CN107240956A - A kind of method of supplying power to and electric supply installation of rocket movable launch platform - Google Patents

Abstract

The invention discloses a power supply method and a power supply device for a rocket movable launching platform. Each electrical equipment is powered, and the two parallel generator sets form the first hot backup power supply system of the main and backup dual circuits; wherein, the process of the rocket transition includes the walking period and the maintenance test stage; the device includes : Power input module, first generator set, second generator set, first power generation monitoring module, second power generation monitoring module, output control module and ground power transfer box. The invention innovatively integrates multiple hot backup power supply systems on the movable launch platform, effectively solving the problems of poor portability and low reliability caused by the power supply of traditional power supply vehicles, so as to ensure reliable power supply of the large movable launch platform.

Description

Power supply method and power supply device for rocket movable launch platform

technical field

The invention relates to the technical field of rocket launching, and more specifically, the invention relates to a power supply method and a power supply device for a rocket movable launch platform.

Background technique

The power supply of the conventional rocket mobile launch platform often depends on the power supply vehicle, and the work of the rocket mobile launch platform is powered by a specially designed power supply vehicle. Especially in the transition process of the rocket launch platform, the power supply of the rocket launch platform must be realized by the way that the power supply vehicle follows the rocket launch platform. The mobile launch platform moves in unison, and it is necessary to ensure that the power supply capacity of the power supply vehicle is not affected by its own movement, which requires very high levels of internal components and operators of the power supply vehicle. However, even if a large amount of manpower and material resources are invested to maintain the reliable power supply of the mobile launch platform by the power supply vehicle, this power supply method still has problems such as poor reliability and poor convenience.

Therefore, how to improve the reliability and convenience of the power supply of the rocket mobile launch platform has become a technical problem to be solved urgently and the focus of research by those skilled in the art.

Contents of the invention

In order to solve the problems of poor reliability and poor portability of the existing power supply vehicle following the movement of the rocket movable launch platform to realize power supply, the present invention innovatively proposes a power supply method and power supply device for the rocket movable launch platform, and innovatively integrates the hot backup system Installed on the movable platform, it effectively solves the problems of unreliable power supply and inconvenient carrying of the power supply vehicle in the conventional solution, and significantly improves the stability of the power supply of the rocket's movable launch platform.

In order to achieve the above-mentioned technical purpose, the present invention discloses a power supply method for a rocket movable launch platform. Provide power for each electrical equipment on the active launch platform, and the two parallel generator sets form the first hot backup power supply system of the main and backup dual circuits; wherein, the process of the rocket transition includes the walking period and the maintenance test stage.

The invention innovatively integrates a hot backup power supply system on the active launch platform, and realizes effective power supply to the active launch platform during the transition process through two parallel generator sets, thus effectively solving the problem of poor portability and reliability caused by the power supply of traditional power supply vehicles Low reliability and other issues, thereby ensuring reliable power supply for large-scale event launch platforms.

Further, in the technical position and/or the launching position, the electrical equipment on the active launching platform is powered by means of an external mains power supply.

In different working stages of the rocket launch platform, the present invention innovatively adopts different power supply modes according to different working stages, which not only improves the flexibility of power supply, but also effectively protects the first hot backup system and improves the service life of the first hot backup system and other technical purposes.

Further, in the technical position and/or launch position, the electrical equipment on the active launch platform is powered by an external UPS power supply, and the UPS power supply and the external mains power supply jointly form a primary and secondary dual-circuit Two hot backup power supply system.

Based on the improved technical solution above, the present invention implements a hot backup power supply design for the whole process during the transition of the rocket, when it is in the technical position and/or the launch position, thereby ensuring the reliability of the power supply.

Further, the active launch platform is alternately powered by the first hot backup power supply system and the second hot backup power supply system.

The invention innovatively links the power supply mode with the working state of the movable launch platform, and the present invention can select the most reliable and stable power supply mode in a targeted manner under different working conditions of the movable launch platform.

