TWM586442U - Aircraft navigation light simulation system - Google Patents

Abstract

An aircraft navigation light simulation system is used to solve the problem that the conventional aircraft navigation light system is controlled and difficult to be used for teaching and training. It can be used for the test of Class B technician certification for aircraft maintenance. The system includes: a teaching module, which generates several light switching signals; a test module, which has several switch units and relays, which switches the relays to generate several light test signals An output module with a display unit coupled to the teaching module and the relays, the display unit switches a plurality of lights according to the plurality of light switching signals and the plurality of light test signals; and a power module Group, electrically connecting the teaching module and the test module, and providing the power required to generate the light switching signal and the light test signal.

Description

Aircraft navigation light simulation system

This creation is about an electronic test device, especially an aircraft navigation light simulation system which can be used for teaching, training and examinations.

According to the aviation law, various lights, such as floor lights, taxi lights, strobe lights, must be installed on the outside of the aircraft, and related lights must be turned on or off at different stages of the flight. Warning of possible collisions, therefore, the aircraft's lighting system has the assistance to ensure the safety of the aircraft navigation and related operations.

In order to reduce flight safety issues, improve the proper rate of lighting systems, and strengthen the training of maintenance personnel, however, considering the flight safety of the aircraft and subject to the relevant aviation law regulations, it is not possible to use actual aircraft training and cannot be arbitrarily tested for operation. In addition, aerospace technology-related teaching practice equipment is expensive and not easy to popularize, which makes it difficult for schools and other training units to provide a proper aircraft navigation lighting system for educational training, making training less effective and extending the training time, resulting in human and material resources. Waste of resources.

In view of this, the conventional navigation light system does still need to be improved.

In order to solve the above problems, the purpose of this creation is to provide an aircraft navigation light simulation system, which can replace the actual machine operation and shorten the training time to save manpower and material resources.

The secondary purpose of this creation is to provide an aircraft navigation light simulation system, which can realize education and training combining vision, hearing and practical operation.

Another purpose of this creation is to provide an aircraft navigation light simulation system, which can be used as an exam test to quickly determine whether the component is damaged or human operation error to ensure that the test result is fair and correct.

Another purpose of this creation is to provide an aircraft navigation light simulation system, which can prevent line damage caused by current overload.

The use of the quantifier "a" or "an" in the elements and components recorded in the entire text of this work is only for convenience and to provide the general meaning of the scope of the work; in this work, it should be interpreted as including one or at least one, and a single The concept of plural also includes the plural case, unless it obviously means otherwise.

The creative aircraft navigation lighting simulation system includes: a teaching module that generates several light switching signals; a test module that has several switch units and several relays that switch the number Each relay generates several light test signals; an output module has a display unit coupled to the teaching module and the several relays, respectively, and the display unit switches according to the several light switching signals and the several light test signals. Several lights; and a power module, which is electrically connected to the teaching module and the test module, and provides the power required to generate the light switching signal and the light test signal.

Based on this, the aircraft navigation lighting simulation system created by this invention simulates the position and function of the actual aircraft navigation lighting system through the display unit, and the display module is used to switch the display unit with the teaching function; and the test module is used. Controlling the display unit has the effect of simulating the actual machine operation and performing the test.

The output module has a reminder unit, which is coupled to the test module, and the reminder unit sends a reminder signal according to the light test signals. In this way, a prompt can be given when the light test signal operates correctly, which has the function of checking the module function to avoid misjudging the test result.

The output module has a data unit, and the data unit displays the working voltage and working current of the output module in real time. In this way, the voltage and current of the output module can be monitored, which has the effect of maintaining stable operation and avoiding overload.

The power module is electrically connected to a plurality of circuit breakers by a plurality of power groups, and the plurality of circuit breakers are electrically connected to the teaching module and the test module. In this way, the system can automatically switch to an open circuit when the current supply is overloaded, and the system has the effect of avoiding line damage caused by overheating.

The aircraft navigation light simulation system created by this invention also includes a control module, which is coupled to the output module and the power module respectively. In this way, it has the effect of directly managing the working state of the light and the power supply.

The control module is coupled to the display unit of the output module by a main switch. In this way, all the lights of the display unit can be turned on at the same time through the total opening relationship, which has the effect of assisting teaching.

The control module is coupled to the prompt unit of the output module by a prompt switch. In this way, it has the function of testing the prompt function and selecting whether to enable the prompt function.

The control module is coupled to the power modules of the power module by a plurality of power switches. In this way, the system has the effect of switching between main power, DC or AC power.

In order to make the above and other purposes, features, and advantages of this creation more obvious and easy to understand, the following describes the preferred embodiment of this creation in conjunction with the accompanying drawings, as follows:

Please refer to FIG. 1, which is a preferred embodiment of the creative aircraft navigation light simulation system, which includes a teaching module 1, a test module 2, an output module 3, a power module 4 and a The control module 5, the teaching module 1 and the test module 2 are respectively coupled to the output module 3, and the power module 4 is electrically connected to the teaching module 1 and the test module 2, respectively, and the control module 5 are coupled to the output module 3 and the power module 4 respectively.

Please refer to Figures 1 and 2. The teaching module 1 can generate several light switching signals. The teaching module 1 can directly turn on or off various lighting devices through each of the light switching signals, which can use one-to-one switching. The lighting method is used to teach the functions and locations of different lights and simulate the lighting system of Airbus A Series Planes. In this embodiment, the teaching module 1 has 7 switching switches, corresponding to 7 different types of aircraft navigation lights, and each of the switching on relationships can generate independent ON / OFF light switching signals. However, the switching in this case The number of switches is not limited to this.

