CN213123505U - Ground support equipment simulator for certain airplane avionics major - Google Patents
Ground support equipment simulator for certain airplane avionics major Download PDFInfo
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- CN213123505U CN213123505U CN202021752223.0U CN202021752223U CN213123505U CN 213123505 U CN213123505 U CN 213123505U CN 202021752223 U CN202021752223 U CN 202021752223U CN 213123505 U CN213123505 U CN 213123505U
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Abstract
The utility model discloses a certain type of aircraft avionics specialty ground support equipment simulator, including handcart and takan simulator, handcart left end surface is provided with the handle, the handcart front end left side has set gradually wireless compass signal simulator, microwave landing signal simulator, beacon signal simulator and takan simulator from top to bottom, instrument landing signal simulator, voler signal simulator, altimeter height signal simulator and radar warning equipment signal simulator have set gradually from top to bottom in the middle of the handcart front end surface, the handcart front end right side has set gradually air traffic buffer stop, time synchronizer, outfield inspection tester and accessory case from top to bottom, the handcart bottom surface is provided with the universal wheel; the utility model has the advantages of realize work process demonstration, analog training, function demonstration, maintenance operation demonstration, the degree of synthesis is high, the reliability is high, with low costs, convenient to use.
Description
Technical Field
The utility model belongs to the technical field of the flight training technique and specifically relates to a certain type aircraft avionics specialty ground support equipment simulator is related to.
Background
The ground support equipment simulation equipment mainly provides environment signals or external simulation signals required by the take-off, flight and landing of the airplane for the comprehensive simulation training platform, such as flight altitude, compass direction, tower radio signals, tacon signals, landing signals, time signals and the like, after the simulation training platform receives the simulation signals provided by the ground, the simulation training platform firstly calculates the signals, then carries out logic analysis and forwards the data to corresponding avionic equipment, and after each simulated avionic equipment receives the data after settlement, the simulation training platform acts on a corresponding display interface, a virtual instrument, an indicator light and a corresponding execution mechanism to simulate various phenomena of the airplane during the take-off, flight and landing, and provides teaching environment and training guidance for students and instructors;
at present, airplanes are more and more complex, the expenses of the airplanes are more and more expensive, the expense cost needed by airplane drivers and airplane crew members for airplane training and testing is more expensive relative to other products, so that the airplane testing and data collection are generally tested by adopting an analog simulation technology at present, the airplane flight training needs to be matched with ground guarantee equipment for matching, the ground guarantee equipment can better solve the training problem of operation skills, the practical ability and the training effect of trainees can be better cultured, meanwhile, the existing simulation equipment has poor overhauling effect on radio stations, so the airplane training and flight training are very necessary, and therefore, a certain airplane avionics professional ground guarantee equipment simulator is provided.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a certain type aircraft avionics specialty ground support equipment simulator with realize work process demonstration, analog training, function demonstration, maintenance operation demonstration, the degree of synthesis is high, the reliability is high, with low costs, convenient to use, has solved the problem among the prior art.
The above utility model discloses an above-mentioned utility model purpose can realize through following technical scheme: certain type aircraft avionics specialty ground support equipment simulator, including handcart and tacan simulator, its characterized in that: handcart left end surface is provided with the handle, handcart front end left side has set gradually wireless compass signal simulator, microwave landing signal simulator, beacon signal simulator and tacan simulator from top to bottom, instrument landing signal simulator, volr signal simulator, altimeter height signal simulator and radar warning device signal simulator have set gradually from top to bottom in the middle of the handcart front end surface, handcart front end right side has set gradually air traffic buffer stop, time synchronization appearance, outfield inspection appearance and annex case from top to bottom, the handcart bottom surface is provided with the universal wheel.
The utility model discloses further set up to: the air traffic collision avoidance device is embedded inside the trolley and used for simulating traffic signals of the GPS.
Through adopting above-mentioned technical scheme, be used for simulating GPS's traffic signal through air traffic buffer stop to and the dangerous barrier that probably meets during the flight, make the early warning to the dangerous condition, prevent accident, guarantee flight safety.
The utility model discloses further set up to: the instrument landing signal simulator simulates a signal when the aircraft landing mode is meter wave landing.
By adopting the technical scheme, when the instrument landing signal simulator has a fault, red 'meter wave' characters are displayed near the downward sliding deviation pointer, and a red rectangular frame appears around the 'meter wave' characters, so that the warning effect is achieved.
The utility model discloses further set up to: the microwave landing signal simulator simulates a signal when the aircraft landing mode is microwave landing.
By adopting the technical scheme, the microwave landing signal simulator is used for simulating the changes of instruments and data during landing, when the microwave signal simulator breaks down, red microwave characters are displayed at the original position close to the platform, and a red rectangular frame is added outside the characters.