Further, the circuits between the first hot backup power supply system and the second hot backup power supply system are interlocked, and the switching between the above two hot backup power supply systems is completed through a PC-level dual power switch.

The present invention avoids possible power supply conflicts between the first hot backup power supply system and the second hot backup power supply system by means of circuit interlocking, and realizes the power supply conflict between the two power supply systems by setting a special switching switch. Fast and stable switching, thus further improving the stability of power supply.

Based on the above-mentioned improved technical solution, the present invention realizes the alternate power supply and fast switching of the external power supply and the generator set power supply, and the circuit interlocking between the two, thereby realizing the real-time and convenience of the whole process of power supply.

Further, the second hot backup power supply system further includes a ground power transfer box arranged between the mains and the electric equipment and between the UPS power supply and the electric equipment.

By setting the ground power supply transfer box, the present invention can provide a more reliable and stable power supply for the movable launch platform, and avoid the possible failure of the mains or UPS power supply from affecting the movable launch platform.

Further, both the first hot backup power supply system and the second hot backup power supply system adopt signal grounding, equipment protection grounding and lightning protection grounding.

The invention effectively protects the power supply system through multiple grounding modes, thereby improving the power supply stability of the rocket launching platform.

Further, the various electrical equipment includes drive control equipment, hydraulic oil source equipment, heating equipment, air conditioning equipment, and room lighting equipment.

The invention realizes the power supply for all electrical equipment on the rocket launch platform, ensures reliable and stable power supply for these equipment, and provides effective support for the normal operation of the equipment in the rocket launch platform.

Further, during the transition of the rocket, the voltage, current, frequency, and power of the two parallel generator sets are collected and monitored respectively, and when the voltage, current, frequency, and power exceed their corresponding preset When the range is set, the alarm will be graded.

Further, the power of the two parallel generator sets is 260KW.

In order to achieve the above-mentioned technical purpose, the present invention also provides a power supply device for a rocket movable launch platform, the power supply device comprising:

Power input module, used to supply power to each subsystem;

a first generating set for generating electricity;

a second generator set for generating electricity;

A first power generation monitoring module, connected to the first generator set, for monitoring the first generator set, and outputting the electric energy generated by the first generator set;

The second power generation monitoring module is connected to the second generator set, and is used to monitor the second generator set and output the electric energy generated by the second generator set;

An output control module, connected to the first power generation monitoring module and the second power generation monitoring module, for parallelizing or decoupling the first generating set and the second generating set, and supplying power to the power input module , the power supply of the first generator set and the power supply of the second generator set are switched and controlled;

The ground power transfer box is connected to the power input module and the output control module, and is used to supply power to each subsystem under the control of the output control module.

The AC power supply device provided by the present invention has a redundant hot backup design for the external power supply and the power supply of the environmental protection generating set, which ensures the reliability of power supply. The external power supply and the power supply of the environmental protection generator set are alternately powered and quickly switched, and the circuit between the two is interlocked, realizing the real-time and convenience of the whole process of power supply.

Further, the device also includes:

The first alarm module is connected to the first power generation monitoring module, and is used to give an alarm when the first power generation monitoring module monitors the first generating set to be abnormal;

The second alarm module is connected to the second power generation monitoring module, and is configured to give an alarm when the second power generation monitoring module monitors the second generating set to be abnormal.

Further, the device also includes:

A platform monitoring module, connected to the output control module, used to monitor the power supply device, and control the power supply of the output control module to the power input module, the power supply of the first generator set and the second generator set switching control of the power supply;

A power distribution combination module, the power distribution combination module is connected to the ground power transfer box, and is used to perform power distribution combination distribution for the distribution box between the pre-equipment and the system between the pre-equipment; the platform monitoring module, through the The power distribution combination module is connected to the output control module;

A grounding device, the grounding device is connected to the power supply device for providing grounding protection.

Further, the power input module includes a main cable module and a backup cable module.

