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CN113467278A - Man-machine interaction terminal for ground maintenance of airborne power system - Google Patents

Man-machine interaction terminal for ground maintenance of airborne power system Download PDF

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Publication number
CN113467278A
CN113467278A CN202110564031.XA CN202110564031A CN113467278A CN 113467278 A CN113467278 A CN 113467278A CN 202110564031 A CN202110564031 A CN 202110564031A CN 113467278 A CN113467278 A CN 113467278A
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China
Prior art keywords
power system
airborne
terminal
onboard
central computer
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CN202110564031.XA
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Inventor
王冲
周莹莹
张波
杨国勇
马欢
刘海港
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Shenyang Aircraft Design and Research Institute Aviation Industry of China AVIC
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Shenyang Aircraft Design and Research Institute Aviation Industry of China AVIC
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Priority to CN202110564031.XA priority Critical patent/CN113467278A/en
Publication of CN113467278A publication Critical patent/CN113467278A/en
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    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B19/00Programme-control systems
    • G05B19/02Programme-control systems electric
    • G05B19/04Programme control other than numerical control, i.e. in sequence controllers or logic controllers
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/40Testing power supplies

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Power Sources (AREA)

Abstract

本申请涉及一种机载电源系统地面维护人机交互终端,包括:终端显示器,与机载中心计算机连接;终端控制器,与机载中心计算机连接;机载中心计算机与各个机载电源系统传感器、机载电源系统信息采集电路连接,能够接收、显示各个机载电源系统传感器、机载电源系统信息采集电路的采集信息,终端显示器能够接收、显示该采集信息;机载中心计算机与各个机载电源系统执行终端、机载电源系统控制器连接,能够控制各个机载电源系统执行终端、机载电源系统控制器进行动作;终端控制器能够向机载中心计算机下发控制指令,使机载中心计算机根据控制指令控制控制各个机载电源系统执行终端、机载电源系统控制器进行相应的动作。

Figure 202110564031

The present application relates to a human-computer interaction terminal for ground maintenance of an airborne power supply system, including: a terminal display connected to an airborne central computer; a terminal controller connected to the airborne central computer; the airborne central computer and each airborne power supply system sensor , The airborne power supply system information collection circuit is connected to receive and display the collection information of each airborne power supply system sensor and the airborne power supply system information collection circuit, and the terminal display can receive and display the collected information; The power system execution terminal and the onboard power system controller are connected, and can control the actions of each onboard power system execution terminal and the onboard power system controller; the terminal controller can issue control instructions to the onboard center computer, so that the onboard center The computer controls and controls each onboard power system execution terminal and the onboard power system controller to perform corresponding actions according to the control instructions.