The utility model discloses further set up to: the beacon signal simulator is used for simulating the passing state of the airplane passing through different navigation stations in the flying process.
By adopting the technical scheme, the beacon signal simulator is used for simulating the beacon signals of a far station, a middle station and a near station generated by a ground pointing beacon station.
The utility model discloses further set up to: the altimeter height signal simulator can simulate the height signal of the altimeter and display the height value.
By adopting the technical scheme, the altimeter signal simulator can be used for detecting whether the radio altimeter on the airplane can accurately detect the flying altitude of the airplane or not, and reminding a pilot through alarm prompt tones such as decision altitude and the like.
The utility model discloses further set up to: four groups of universal wheels are arranged, and the universal wheels are uniformly arranged at four corners of the bottom of the trolley.
Through adopting above-mentioned technical scheme, can be convenient remove the use to the device through the universal wheel design, improve the mobility that uses.
To sum up, the utility model discloses a beneficial technological effect does:
1. when the simulator is used, structurally, the ground support equipment simulation equipment is integrated on a trolley and is connected with an external power supply through a cable to supply power to the simulator, when various radio stations on an airplane are detected, the ground simulator simulates the wave channel and frequency of a radio station and transfers a certain radio station on the airplane to the same wave channel and frequency as a navigation station, if the radio station on the airplane can be normally communicated, the radio station is proved to be good, and if the radio station cannot be normally communicated, the radio station needs to be overhauled so as to achieve the effect of conveniently overhauling the radio station;
2. structurally, simulated imitation pieces and devices such as a device-free related time synchronizer, an outfield inspection tester and a radar warning device signal simulator are utilized, simulation training software of the air traffic collision avoidance device is matched, an operation platform capable of repeatedly performing simulation training is provided for crew training personnel, and the simulation device has the advantages of being high in comprehensive degree, comprehensive in training level, strong in function expansion capability and the like, simple in structure and high in practicability.
Drawings
FIG. 1 is a schematic diagram of the overall structure of a ground support equipment simulator for the avionics specialty of a certain type of the present invention;
FIG. 2 is a schematic view of the front view structure of the ground support equipment simulator for the avionics specialty of the aircraft of the present invention;
FIG. 3 is a schematic diagram of a side view structure of a ground support equipment simulator for the avionics specialty of the aircraft of the present invention;
FIG. 4 is a schematic view of the flow of the detection aircraft radio station of the ground support equipment simulator for the avionics specialty of the present invention;
fig. 5 is an interactive flow diagram of the ground support equipment simulator for the avionics specialty of the aircraft of the present invention.
In the figure, 1, a trolley; 2. a wireless compass signal simulator; 3. a handle; 4. a microwave landing signal simulator; 5. a beacon signal simulator; 6. a Takang simulator; 7. a universal wheel; 8. a volt signal simulator; 9. an instrument landing signal simulator; 10. an altimeter height signal simulator; 11. a radar warning device signal simulator; 12. an air traffic collision avoidance device; 13. a time synchronizer; 14. an outfield inspection instrument; 15. an accessory case.
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 ground support equipment simulator for the special aviation and electric specialties of the airplane disclosed by the utility model, the ground support equipment simulator comprises a handcart 1 and a tacan simulator 6, wherein the surface of the left end of the handcart 1 is provided with a handle 3, and the left side of the front end of the handcart 1 is sequentially provided with a wireless compass signal simulator 2, a microwave landing signal simulator 4, a beacon signal simulator 5 and a tacan simulator 6 from top to bottom;
in this embodiment, when in use, the ground support equipment simulation device is integrated on a trolley 1, a power socket is configured inside the trolley 1, the power socket supplies power to the simulator through a cable, the wireless compass signal simulator 2 provides simulation signals for the radio compass, such as azimuth signals and heading signals of the compass, the instrument landing signal simulator 9 simulates signals of the airplane during the 'meter wave landing', and when a pilot selects a landing mode on a control panel of a cockpit to be meter wave landing, the airplane needs to be communicated with a ground tower at the moment;
the instrument landing signal simulator is used for simulating a ground signal emitted by a tower when the instrument lands, the numerical values of the downward slip deviation and the azimuth deviation are generated by the instrument landing signal simulator 9 in the ground simulation signal, when the value changes, the glide deviation and the azimuth deviation on the flight display change along with the change, the signal of the airplane during the microwave landing is simulated by the microwave landing signal simulator 4 to simulate the change of instruments and data during the landing, the beacon signal simulator 5 is used for simulating the beacon signals of a far station (400 Hz), a middle station (1300 Hz) and a near station (3000 Hz) generated by a ground pointing beacon station, when the simulator switches from different frequency values of a point slip or continuous area, the signal of the beacon station is transmitted in the comprehensive simulation training station, the orientation signal can be sent to the airplane through the Tacan simulator 6, and the airplane is guided to fly according to the appointed course.