The beneficial effects of the present invention are: based on the first hot backup system installed on the active launch platform of the rocket, combined with the second hot backup system, the present invention significantly improves each power consumption on the active launch platform through at least two hot backup systems. The safety, convenience and reliability of equipment electricity.

Description of drawings

Fig. 1 is a functional block diagram of the power supply and distribution of the rocket movable launch platform of the present invention.

Fig. 2 is a functional block diagram of the TN-S system involved in the present invention.

Fig. 3 is a schematic diagram of a grounding device provided by an embodiment of the present invention.

detailed description

The power supply method and power supply device of a rocket mobile launch platform of the present invention will be explained and described in detail below in conjunction with the accompanying drawings.

Embodiment one:

As shown in Figures 1, 2, and 3, the rocket movable launch platform involved in the present invention is a large-scale movable launch platform, and the power supply and distribution system of the large-scale movable launch platform is an important supporting equipment of the movable launch platform. Provide sufficient and suitable power for the active launch platform drive control system, air-conditioning system and room lighting through the power generation of the generator set, and realize the power supply for the pre-equipment room system, platform environment monitoring equipment and other equipment through the power distribution combination equipment; and In the technical position and the launch position, the power supply can be provided for the control equipment in the pre-equipment room by transferring the mains power, and it can also provide power for the drive control system, air conditioning system, hydraulic oil source and heater. In order to ensure the reliability of the power supply and distribution system and ensure the normal power supply of key systems, the invention proposes to be installed on the platform, which can realize the whole process of power supply, which includes the power supply during the walking period and the maintenance test stage of the large-scale movable launching platform, and realizes the thermal Backup power supply and distribution system. The invention changes the previous method of using a power supply vehicle to follow the movement of the platform to realize power supply, and effectively improves the convenience and reliability of power supply and distribution. The specific description of this invention is as follows.

A power supply method for a movable launch platform of a rocket. During the transition of a rocket, power is supplied to each electrical device on the movable launch platform by means of two parallel generator sets installed on the movable launch platform, and the two parallel generators The generating set forms the first hot backup power supply system of the main and standby circuits; in the present embodiment, the generating set can be an environment-friendly generating set, and the process of the rocket transition includes the walking period and the maintenance test stage, and this process adopts the power supply system of the present invention. The method can ensure reliable power supply of key systems on the active launch platform of the rocket. In this embodiment, the power of the two parallel generator sets is 260KW, and each electrical equipment includes drive control equipment, hydraulic oil source equipment, heating equipment, air conditioning equipment, and room lighting equipment. The number of generating sets is two, of course, under the enlightenment of the present invention, more than two generating sets connected in parallel can also be used. More specifically, two 260kW generator sets are connected in parallel to supply power to the drive and other systems during the transition process of the mobile launch platform. The two sets can operate independently or in parallel. The two units have the functions of automatic parallel connection and automatic load distribution. When working in parallel, the two units can provide electric energy for the load at the same time. During the operation of the unit, any unit can be paralleled or disassembled at any time according to the needs, and the output switching control of the unit power supply and the mains power can be realized to ensure the normal power supply and distribution system of the rocket launch platform during the transition process. powered by.

In the technical position and/or launch position, power the electrical equipment on the active launch platform by means of an external mains power supply. In the technical position and/or launch position, the electrical equipment on the active launch platform is powered by an external UPS power supply. In this embodiment, the external UPS power supply voltage is 380V, and the UPS power supply and the external mains power supply jointly form a The second hot backup power supply system of the main and backup dual circuits, not only that, the present invention also adopts a hot backup design for the external mains power supply, the main and backup cables take power from the ground mains of the factory building, and pass The power transfer connects the mains power to the distribution boxes of each system located in Zone 1 of the pre-equipment room, and the main and backup output sockets of the distribution boxes of each subsystem supply power to the subsystems at the same time to realize hot backup power supply. The active launch platform is alternately powered by the first hot backup power supply system and the second hot backup power supply system, thereby improving the reliability of power supply. The circuits between the first hot backup power supply system and the second hot backup power supply system are interlocked, and the present invention completes the switching between the above two hot backup power supply systems through a PC-level dual power switch. Compared with the traditional switch driven by a motor, the switching switch has the advantages of simple structure, rapid switching and the like. The switching appliance has automatic and manual switching modes. In the automatic mode, it can automatically complete the conversion between the two power sources according to the power supply status; in the manual mode, press the power conversion button to switch between the two power sources, realizing the whole process of power supply. real-time and convenience.