Figure 202110564031

Description

Man-machine interaction terminal for ground maintenance of airborne power system
Technical Field
The application belongs to the technical field of ground maintenance of airborne power systems, and particularly relates to a ground maintenance human-computer interaction terminal of an airborne power system.
Background
The airborne power supply system is the source and distribution center of the airplane electric energy, and during the ground maintenance work of the airplane, the airborne power supply system is comprehensively checked and maintained, so that the airborne power supply system is in a good state, and is important for safe flight of the airplane and execution of a mission of the airplane.
At present, the multi-functional display that sets up in the aircraft cockpit is mostly read the machine and is carried electrical power generating system state information in the ground maintenance work to and realize the control to machine carries electrical power generating system through the controlling means that sets up in the aircraft cockpit, carry out machine and carry out the operation, carry out machine and carry out the following defect in the operation, carry out the machine and carry out the control system and carry out the control of carrying out the control of:
in the aircraft ground maintenance work, the position that airborne power supply system needs to inspect, maintain is more, and distributes in full aircraft within range, and distribution range is wider, and multi-functional display and corresponding controlling means are fixed in aircraft cockpit, and the position that needs inspection, maintenance with most airborne power supply system has great space interval, read airborne power supply system state information and to airborne power supply system control inconvenient, the efficiency of serious influence to airborne power supply system ground maintenance, and can consume great manpower, material resources.
The present application has been made in view of the above-mentioned technical drawbacks.
It should be noted that the above background disclosure is only for the purpose of assisting understanding of the inventive concept and technical solutions of the present invention, and does not necessarily belong to the prior art of the present patent application, and the above background disclosure should not be used for evaluating the novelty and inventive step of the present application without explicit evidence to suggest that the above content is already disclosed at the filing date of the present application.
Disclosure of Invention
The present application is directed to an on-board power system ground maintenance human-computer interaction terminal that overcomes or mitigates at least one aspect of the technical deficiencies known to exist.
The technical scheme of the application is as follows:
a man-machine interaction terminal for ground maintenance of an airborne power system comprises:
the terminal display is connected with the airborne central computer;
the terminal controller is connected with the airborne central computer;
the airborne central computer is connected with each airborne power system sensor and each airborne power system information acquisition circuit, and can receive and display the acquired information of each airborne power system sensor and each airborne power system information acquisition circuit, and the terminal display can receive and display the acquired information;
the airborne central computer is connected with each airborne power system execution terminal and each airborne power system controller and can control each airborne power system execution terminal and each airborne power system controller to act;
the terminal controller can issue a control instruction to the airborne central computer, so that the airborne central computer controls each airborne power system execution terminal and the airborne power system controller to perform corresponding actions according to the control instruction.
According to at least one embodiment of the application, the central computer in the onboard power system ground maintenance human-computer interaction terminal is connected with the onboard power system sensors and the onboard power system information acquisition circuit in a non-bus mode.
According to at least one embodiment of the application, the onboard central computer in the onboard power system ground maintenance human-computer interaction terminal obtains corresponding fault information based on the received onboard power system sensors and the onboard power system information acquisition circuit, and the terminal display can receive and display the fault information.
According to at least one embodiment of the application, the onboard central computer in the onboard power system ground maintenance human-computer interaction terminal is connected with the non-bus between the execution terminals of the onboard power systems;
the airborne central computer is connected with each airborne power system controller through a bus.
According to at least one embodiment of the application, the terminal controller in the airborne power system ground maintenance human-computer interaction terminal is connected with the airborne central computer through a bus.
According to at least one embodiment of the application, in the above-mentioned ground maintenance human-computer interaction terminal for an onboard power system, a touch control area corresponding to each of an execution terminal for the onboard power system and a controller for the onboard power system is provided on a terminal display;
and the terminal controller is connected with the terminal display so as to respond to the touch control area being touched and issue a corresponding control instruction to the airborne central computer.
Drawings
Fig. 1 is a schematic diagram of a ground maintenance human-computer interaction terminal of an onboard power system according to an embodiment of the present application;
wherein:
1-terminal display; 2-airborne central computer; 3-an onboard power system sensor; 4-an onboard power system information acquisition circuit; 5-an execution terminal of the airborne power system; 6-onboard power system controller; 7-terminal controller.
For the purpose of better illustrating the embodiments, certain features of the drawings may be omitted, enlarged or reduced, and do not represent the size of an actual product; further, the drawings are for illustrative purposes, and terms describing positional relationships are limited to illustrative illustrations only and are not to be construed as limiting the patent.
Detailed Description
In order to make the technical solutions and advantages of the present application clearer, the technical solutions of the present application will be further clearly and completely described in the following detailed description with reference to the accompanying drawings, and it should be understood that the specific embodiments described herein are only some of the embodiments of the present application, and are only used for explaining the present application, but not limiting the present application. It should be noted that, for convenience of description, only the parts related to the present application are shown in the drawings, other related parts may refer to general designs, and the embodiments and technical features in the embodiments in the present application may be combined with each other to obtain a new embodiment without conflict.