Referring to fig. 1 and 2, an instrument landing signal simulator 9, a volr signal simulator 8, an altimeter height signal simulator 10 and a radar warning device signal simulator 11 are sequentially arranged in the middle of the front end surface of the trolley 1 from top to bottom;
in this embodiment, the voler signal simulator 8 is used to simulate a navigation station base station to send information to an airplane, if various stations on the airplane need to be detected, the ground simulator simulates the channel and frequency of a radio station, and turns a radio station on the airplane to the same channel and frequency as the navigation station, if the radio station on the airplane can normally talk, the radio station is good, if the radio station cannot talk, the radio station needs to be overhauled, the altimeter height signal simulator 10 can simulate the height signal of an altimeter, when the altitude value sent by the altimeter simulator is received, the altitude value is compared with the decision altitude, when the radio altitude is detected to be lower than the decision altitude, all the pilots 'decision altitude warning' voices are heard in the earphones, the warning voices are repeated twice to remind the pilots of paying attention to the airplane altitude so as to avoid danger, the type of alert signal is simulated by the radar warning device signal simulator 11.
Referring to fig. 2 and 3, the air traffic collision avoidance device 12, the time synchronizer 13, the outfield inspection instrument 14 and the accessory box 15 are sequentially arranged on the right side of the front end of the trolley 1 from top to bottom, and the universal wheels 7 are arranged on the bottom surface of the trolley 1;
in the embodiment, the universal wheel 7 is driven by the handle 3 to change the moving position of the device, the device is convenient to use, the air traffic anti-collision device 12 is used for simulating a traffic signal of a GPS and a dangerous obstacle which can be met during flying, the outfield inspection instrument 14 is used for inspecting information such as an output mode, a wave channel, a net number and the like, the time of a tower and the time of an aerial hour hand on an airplane are synchronized by the time synchronizer 13, calculation is carried out by the simulation training platform, the aerial clock is controlled, the time is synchronized to the time transmitted by the tower, the time calibration is completed, and files are conveniently stored by the accessory box 15.
Referring to fig. 1, the air traffic collision avoidance device 12 is embedded inside the trolley 1, the air traffic collision avoidance device 12 is used for simulating a traffic signal of a GPS, and the air traffic collision avoidance device 12 is used for simulating a traffic signal of a GPS and a dangerous obstacle which may be encountered during flight, so as to warn a dangerous situation, prevent accidents and ensure flight safety.
Referring to fig. 2, the instrument landing signal simulator 9 simulates a signal when the aircraft landing mode is "meter wave landing", and when a fault occurs in the instrument landing signal simulator 9, red "meter wave" characters are displayed near the glide deviation pointer, and a red rectangular frame appears around the "meter wave" characters to play a role of warning.
Referring to fig. 2, the microwave landing signal simulator 4 simulates a signal when the aircraft landing mode is microwave landing, and the microwave landing signal simulator 4 is used for simulating changes of instruments and data during landing, so that when the microwave signal simulator breaks down, red microwave characters are displayed at the original position close to the platform, and a red rectangular frame is added outside the characters.
Referring to fig. 2, the beacon signal simulator 5 is used for simulating the station passing state of the aircraft passing through different navigation stations during the flight, and the beacon signal simulator 5 is used for simulating the beacon signals of a far station, a middle station and a near station generated by a ground pointing beacon station.
Referring to fig. 2, the altimeter signal simulator 10 may simulate an altitude signal of an altimeter to display an altitude value, and may be configured to detect whether a radio altimeter on an aircraft can accurately detect a flying altitude of the aircraft, and to alert a pilot through an alarm tone such as a decision altitude.
Referring to fig. 1, the universal wheels 7 are provided with four groups, the universal wheels 7 are uniformly arranged at four corners of the bottom of the trolley 1, the device can be conveniently moved and used through the design of the universal wheels 7, and the using maneuvering performance is improved.