In addition, the second hot backup power supply system also includes a ground power transfer box installed between the mains and the electrical equipment and between the UPS power supply and the electrical equipment. The power supply to each electrical equipment is completed through the ground power transfer box. Both the first hot backup power supply system and the second hot backup power supply system adopt signal grounding, equipment protection grounding and lightning protection grounding. As shown in Figure 2, in this embodiment, there is a protective ground terminal in the power supply connector, and the power supply system is a TN-S system: this system has five wires, namely three phase wires A, B, C, and one middle wire A neutral line N and a protective line PE, only one point of the power system power supply transformer is grounded, and the exposed conductive part of the electrical equipment is connected to the PE line. The advantage is that there is no current on the PE line during normal operation, so the exposed conductive parts of the equipment do not present a voltage to ground. It is also easy to cut off the power supply in the event of an accident. Therefore, the present invention adopts this scheme to make the power supply safer and can be used in places with relatively harsh environmental conditions. In addition, because there is no current on the PE line, it has strong electromagnetic applicability, so it is also suitable for power supply in systems such as data processing and precision detection devices. After the protection ground of each subsystem is led out through the power supply connector, the shell of each cabinet can be overlapped with the launch platform body at the same time, and grounded through the body grounding device. The grounding of the power supply and distribution system includes signal grounding, equipment protection grounding, and lightning protection grounding, and the three grounds are isolated from each other in the active launch platform, and are connected to the ground network at a single point outside the active launch platform.

The present invention collects and monitors the voltage, current, frequency, and power of two parallel generator sets during the rocket transition process, and performs hierarchical alarms when the voltage, current, frequency, and power exceed their corresponding preset ranges . Specifically, information collection is realized through the generator set controller, and various parameters in the operation process of the power supply and distribution system are displayed in real time through the liquid crystal display unit. When the system fails, graded alarms are issued according to the fault level, so that corresponding measures can be taken in time , to protect the reliability of the system power supply. The power supply and distribution system involved in the present invention has complete protection measures. When a fault occurs, it will immediately alarm and automatically cut off or stop power supply; it has overload and short-circuit protection for each electrical circuit; it also has protection measures to prevent misoperation, such as preventing asynchronous closing Electrical interlocking circuits for accidents, etc. On the basis of the present invention, a convenient human-computer interaction interface and a parameter storage unit can also be designed, which facilitates system failure analysis and system maintenance. The control acquisition system collects and displays the three-phase voltage, three-phase current, frequency, and power parameters of the mains/generator; at the same time, it realizes the control operation, synchronous parallel operation and status monitoring of the two units, and can realize the automatic start/stop of the generator set, Data measurement and storage, alarm and protection functions, and can realize the switching control of mains power and unit power. Mains has over-voltage, under-voltage, over-frequency, under-frequency, phase loss, and reverse phase sequence detection functions, and generator sets also have over-voltage, under-voltage, over-frequency, under-frequency, over-current, over-power, reverse power, Phase and reverse phase sequence detection function.

It should be noted that "and/or" in the present invention should be understood as three situations, that is, "A and/or B" means that A, B and AB exist simultaneously.

