CN213123427U - Comprehensive simulation training platform for avionics specialty of certain type of transporter - Google Patents

Comprehensive simulation training platform for avionics specialty of certain type of transporter Download PDF

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Publication number
CN213123427U
CN213123427U CN202021752185.9U CN202021752185U CN213123427U CN 213123427 U CN213123427 U CN 213123427U CN 202021752185 U CN202021752185 U CN 202021752185U CN 213123427 U CN213123427 U CN 213123427U
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China
Prior art keywords
control box
avionics
specialty
certain type
training platform
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CN202021752185.9U
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Chinese (zh)
Inventor
张磊
贾德宇
曹乃森
黄家成
闫涛
黄国庆
白雪琪
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Air Force Engineering University of PLA Aircraft Maintenace Management Sergeant School
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Air Force Engineering University of PLA Aircraft Maintenace Management Sergeant School
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Abstract

The utility model discloses a comprehensive simulation training platform for the avionics major of a certain type of transport plane, which comprises a simulation operation platform and a main power switch, wherein one side of the simulation operation platform body is provided with a TACAN control box, an airborne friend-foe identification transponder, a centralized control panel, a combined receiving device control box, a short wave radio station control box and a near-earth warning system control box; the utility model has the advantages of realize work process demonstration, function demonstration, maintenance operation demonstration, comprehensive degree is high, the reliability is high, with low costs, convenient to use.

Description

Comprehensive simulation training platform for avionics specialty of certain type of transporter
Technical Field
The utility model belongs to the technical field of flight training technique and specifically relates to a simulation training platform is synthesized to certain type cargo airplane avionics specialty.
Background
Flight simulation (flight simulation) is based on professional technologies in the fields of system engineering, similar theory, control theory, computer technology, information technology and application thereof, takes a computer and various physical effect devices as tools, utilizes a mathematical model to be combined with partial real objects in an airplane, and carries out dynamic test and comprehensive application of research on an airplane system; in the training of aviation pilots, simulation training has become a main training means with safety, high efficiency and low cost, and even the training effect in some aspects (such as airplane emergency or fault handling training) exceeds that of the real-mounted flight training, so that the related technology of flight simulation is highly valued by the aviation world and the development of flying speed is achieved;
at present, the systematic skill training of aircraft crew mainly adopts a mode of combining classroom teaching with aircraft actual installation practice, the classroom teaching is mainly used for teaching by means of teaching aids such as multimedia courseware, wall map, templates and the like, a plurality of people can be trained simultaneously, the training efficiency is high, the teaching effect is better for principle teaching contents, but the problem of disjointed theoretical learning and practical operation exists, the training problem of operation skills can be better solved by the on-board actual installation practice, the practical ability of trainees can be better cultured, the training effect is good, but the training efficiency is lower due to the limitation of factors such as the number of airplanes, fields, time, weather, other professional work coordination, safety and the like, meanwhile, the frequent practice of trainees on actual aircraft not only influences the service life of the aircraft, but also generates fault hidden dangers and poses potential threats to flight safety, therefore, a comprehensive simulation training platform for the avionics specialty of a certain type of transporter is provided.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a certain type cargo airplane avionics specialty comprehensive simulation training platform with realize work process demonstration, function demonstration, maintenance operation demonstration, the degree of synthesis is high, the reliability is high, with low costs, convenient to use, solved the problem among the prior art.
The above utility model discloses an above-mentioned utility model purpose can realize through following technical scheme: a simulation training platform is synthesized to certain type cargo airplane avionics specialty, including emulation operation panel and master switch, its characterized in that: one side is equipped with ta kang control box, machine carries friend or foe identification transponder, centralized control board, combination receiving equipment control box, shortwave radio station control box and warning system control box near the ground on the emulation operation panel stage body, be equipped with master switch, display control board, passenger cabin display and built-in interphone control box in the middle of the emulation operation panel stage body, the right side is equipped with built-in conversation, air traffic warning, multifunctional control board, meteorological radar control box, radar warning device, passenger cabin audio recording system, inertial navigation equipment control box and infrared decoy input ware on the emulation operation panel stage body.
