supply control system to input power to the AIMMS subsystem of the weather modification system; A ZBT-LC-01 toggle switch, wherein the input end of the ZBT-LC-01 toggle switch is connected to the output end of the ZBT-LC-01 circuit breaker, and is used to control the power supply control system to input power to the ZBT-LC-01 subsystem of the weather modification system; A ZBT-LC-02 toggle switch, wherein the input end of the ZBT-LC-02 toggle switch is connected to the output end of the ZBT-LC-02 circuit breaker, and is used to control the power supply control system to input power to the ZBT-LC-02 subsystem of the weather modification system; A ZBT-LC-03 toggle switch, wherein the input end of the ZBT-LC-03 toggle switch is connected to the output end of the ZBT-LC-03 circuit breaker, and is used to control the power supply control system to input power to the ZBT-LC-03 subsystem of the weather modification system; a YGDS / C toggle switch, wherein the input end of the YGDS / C toggle switch is connected to the output end of the YGDS / C circuit breaker and is used to control the power supply control system to input power to the YGDS / C subsystem of the weather modification system; The industrial computer switches the power switch, the input end of which is connected to the output end of the industrial computer circuit breaker, for controlling the power control system to input power to the industrial computer / display subsystem of the weather modification system.

4. The power control system device of an airborne weather modification system according to any one of claims 1 to 3, characterized in that: The contactor is a normally open contactor. When the master control switch is pressed, the contactor is controlled to be turned on and the circuit is turned on; when the master control switch is lifted, the contactor is controlled to be turned off and the circuit is turned off.

5. The power control system device of an airborne weather modification system according to any one of claims 1 to 3, characterized in that: The internal safety structure of the master control circuit breaker is a fuse.

6. The power control system device of an airborne weather modification system according to any one of claims 1 to 3, characterized in that: The internal safety structure of the circuit breakers of all subsystems in the circuit breaker module is a fuse.

7. The power control system device of an airborne weather modification system according to any one of claims 1 to 3, characterized in that: The master control switch is an aviation-specific toggle switch.

8. The power control system device of an airborne weather modification system according to any one of claims 1 to 3, characterized in that: The toggle switches of all subsystems in the toggle switch module are aviation-specific toggle switches.

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