Embodiment two:

As shown in Figures 1, 2, and 3, this embodiment provides an AC power supply device, including:

Power input module, used to supply power to each subsystem;

a first generating set for generating electricity;

a second generator set for generating electricity;

The first power generation monitoring module is connected to the first generating set, and is used to monitor the first generating set and output the electric energy generated by the first generating set;

The second power generation monitoring module is connected to the second generator set, and is used to monitor the second generator set and output the electric energy generated by the second generator set;

The output control module is connected with the first power generation monitoring module and the second power generation monitoring module, and is used for paralleling or separating the first generator set and the second generator set, and supplying power to the power input module, the power supply of the first generator set and the second generator set The power supply of the generating set is switched and controlled;

The ground power transfer box is connected to the power input module and the output control module, and is used to accept the control of the output control module to supply power to each subsystem.

The AC power supply device provided by the embodiment of the present invention can be installed on the platform, can supply power in the whole process (during walking and maintenance test phase), and has a redundant hot backup power supply and distribution system to ensure reliable power supply of key systems.

Wherein, the movable launch platform is powered by mains power in the factory building, and supplies power to each power system of the movable launch platform through a power distribution system (including at least a power input module) installed on the platform, as an optional option in the embodiment of the present invention In the implementation mode, the power input module includes a main cable module and a backup cable module; the main and backup dual-way hot backup is adopted to ensure reliable power supply of these key systems. As an implementation of the embodiment of the present invention, the ground power transfer box is also connected to the power distribution box between the pre-equipment rooms, and is used to provide electric energy for the power distribution box between the pre-equipment rooms. Specifically, the redundant design of mains power of the power supply and distribution system uses the main and backup cables to take power from the ground mains of the factory building, connect it to the UPS power transfer box on the active launch platform, and then use the main and backup cables to get power from the UPS power supply. The transfer box is connected to the main and standby input terminals of the power distribution box in the pre-equipment room located in Zone 1, and cables of different current specifications are used to connect the output terminals of the main and standby sub-system circuit breakers in the power distribution box The main and backup input terminals of the distribution boxes of each subsystem, and the main and backup output sockets of the distribution boxes of each subsystem supply power to the subsystems at the same time, realizing redundant hot backup power supply. As an optional implementation of the embodiment of the present invention, the power supply device further includes: a power distribution combination module, which is connected to the ground power transfer box, and is used to perform power distribution on the distribution box between the pre-equipment room and the system between the pre-equipment room Power distribution combination assignment.

At the same time, the mobile launch platform is powered by two generator sets (the first generator set and the second generator set) installed on the platform in parallel hot backup during the walking process to ensure reliable power supply to the drive and other systems. Specifically, during the transition process, the active launch platform is powered by two 260kW generator sets connected in parallel to drive and other systems. The two sets can operate independently or in parallel. The two units have the functions of automatic parallel connection and automatic load distribution. When working in parallel, the two units can provide electric energy for the load at the same time. During the operation of the unit, any unit can be paralleled or disassembled at any time according to the needs, and the output switching control of the unit power supply and the mains power can be realized to ensure the normal power supply of the power supply and distribution system of the platform during the transition process. Therefore, the full redundant hot backup design of the power supply and distribution system ensures the reliability of the power supply and distribution system when supplying power to key systems

It can be seen that both the external power supply and the power supply of the environmental protection generator set have redundant hot backup design to ensure the reliability of power supply. The external power supply and the power supply of the environmental protection generator set are alternately powered and quickly switched, and the circuit between the two is interlocked, realizing the real-time and convenience of the whole process of power supply.

As an optional implementation of the embodiment of the present invention, the power supply device further includes: a first alarm module, connected to the first power generation monitoring module, and used to give an alarm when the first power generation monitoring module monitors the first generator set for abnormality; The alarm module is connected to the second power generation monitoring module, and is used for giving an alarm when the second power generation monitoring module monitors the second generating set to be abnormal. Specifically, through the alarm module, a system fault can be reported in time during operation, and corresponding protection measures can be taken to ensure the safety of the power supply of the system. The power supply and distribution system has complete protection measures. In case of failure, it will immediately alarm and automatically cut off or stop power supply; overload and short circuit protection of each electrical circuit; protection measures to prevent misoperation, such as electrical interlock to prevent asynchronous closing accidents circuit etc. Fault display and protection functions include: high temperature warning, high temperature shutdown alarm, low oil pressure warning, low oil pressure shutdown alarm, overspeed shutdown alarm, low fuel level warning, high battery voltage warning, low battery voltage warning, load Overcurrent shutdown alarm, start failure alarm, shutdown failure alarm, emergency shutdown alarm, oil pressure sensor open circuit alarm, temperature sensor open circuit alarm, etc.