The utility model discloses further set up to: the short-wave radio station control box comprises an ultra-short-wave radio station I and an ultra-short-wave radio station II, can be controlled by the short-wave radio station control box, and can select a receiving/transmitting mode, a double receiving mode and a lifesaving mode.
Through adopting above-mentioned technical scheme, through the button operation on the short wave radio station control box, can set up each item parameter of two ultrashort wave radio stations, if the conversation adopts open-air speech or secret speech, number word mode, simple tone or two-tone mode, the conversation volume can be adjusted by volume knob.
The utility model discloses further set up to: the control box of the Takang is one of navigation equipment, and the control box of the Takang is adaptive to a Takang resolving indicator lamp.
Through adopting above-mentioned technical scheme, can realize empty/empty ranging function of carrying on of takang through the control box of takang, provide the navigation guidance for the aircraft, the pilot lamp is solved to takang and is used for instructing the result information of takang settlement, solves and successfully to show green, red scintillation when solving, and it shows red to solve the failure.
The utility model discloses further set up to: the display control panel and the multifunctional control panel are matched with each other for use.
By adopting the technical scheme, the method is used for controlling the display and control operation in the main flight display and the multifunctional display, such as selecting a landing mode, a true course or a magnetic course, a compass or a tacan for far azimuth, a decision altitude and field pressure information.
The utility model discloses further set up to: the centralized control board is a comprehensive device for controlling the avionics equipment, and a large screen display is arranged in the middle of the centralized control board.
By adopting the technical scheme, the avionics equipment operates and displays parameters and contents on the centralized control panel through the large-screen display, so that the simplicity and convenience of operation are improved.
The utility model discloses further set up to: the inertial navigation equipment control box is used for controlling navigation equipment, an alarm lamp is arranged on one side of the inertial navigation equipment, and three groups of band switches are arranged on the lower portion of the inertial navigation equipment control box.
By adopting the technical scheme, the corresponding parameters can be selected through the band switch, the inertial navigation equipment can be controlled, the warning lamp of the system fault is arranged at the upper right corner, the red color is lightened when the warning is given, the key on the red color lamp is pressed, and the warning reminding is turned off.
The utility model discloses further set up to: the infrared bait dispenser is used for dispensing foil strips and infrared baits.
By adopting the technical scheme, bait parameters to be thrown in, such as the number of foils, the number of points, the interval and the like, are set on the program set, then a corresponding throwing mode is selected on the control box, the throwing switch is pressed down, and the throwing quantity of the foils and the infrared rays is displayed on the display control box.
The utility model discloses further set up to: the cockpit audio recording system is used by carrying a flight data recorder.
By adopting the technical scheme, the system to be recorded can be opened or closed through the cockpit audio recording system and the flight data recorder, then the audio recorder is carried by the cockpit audio recording system for recording, and the data is stored in the flight data recorder and is used for restoring scenes and analyzing information.
The utility model discloses further set up to: the radar warning device is RKL204A and consists of a control box and a warning display and control device.
By adopting the technical scheme, the radar warning device is used for displaying the radar warning information, intercepting, analyzing and identifying enemy radar signals, judging the threat degree in real time and giving an alarm in time, and when a plurality of threats exist, sequencing according to the threat level so that a pilot or an operator can take countermeasures in time to defend themselves.