In addition, unless otherwise defined, technical or scientific terms used in the description of the present application shall have the ordinary meaning as understood by one of ordinary skill in the art to which the present application belongs. The terms "upper", "lower", "left", "right", "center", "vertical", "horizontal", "inner", "outer", and the like used in the description of the present application, which indicate orientations, are used only to indicate relative directions or positional relationships, and do not imply that the devices or elements must have a specific orientation, be constructed and operated in a specific orientation, and when the absolute position of the object to be described is changed, the relative positional relationships may be changed accordingly, and thus, should not be construed as limiting the present application. The use of "first," "second," "third," and the like in the description of the present application is for descriptive purposes only to distinguish between different components and is not to be construed as indicating or implying relative importance. The use of the terms "a," "an," or "the" and similar referents in the context of describing the application is not to be construed as an absolute limitation on the number, but rather as the presence of at least one. The word "comprising" or "comprises", and the like, when used in this description, is intended to specify the presence of stated elements or items, but not the exclusion of other elements or items.
Further, it is noted that, unless expressly stated or limited otherwise, the terms "mounted," "connected," and the like are used in the description of the invention in a generic sense, e.g., connected as either a fixed connection or a removable connection or integrally connected; can be mechanically or electrically connected; they may be directly connected or indirectly connected through an intermediate medium, or they may be connected through the inside of two elements, and those skilled in the art can understand their specific meaning in this application according to the specific situation.
The present application is described in further detail below with reference to fig. 1.
A man-machine interaction terminal for ground maintenance of an airborne power system comprises:
the terminal display 1 is connected with the airborne central computer 2;
the terminal controller 7 is connected with the airborne central computer 2;
the airborne central computer 2 is connected with each airborne power system sensor 3 and each airborne power system information acquisition circuit 4, can receive and display the acquired information of each airborne power system sensor 3 and each airborne power system information acquisition circuit 4, and the terminal display 1 can receive and display the acquired information;
the airborne central computer 2 is connected with each airborne power system execution terminal 5 and each airborne power system controller 6, and can control each airborne power system execution terminal 5 and each airborne power system controller 6 to act;
the terminal controller 7 can issue a control instruction to the airborne central computer 2, so that the airborne central computer 2 controls each airborne power system execution terminal 5 and the airborne power system controller 6 to perform corresponding actions according to the control instruction;
feedback information of the actions of each onboard power system execution terminal 5 and the onboard power system controller 6 can be received and displayed by the onboard central computer 2, and the terminal display 1 can receive and display the feedback information.
For the above-mentioned ground maintenance man-machine interaction terminal of the onboard power system disclosed in the embodiment, those skilled in the art can understand that the onboard central computer 2 is the core of the aircraft information processing and control, is connected with each onboard power system sensor 3 and onboard power system information acquisition circuit 4, can receive and display the acquired information of each onboard power system sensor 3 and onboard power system information acquisition circuit 4, and is connected with each onboard power system execution terminal 5 and onboard power system controller 6, can control each onboard power system execution terminal 5 and onboard power system controller 6 to act, and designs that the terminal display 1 is connected with the onboard central computer 2, can receive and display the acquired information of each onboard power system sensor 3 and onboard power system information acquisition circuit 4 from the central computer 2, the state information of the airborne power system can be received and displayed, in addition, the terminal controller 7 is designed to be connected with the airborne central computer 2, and the airborne central computer 2 can control each airborne power system execution terminal 5 and the airborne power system controller 6 to perform corresponding actions, namely control of the airborne power system is achieved.
To the above-mentioned onboard power system ground maintenance human-computer interaction terminal disclosed in the embodiment, a skilled person in the art can understand that, in the aircraft ground maintenance work, a relevant technical person can carry the human-computer interaction terminal to move in the aircraft space, so that the state information of the onboard power system can be conveniently read through the terminal display 1 at each part of the aircraft, and the onboard power system is controlled through the terminal controller 7, thereby greatly improving the efficiency of the onboard power system ground maintenance, and saving manpower and material resources.
In some optional embodiments, the central computer 2 in the above-mentioned ground maintenance human-computer interaction terminal for an onboard power system is non-bus connected with each of the sensors 3 of the onboard power system and the information acquisition circuit 4 of the onboard power system.
In some optional embodiments, the onboard central computer 2 in the above-mentioned onboard power system ground maintenance human-computer interaction terminal obtains corresponding fault information based on the received onboard power system sensors 3 and the onboard power system information acquisition circuit 4, and the terminal display 1 can receive and display the fault information.
In some optional embodiments, the onboard central computer 2 in the onboard power system ground maintenance human-computer interaction terminal is not in bus connection with each onboard power system execution terminal 5;
the onboard central computer 2 is connected with each onboard power system controller 6 through a bus.
In some optional embodiments, the terminal controller 7 in the above-mentioned ground maintenance human-computer interaction terminal for the onboard power system is connected with the onboard central computer 2 through a bus.
In some optional embodiments, in the above-mentioned ground maintenance human-computer interaction terminal for an onboard power system, the terminal display 1 has a touch control area corresponding to each of the onboard power system execution terminal 5 and the onboard power system controller 6;
the terminal controller 7 is connected with the terminal display 1 so as to respond to the touch control area being touched and issue a corresponding control instruction to the onboard central computer 2.
For the above-mentioned man-machine interaction terminal for ground maintenance of an onboard power system disclosed in the embodiment, those skilled in the art can understand that the terminal display 1 and the terminal controller 7 are integrated, and on the basis that the terminal display 1 can display the state information of the onboard power system, the onboard power system can be controlled through the touch control area on the terminal display, so that the terminal is convenient to carry and use.
The embodiments are described in a progressive manner in the specification, each embodiment focuses on differences from other embodiments, and the same and similar parts among the embodiments are referred to each other.
Having thus described the present application in connection with the preferred embodiments illustrated in the accompanying drawings, it will be understood by those skilled in the art that the scope of the present application is not limited to those specific embodiments, and that equivalent modifications or substitutions of related technical features may be made by those skilled in the art without departing from the principle of the present application, and those modifications or substitutions will fall within the scope of the present application.