As an optional implementation of the embodiment of the present invention, the power supply device further includes: a platform monitoring module, connected to the output control module, for monitoring the power supply device, and controlling the output control module to supply power to the power input module, the first generator set The power supply of the power supply and the power supply of the second generator set are switched and controlled. In order to facilitate system failure analysis and system maintenance, a platform monitoring module (such as a human-computer interaction interface and a parameter storage unit) and the like can also be set on the power supply device. Through the human-computer interaction interface, the control operation, synchronous parallel operation and status monitoring of the two units can be controlled, and the automatic start/stop, data measurement and storage, alarm and protection functions of the generator set can be realized, and the utility power and the unit can be monitored. Electric switching control. Mains has over-voltage, under-voltage, over-frequency, under-frequency, phase loss, and reverse phase sequence detection functions; power generation has over-voltage, under-voltage, over-frequency, under-frequency, over-current, over-power, reverse power, Reverse phase sequence detection function; collect and display mains/generator three-phase voltage, three-phase current, frequency, power parameters, etc. As an optional implementation of the embodiment of the present invention, the platform monitoring module is connected to the output control module through the power distribution combination module, so as to facilitate various application occasions.

In order to ensure the safety of personnel and equipment, a complete safety grounding device is designed. As an optional implementation of the embodiment of the present invention, the grounding device is connected to the power supply device to provide grounding protection. For the specific setting of the grounding device, reference may be made to FIG. 3 , which will not be described in detail here.

Any process or method descriptions in flowcharts or otherwise described herein may be understood to represent modules, segments or portions of code comprising one or more executable instructions for implementing specific logical functions or steps of the process , and the scope of preferred embodiments of the invention includes alternative implementations in which functions may be performed out of the order shown or discussed, including substantially concurrently or in reverse order depending on the functions involved, which shall It is understood by those skilled in the art to which the embodiments of the present invention pertain.

Those of ordinary skill in the art can understand that all or part of the steps carried by the methods of the above embodiments can be completed by instructing related hardware through a program, and the program can be stored in a computer-readable storage medium. During execution, one or a combination of the steps of the method embodiments is included.

In addition, the terms "first" and "second" are used for descriptive purposes only, and cannot be interpreted as indicating or implying relative importance or implicitly specifying the quantity of indicated technical features. Thus, the features defined as "first" and "second" may explicitly or implicitly include at least one of these features. In the description of the present invention, "plurality" means at least two, such as two, three, etc., unless specifically defined otherwise.

In the present invention, unless otherwise clearly specified and limited, terms such as "installation", "connection", "connection" and "fixation" should be understood in a broad sense, for example, it can be a fixed connection or a detachable connection , or integrated; it may be mechanically connected or electrically connected; it may be directly connected or indirectly connected through an intermediary, and it may be the internal communication of two components or the interaction relationship between two components, unless otherwise specified limit. Those of ordinary skill in the art can understand the specific meanings of the above terms in the present invention according to specific situations.

In the description of this specification, descriptions referring to the terms "this embodiment", "one embodiment", "some embodiments", "examples", "specific examples", or "some examples" mean that the embodiments are combined A specific feature, structure, material, or characteristic described by or example is included in at least one embodiment or example of the present invention. In this specification, the schematic representations of the above terms are not necessarily directed to the same embodiment or example. Furthermore, the described specific features, structures, materials or characteristics may be combined in any suitable manner in any one or more embodiments or examples. In addition, those skilled in the art can combine and combine different embodiments or examples and features of different embodiments or examples described in this specification without conflicting with each other.