To sum up, the utility model discloses a beneficial technological effect does:
1. in the use process of the comprehensive simulation training platform for the avionics major of a certain type of transport plane, the teaching training functions such as working process demonstration, function demonstration, maintenance operation demonstration and the like are structurally realized through hardware simulation and matched simulation software, and the teaching functions such as learning of avionics major knowledge of the transport plane, training of maintenance skills, checking of training effects and the like are realized by utilizing devices such as a simulated simulation operating platform, a platform body related TACAN control box, an airborne friend-foe identification responder, a centralized control panel, a combined receiving equipment control box, a short-wave radio station control box and a near-to-earth warning system control box and the like and matching simulation software;
2. structurally, the simulation operating platform is structurally designed by adopting a console structure, avionics equipment simulated according to the ratio of 1:1 is installed on a front panel of the console, the operating method is basically consistent with that of the original airborne equipment, a main control computer is installed in an embedded mode, all back doors of the console can be opened, equipment installation and subsequent maintenance are facilitated, and the training platform has the characteristics of high comprehensive degree, comprehensive training levels, strong function expansion capability and the like, and is simple in structure and strong in practicability.
Drawings
FIG. 1 is a schematic view of the front view structure of a comprehensive simulation training platform for avionics specialty of a certain type of transport plane;
fig. 2 is the utility model discloses a side view structure schematic diagram of a certain type of cargo airplane avionics specialty comprehensive simulation training platform.
In the figure, 1, a simulation console; 2. a cockpit display; 3. a Takang control box; 4. an airborne friend or foe identification transponder; 5. a centralized control panel; 6. a combination receiving device control box; 7. a short-wave radio station control box; 8. a ground proximity warning system control box; 9. a main power switch; 10. a display control panel; 11. carrying out built-in conversation; 12. air traffic warning; 13. a multifunctional control panel; 14. a meteorological radar control box; 15. a radar warning device; 16. a cockpit audio recording system; 17. an inertial navigation device control box; 18. an infrared bait dispenser; 19. and a built-in interphone control box.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, rather than all embodiments, and all other embodiments obtained by a person of ordinary skill in the art without creative work belong to the protection scope of the present invention based on the embodiments of the present invention.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
Referring to fig. 1 and 2, for the utility model discloses a comprehensive simulation training platform for the avionics specialty of a certain type of transport plane, which comprises a simulation operation platform 1 and a master power switch 9, wherein a short-wave radio control box 7 is arranged on one side of the simulation operation platform 1, the master power switch 9 and a built-in interphone control box 19 are arranged in the middle of the simulation operation platform 1, and a built-in interphone 11 is arranged on the right side of the simulation operation platform 1;
in the embodiment, when the short wave radio station control box is used, a main power switch 9 is turned on, teaching and training functions such as working process demonstration, function demonstration, maintenance operation demonstration and the like are realized through hardware simulation and matched simulation software, the communication between an airplane and the ground, between the airplane and between the airplane and a satellite is realized through an in-machine call 11, the communication can also be carried out through the in-machine call 11, the information such as cockpit voice is recorded, the in-machine call 11 is switched on and off through an in-machine call controller 19, and the short wave radio station control box 7 is used for communication;
can set for the frequency of shortwave radio station through this control box, the work type, self-adaptation, frequency modulation communication, decide the communication frequently, parameter injection joint on the control box panel is for the navigation insertion interface, accessible this interface from the outside injects into each item parameter information for shortwave radio station control box 7, through the key-press operation on the control box, can set up each item parameter of ultrashort wave radio station I and ultrashort wave radio station II, adopt open-air or secret words, number word mode, simple tone or two-tone mode if the conversation, the conversation volume can be adjusted by volume knob.
Referring to fig. 1 and 2, a tacan control box 3, an onboard friend or foe identification transponder 4 and a combined receiving equipment control box 6 are arranged on one side of a platform body of a simulation operating platform 1;
in this embodiment, the combined receiving device control box 6 is a device for guiding an airplane to land, and can set modes such as microwave landing, instrument landing, volr landing, and the like, the tacan control box 3 is one of navigation devices and is a navigation device for indicating parameters such as azimuth, distance, and the like, and when channels, frequencies, and modes between two airplanes or an airplane and a navigation platform are consistent, the tacan can realize the empty/empty ranging function, and provide navigation guidance for the airplane;
the airborne friend-foe identification transponder 4 is used before an external identification card is inserted from the right side of the transponder, information of the identification card is deployed before battle, only friend machines participating in the battle can receive codes and can analyze correct code content information to realize intercommunication among airplanes, the information is sent in a coding mode, if the airplane is the airplane of the same party, the code content can be analyzed and translated into corresponding inquiry information, such as reporting the current flight altitude, reporting the codes of the airplane and reporting some special codes, and if the airplane is the enemy machine, the code content cannot be analyzed.