The implementation principle of the embodiment is as follows:
the utility model discloses a certain type aircraft avionics specialty ground security equipment simulator, during the use, ground security equipment simulation equipment is integrated on a handcart 1, the handcart 1 is internally provided with a power socket, power is supplied to the simulator through a cable, analog signals such as compass azimuth signal, course signal and the like are provided for a radio compass through a radio compass signal simulator 2, signals during the 'meter wave landing' of the aircraft are simulated through an instrument landing signal simulator 9, when a pilot selects the landing mode to be the meter wave landing on a control panel of a cockpit, the aircraft needs to keep communication with a ground tower at the moment, the instrument landing signal simulator is used for simulating the ground signals transmitted by the tower during the instrument landing, the numerical values of the downward slip deviation and the azimuth deviation are generated by the instrument landing signal simulator 9 in the ground analog signals, when the numerical value changes, the downward slip deviation and the azimuth deviation on a flight display change along with the change, simulating a signal of the airplane during microwave landing by using the microwave landing signal simulator 4 to simulate changes of instruments and data during landing;
the beacon signal simulator 5 is used for simulating beacon signals of a far station (400 Hz), a middle station (1300 Hz) and a near station (3000 Hz) which are generated by a ground pointing beacon station, when the simulator switches from different frequency values of a point slip or a continuous area, in the comprehensive simulation training station which transmits the beacon station signals, the Takong simulator 6 can be used for transmitting direction signals for the airplane and guiding the airplane to fly according to a specified course, the Voll signal simulator 8 is used for simulating a navigation station base station to transmit information to the airplane, if various electric stations on the airplane need to be detected, the ground simulator simulates the wave channel and frequency of a radio station and adjusts a certain radio station on the airplane to the same wave channel and frequency as the navigation station, if the radio station on the airplane can be normally communicated, the radio station is proved to be good, if the communication cannot be normally communicated, the radio station needs to be overhauled, the altimeter altitude signal simulator 10 can simulate the altitude signal of the altimeter, when receiving the altitude value sent by the altimeter simulator, comparing with the decision altitude, when detecting that the radio altitude is lower than the decision altitude, all the pilots will hear the decision altitude warning sound, the warning sound is repeated twice to remind the pilots to pay attention to the aircraft altitude to avoid danger, the radar warning device signal simulator 11 simulates the type warning signal, the universal wheel 7 is driven by the handle 3 to change the mobile position of the device, the device is convenient to use, the air traffic anti-collision device 12 simulates the traffic signal of GPS and the dangerous obstacles which can be encountered during flying, the external field inspection instrument 14 is used for inspecting the information of output mode, wave channel, network number and the like, the tower time and the aviation hour time on the aircraft are synchronized by the time synchronizer 13, the simulation training platform is used for calculating, the aviation clock is controlled, the time is synchronized to the launching time of the tower, the time calibration is completed, and files are conveniently stored through the accessory box 15, so that the technical problem in the prior art is solved.
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 (7)
1. Certain type aircraft avionics specialty ground support equipment simulator, including handcart (1) and ta kang simulator (6), its characterized in that: handcart (1) left end surface is provided with handle (3), handcart (1) front end left side has set gradually wireless compass signal simulator (2), microwave landing signal simulator (4), beacon signal simulator (5) and tacan simulator (6) from top to bottom, instrument landing signal simulator (9), voler signal simulator (8), altimeter height signal simulator (10) and radar warning equipment signal simulator (11) have set gradually from top to bottom in the middle of handcart (1) front end surface, handcart (1) front end right side has set gradually air traffic buffer stop (12), time synchronization appearance (13), external field inspection appearance (14) and annex case bottom surface (15) from top to bottom, handcart (1) is provided with universal wheel (7).
2. An aircraft avionics professional ground support equipment simulator according to claim 1, characterized in that: the air traffic anti-collision device (12) is embedded in the trolley (1), and the air traffic anti-collision device (12) is used for simulating a traffic signal of a GPS.
3. An aircraft avionics professional ground support equipment simulator according to claim 1, characterized in that: the instrument landing signal simulator (9) simulates signals when the aircraft landing mode is meter wave landing.
4. An aircraft avionics professional ground support equipment simulator according to claim 1, characterized in that: the microwave landing signal simulator (4) simulates signals when the aircraft landing mode is microwave landing.
5. An aircraft avionics professional ground support equipment simulator according to claim 1, characterized in that: the beacon signal simulator (5) is used for simulating the passing state of the airplane passing through different navigation stations in the flying process.
6. An aircraft avionics professional ground support equipment simulator according to claim 1, characterized in that: the altimeter height signal simulator (10) can simulate the height signal of the altimeter and display a height value.
7. An aircraft avionics professional ground support equipment simulator according to claim 1, characterized in that: the trolley is characterized in that four groups of universal wheels (7) are arranged, and the universal wheels (7) are uniformly arranged at four corners of the bottom of the trolley (1).
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| Application Number | Priority Date | Filing Date | Title |
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| CN202021752223.0U CN213123505U (en) | 2020-08-20 | 2020-08-20 | Ground support equipment simulator for certain airplane avionics major |
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| CN202021752223.0U CN213123505U (en) | 2020-08-20 | 2020-08-20 | Ground support equipment simulator for certain airplane avionics major |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115065424A (en) * | 2022-08-18 | 2022-09-16 | 南京新频点电子科技有限公司 | Vehicle-mounted communication signal comprehensive simulation device |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115065424A (en) * | 2022-08-18 | 2022-09-16 | 南京新频点电子科技有限公司 | Vehicle-mounted communication signal comprehensive simulation device |
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