The above descriptions are only preferred embodiments of the present invention, and are not intended to limit the present invention. Any modifications, equivalent replacements and simple improvements made on the essence of the present invention should be included in the protection scope of the present invention. Inside.

Claims (10)

1. a kind of method of supplying power to of rocket movable launch platform, it is characterised in that：During rocket transition, by being installed on The mode of two generating sets in parallel on movable launch platform is each power supply for electrical equipment on movable launch platform, and Described two generating sets in parallel form the first Hot Spare electric power system of active and standby two-way；Wherein, the mistake of the rocket transition Journey include walking during and the checking experiment stage.

2. the method for supplying power to of rocket movable launch platform according to claim 1, it is characterised in that：Technical area and/ Or be the power supply for electrical equipment on movable launch platform by way of external mains supply during launching site.

3. the method for supplying power to of rocket movable launch platform according to claim 2, it is characterised in that：Technical area and/ Or be the power supply for electrical equipment on movable launch platform, the ups power by way of external ups power during launching site The second Hot Spare electric power system of active and standby two-way is collectively forming with the external mains supply.

4. the method for supplying power to of rocket movable launch platform according to claim 3, it is characterised in that：Pass through the described first heat Backup electric power system and the second Hot Spare electric power system are the movable launch platform interleaved power.

5. the method for supplying power to of rocket movable launch platform according to claim 4, it is characterised in that：First Hot Spare Circuit interlock between electric power system and the second Hot Spare electric power system, above-mentioned two are completed by PC grades of double power supply converting switch Switching between individual Hot Spare electric power system.

6. the method for supplying power to of the rocket movable launch platform according to claim 3 or 5, it is characterised in that：Second heat Backup electric power system also includes being arranged at the ground power supply between civil power and electrical equipment and between ups power and electrical equipment Transfer box.

7. a kind of electric supply installation of rocket movable launch platform, it is characterised in that including：

Power Entry Module, for being powered for each subsystem；

First generating set, for being generated electricity；

Second generating set, for being generated electricity；

First generating monitoring module, connects first generating set, for being monitored to first generating set, and will The electric energy that first generating set is sent is exported；

Second generating monitoring module, connects second generating set, for being monitored to second generating set, and will The electric energy that second generating set is sent is exported；

Output control module, connects the first generating monitoring module and the second generating monitoring module, for side by side or First generating set described in off-the-line and second generating set, and to the powering of the Power Entry Module, first hair The power supply of group of motors and the power supply of the second generating set switch over control；

Ground power supply transfer box, connects the Power Entry Module and the output control module, for receiving the output control The control of molding block is powered to each subsystem.

8. the electric supply installation of rocket movable launch platform according to claim 7, it is characterised in that also include：

First alarm module, connects the first generating monitoring module, for described in the first generating monitoring module monitoring First generating set is alarmed when occurring abnormal；

Second alarm module, connects the second generating monitoring module, for described in the second generating monitoring module monitoring Second generating set is alarmed when occurring abnormal.

9. the electric supply installation of the rocket movable launch platform according to claim 7 or 8, it is characterised in that also include：

Platform monitoring modular, connects the output control module, for being monitored to the electric supply installation, and controls described defeated Go out control module to the powering of the Power Entry Module, the power supply of first generating set and the power supply of the second generating set Switch over control；

Distribution composite module, the distribution composite module connects the ground power supply transfer box, for distribution preposition equipment System carries out distribution combination distribution between case and preposition equipment；The platform monitoring modular, is connected by the distribution composite module The output control module；

Earthing or grounding means, the earthing or grounding means connects the electric supply installation, for providing ground protection.

10. the electric supply installation of rocket movable launch platform according to claim 7, it is characterised in that Power Entry Module Including leader cable module and standby cable module.