Referring to fig. 1 and 2, a centralized control board 5 is arranged on one side of the body of the simulation operating platform 1, a cockpit display 2 is arranged in the middle of the body of the simulation operating platform 1, and a multifunctional control board 13, a meteorological radar control box 14, an inertial navigation equipment control box 17 and an infrared bait dispenser 18 are arranged on the right side of the body of the simulation operating platform 1;
in the embodiment, the weather radar control box 14 knows various weather information through a weather radar, the infrared bait dispenser 18 is used for dispensing bait information, the enemy plane is puzzled through two dispensing modes of foil strip dispensing and infrared dispensing, the inertial navigation equipment control box 17 is used for controlling navigation equipment, the inertial navigation equipment can be controlled by matching with keys on a panel, the centralized control panel 5 is comprehensive equipment for controlling avionic equipment, and the centralized control panel 5 is used for operating and displaying;
the display control panel 10 and the multifunctional control panel 13 are used in cooperation with each other to control the display and control operation in the main flight display and the multifunctional display, such as selecting the landing mode, the true or magnetic heading, the azimuth far from being compass or tacan, the decision altitude, the field pressure information, etc., the ground proximity warning system control box 8 is a warning prompt when the airplane approaches the ground, and the cockpit display 2 is a display control instrument capable of displaying some information outside the airplane body, such as terrain information, landing gear, flap, wing measurement, wind direction, wind speed, air pressure, mach number, etc.
Referring to fig. 1, shortwave radio station control box 7 is including ultrashort wave radio station I and ultrashort wave radio station II, all can be controlled by shortwave radio station control box 7, and optional receipts/send mode, two modes of receiving, lifesaving mode through the button operation on the shortwave radio station control box 7, can set up each item parameter of two ultrashort wave radio stations, if the conversation adopts open-air speech or secret speech, number speech mode, simple tone or two-tone mode, the conversation volume can be adjusted by volume control knob.
Referring to fig. 1, a tacan control box 3 is one of navigation devices, the tacan control box 3 is adapted with a tacan resolving indicator light, the tacan control box 3 can achieve the function of empty/empty distance measurement of tacan, and provides navigation guidance for an airplane, the tacan resolving indicator light is used for indicating result information of tacan settlement, green is displayed when the tacan resolving is successful, red flickers when the tacan resolving is performed, and red is displayed when the tacan resolving is failed.
Referring to FIG. 1, the display control panel 10 and the multi-function control panel 13 are used in cooperation with each other to control the main flight display, the display in the multi-function display, and the control operations, such as selecting the landing mode, the true or magnetic heading, the far compass or tacon, the decision altitude, and the field pressure information.
Referring to fig. 2, the centralized control board 5 is a comprehensive device for controlling the avionics device, and a large screen display is arranged in the middle of the centralized control board 5, and the avionics device operates and displays parameters and contents on the centralized control board 5 through the large screen display, so that the simplicity of operation is improved.
Referring to fig. 1, an inertial navigation device control box 17 is a control navigation device, an alarm lamp is disposed on one side of the inertial navigation device, three sets of band switches are disposed on the lower portion of the inertial navigation device control box 17, and are used for selecting corresponding parameters through the band switches, the inertial navigation device can be controlled, the alarm lamp of a system fault is disposed on the upper right corner, when an alarm is given, the alarm lamp is red, a key on the red lamp is pressed, and alarm reminding is turned off.