Claims (6)

1. The utility model provides an airborne power system ground maintenance human-computer interaction terminal which characterized in that includes:
the terminal display (1) is connected with the airborne central computer (2);
the terminal controller (7) is connected with the airborne central computer (2);
the airborne central computer (2) is connected with each airborne power system sensor (3) and each airborne power system information acquisition circuit (4) and can receive and display the acquired information of each airborne power system sensor (3) and each airborne power system information acquisition circuit (4), and the terminal display (1) can receive and display the acquired information;
the airborne central computer (2) is connected with each airborne power system execution terminal (5) and each airborne power system controller (6) and can control each airborne power system execution terminal (5) and each airborne power system controller (6) to act;
the terminal controller (7) can issue a control instruction to the airborne central computer (2), so that the airborne central computer (2) controls each airborne power system execution terminal (5) and the airborne power system controller (6) to perform corresponding actions according to the control instruction.
2. The ground-based maintenance human-computer interaction terminal of the onboard power system according to claim 1,
the central computer (2) is connected with the airborne power system sensors (3) and the airborne power system information acquisition circuit (4) in a non-bus manner.
3. The ground-based maintenance human-computer interaction terminal of the onboard power system according to claim 1,
the onboard central computer (2) obtains corresponding fault information based on the received onboard power system sensors (3) and the onboard power system information acquisition circuit (4), and the terminal display (1) can receive and display the fault information.
4. The ground-based maintenance human-computer interaction terminal of the onboard power system according to claim 1,
the airborne central computer (2) is connected with each airborne power system execution terminal (5) in a non-bus manner;
and the airborne central computer (2) is connected with each airborne power system controller (6) through a bus.
5. The ground-based maintenance human-computer interaction terminal of the onboard power system according to claim 4,
the terminal controller (7) is connected with the airborne central computer (2) through a bus.
6. The ground-based maintenance human-computer interaction terminal of the onboard power system according to claim 1,
the terminal display (1) is provided with a touch control area corresponding to each airborne power system execution terminal (5) and each airborne power system controller (6);
the terminal controller (7) is connected with the terminal display (1) so as to respond to the touch control area being touched and issue a corresponding control instruction to the airborne central computer (2).
CN202110564031.XA 2021-05-24 2021-05-24 Man-machine interaction terminal for ground maintenance of airborne power system Pending CN113467278A (en)

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CN116123926A (en) * 2022-12-30 2023-05-16 中国人民解放军32382部队 Weapon equipment car electricity detecting system based on multi-bus multi-signal

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CN104803009A (en) * 2015-04-27 2015-07-29 中国航空工业集团公司沈阳飞机设计研究所 Unmanned aerial vehicle (UAV) ground comprehensive detection system and UAV ground comprehensive detection method
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CN116123926A (en) * 2022-12-30 2023-05-16 中国人民解放军32382部队 Weapon equipment car electricity detecting system based on multi-bus multi-signal

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