Referring to fig. 2, the infrared bait dispenser 18 dispenses foil strips and infrared baits, and by setting bait parameters to be dispensed on a program set, such as the number of foil strips, the number of points, the intervals and the like, selecting a corresponding dispensing mode on the control box, pressing a dispensing switch, and displaying the number of foil strips and infrared baits on the display control box.
Referring to fig. 2, the cockpit audio recording system 16 is used by loading a flight data recorder, and the system to be recorded can be turned on or off through the cockpit audio recording system 16 and the flight data recorder, and then the audio recorder is loaded through the cockpit audio recording system 16 for recording, and the data is stored in the flight data recorder for restoring the scene and analyzing the information.
Referring to fig. 1, the radar warning device 15 is RKL204A, the radar warning device 15 is composed of a control box and a warning display and control device, and is used for displaying warning information of radar, intercepting, analyzing and identifying radar signals of enemies, judging threat degree in real time and giving a warning in time, and when a plurality of threats exist, sequencing according to threat levels so that a pilot or an operator can take countermeasures in time to defend themselves.
The implementation principle of the embodiment is as follows:
the utility model discloses a certain type of cargo airplane avionics specialty comprehensive simulation training platform, during the use, open main switch 9, through hardware simulation and supporting simulation software realization working process demonstration, teaching training functions such as function demonstration and maintenance operation demonstration, through built-in conversation 11 be used for realizing the intercommunication between aircraft and ground, between aircraft and the aircraft, between aircraft and the satellite, also can be used for carrying out built-in conversation 11, record cockpit voice information etc., built-in conversation ware control box 19 realizes using the break-make of built-in conversation 11, short wave radio station control box 7 is used for communicating;
the frequency, work type, self-adaptation, frequency modulation communication, fixed frequency communication of the short wave radio station can be set through the control box, a parameter injection joint on a panel of the control box is an aerial interface, various parameter information can be injected into the control box 7 of the short wave radio station from the outside through the interface, various parameters of the ultra-short wave radio station I and the ultra-short wave radio station II can be set through key operation on the control box, the communication adopts a clear communication mode or a secret communication mode, a digital communication mode, a single tone mode or a double tone mode, the communication volume can be adjusted by a volume adjusting knob, equipment for guiding the aircraft to land is combined with a receiving equipment control box 6, the modes of microwave landing, instrument landing, Vol landing and the like can be set, the Takang control box 3 is one of navigation equipment and is used for indicating navigation equipment of parameters such as azimuth, distance and the like, when wave channels, frequencies and modes between two aircrafts or the aircraft and the navigation stations, can realize the air/air ranging function of TACAN, provides navigation guidance for the airplanes, realizes the mutual communication between the airplanes because the airborne friend or foe identification transponder 4 belongs to the communication equipment, sends the information in a coding mode, if the aircraft is the airplane of our party, the coded content can be analyzed and translated into corresponding inquiry information, such as reporting the current flight altitude, reporting the code of the airplane, reporting some special codes, if the friend is the enemy, the coded content can not be analyzed, before the enemy is used, an external identification card needs to be inserted from the right side of the answering machine, the information of the identification card is deployed before battle, only the friend participating in the battle can receive the code, correct coded content information can be analyzed, the weather radar control box 14 can know various weather information through a weather radar, the infrared bait dispenser 18 is used for dispensing bait information, and two dispensing modes, namely foil strip dispensing and infrared dispensing, are used for puzzling enemies;
the inertial navigation equipment control box 17 is used for controlling the navigation equipment, can control the inertial navigation equipment by matching with keys on a panel, the centralized control panel 5 is comprehensive equipment used for controlling the avionic equipment, the display control panel 10 and the multifunctional control panel 13 are used in cooperation with each other through the centralized control panel 5 for operation and display, and are used for controlling the display and control operation in the main flight display and the multifunctional display, such as the selection of landing mode, true or magnetic heading, compass or tacan azimuth far away, decision altitude, field pressure information, etc., the ground proximity warning system control box 8 is the warning prompt when the airplane approaches the ground, the cockpit display 2 is the display control instrument, the aircraft can display some external information of the aircraft body such as terrain information, landing gear, flaps, wing measurement, wind direction, wind speed, air pressure, Mach number and the like, so as to solve the technical problems in the prior art.
Having shown and described the basic principles and principal features of the invention and advantages thereof, it will be apparent to those skilled in the art that the invention is not limited to the details of the foregoing exemplary embodiments, but is capable of other specific forms without departing from the spirit or essential characteristics thereof; the present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein, and any reference signs in the claims are not intended to be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.

Claims (9)

1. A simulation training platform is synthesized to certain type cargo airplane avionics specialty, including emulation operation panel (1) and main power switch (9), its characterized in that: one side is equipped with tacan control box (3), machine-carried friend or foe discernment answering machine (4), centralized control board (5), combination receiving equipment control box (6), short wave radio station control box (7) and ground warning system control box (8) on emulation operation panel (1) stage body, be equipped with in the middle of emulation operation panel (1) stage body master switch (9), display control board (10), passenger cabin display (2) and built-in interphone control box (19), right side is equipped with built-in conversation (11), air traffic warning (12), multifunctional control board (13), meteorological radar control box (14), radar warning device (15), passenger cabin audio frequency recording system (16), inertial navigation equipment control box (17) and infrared bait dispenser (18) on the emulation operation panel (1) stage body.
2. The comprehensive simulation training platform for the avionics specialty of a certain type of transport plane according to claim 1, characterized in that: short-wave radio set control box (7) are including ultrashort-wave radio set I and ultrashort-wave radio set II, all can be controlled by short-wave radio set control box (7), and optional receipts/mode, two receipts mode, lifesaving mode.
3. The comprehensive simulation training platform for the avionics specialty of a certain type of transport plane according to claim 1, characterized in that: the control box (3) is one of navigation equipment, and the control box (3) is adapted with a Takang resolving indicator lamp.
4. The comprehensive simulation training platform for the avionics specialty of a certain type of transport plane according to claim 1, characterized in that: the display control panel (10) and the multifunctional control panel (13) are matched with each other for use.
5. The comprehensive simulation training platform for the avionics specialty of a certain type of transport plane according to claim 1, characterized in that: the central control panel (5) is comprehensive equipment for controlling the avionics equipment, and a large screen display is arranged in the middle of the central control panel (5).
6. The comprehensive simulation training platform for the avionics specialty of a certain type of transport plane according to claim 1, characterized in that: the inertial navigation equipment control box (17) is used for controlling navigation equipment, an alarm lamp is arranged on one side of the inertial navigation equipment, and three groups of band switches are arranged on the lower portion of the inertial navigation equipment control box (17).
7. The comprehensive simulation training platform for the avionics specialty of a certain type of transport plane according to claim 1, characterized in that: the infrared bait dispenser (18) is used for dispensing foil strips and infrared baits.
8. The comprehensive simulation training platform for the avionics specialty of a certain type of transport plane according to claim 1, characterized in that: the cockpit audio recording system (16) is used with a flight data recorder.
9. The comprehensive simulation training platform for the avionics specialty of a certain type of transport plane according to claim 1, characterized in that: the radar warning device (15) is RKL204A, and the radar warning device (15) is composed of a control box and a warning display and control device.
CN202021752185.9U 2020-08-20 2020-08-20 Comprehensive simulation training platform for avionics specialty of certain type of transporter Expired - Fee Related CN213123427U (en)

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Application Number Priority Date Filing Date Title
CN202021752185.9U CN213123427U (en) 2020-08-20 2020-08-20 Comprehensive simulation training platform for avionics specialty of certain type of transporter

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Granted publication date: 20210504