The test module 2 is an operation circuit composed of a plurality of switch units 21 and a plurality of relays 22, and each of the switch units 21 is manually switched whether an electrical signal passes through the switch unit 21, and each of the relays 22 is based on a Whether the electric signal acts on the relay 22 to switch the route of another electric signal. In this way, the switch units 21 and the relays 22 can directly or indirectly affect each other's path, so that the electric signals are switched according to the switching procedure. Several light test signals are transmitted and generated in the test module 2, and various light devices are turned on by each of the light test signals. The test module 2 can generate the light switch signals 21 individually or simultaneously by switching the switch units 21 in steps. Each of these light test signals simulates the working conditions of various functions of operating the Airbus civil aircraft (A Series) in accordance with the sequence.

Please refer to FIGS. 1, 2 and 3, the output module 3 has a display unit 31, which is coupled to the teaching module 1 and the test module 2, respectively. The display unit 31 can accept the number Light switching signals and the plurality of light test signals, switching the lights to light, dark, blinking or constant light status, as shown in FIG. 3, in this embodiment, the display unit 31 may be a virtual airplane Frontal image, and install several LED lights at the position corresponding to the navigation light system of Airbus civil aircraft (A Series), representing two navigation lights L1, two warning lights L2, one left floor lamp L3, one right floor lamp L4, one front The floor lamp L5, a taxi light L6, and the tri-strobe light L7. The aircraft image of the display unit 31 can also be separated from the output module 3, so that the aircraft pattern extends beyond the system panel, or the aircraft pattern is erected on the system. The panel, when operating the teaching module 1 or the test module 2, can easily observe the light projected by the LED lamps of the display unit 31, but this case is not limited to this case.

The output module 3 may further have a prompting unit 32, which is coupled to the test module 2. When the test module 2 can effectively transmit the correct light test signal, the prompting unit 32 sends a reminder signal. It can be used to check whether the test module 2 is working normally before the exam. The prompt unit 32 can be a buzzer or a light, which is not limited in this case. In addition, the output module 3 can also have a data unit 33. The data unit 33 can display the working voltage and current of the output module 3 in real time, and can observe whether the voltage and current acting on the output module 3 during the test module 2 switching the display unit 31. Stability and whether there is any risk of overload.

The power supply module 4 can be electrically connected to a plurality of circuit breakers 42 by a plurality of power supply groups 41, so that the plurality of circuit breakers 42 are electrically connected to the teaching module 1 and the test module 2, the plurality of power sources. The group 41 can provide the power required by the teaching module 1 and the test module 2 to generate the light switching signal and the light test signal, and the current is overloaded by the power interrupters 42 in the power groups 41 In this case, it will automatically switch to open circuit to avoid overheating and damage to the line. Each of the power supply groups 41 can also be divided into DC power supply and AC power supply, which can supply power requirements for lights with different functions. However, the virtual system in this case only needs students to understand the functional requirements of DC power supply and AC power supply. Therefore, the power supply module 41 Group 4 is powered by DC power only.

The control module 5 is connected to the output module 3 by coupling, and can directly control the power supply of the output module 3 and the working states of the display unit 31 and the prompt unit 32. For example, the control module 4 may have A master switch and a reminder switch. The master switch can simultaneously turn on all the lights of the display unit 31. The reminder switch can be used for the function test of the reminder unit 32, or choose whether to enable the reminder function. The control module 5 can also borrow The use of power is managed by coupling to the power module 4, for example, the control module 4 can have several power switches, and the DC or AC power can be switched by the power switches. The control module 4 can also be set A fuse or circuit breaker prevents overloading the line.

According to the foregoing structure, the teaching module 1 can switch several lights of the display unit 31 respectively, and conducts education and training by simulating the operation of the lighting system of the Airbus civil aircraft (A Series), so that the trainees can quickly recognize The positions of lights with different functions, without the need for actual training; In addition, the test module 2 provides the trainees with practical hands-on wiring and power-on tests, so that several lights of the display unit 31 can operate according to the functions of the actual flight, more Further, the test module 2 can be used to learn fault analysis, judgment, and troubleshooting, and to use simulation training instead of actual machine operation, which can avoid real aircraft damage during the learning process.

In addition, by using at least two switching switches of the teaching module 1, at least four switching units 21 of the test module 2, at least four relays 22, at least two power packs 41 of the power module 4, and at least two Each circuit breaker 42 is a test that can be used for aircraft maintenance technician B certification. It is used for trainees to conduct tests by wiring operation. With correct connection and operation steps, the output module 3 will produce the expected signal. And output response.

In addition, both the teaching module 1 and the control module 5 can directly switch on and off several lights of the display unit 31. Therefore, when the test module 2 is operated, if the display unit 31 does not operate as expected, The teaching module 1 or the control module 5 quickly judges whether the lamp is damaged or the trainee operates incorrectly. In addition, the relays 22 of the test module 2 can be electrically connected to the teaching module 1 and the display respectively. The unit 31 double-checks to check whether the functions of the relays 22 are normal, so as to avoid affecting the test results of the trainees.

In summary, the aircraft navigation light simulation system created by this invention uses the display unit to simulate the position and function of a real aircraft navigation light system. Switching the display unit with the teaching module has the teaching function; and the test The module controls the display unit to have the effect of simulating the actual machine operation and testing.

Although this creation has been disclosed using the above-mentioned preferred embodiments, it is not intended to limit this creation. Anyone skilled in this art can make various changes and modifications to the above-mentioned embodiments without departing from the spirit and scope of this creation. The technical scope protected by the creation, so the scope of protection of this creation shall be determined by the scope of the attached patent application.

1‧‧‧ teaching module
2‧‧‧ Quiz Module
21‧‧‧ switch unit
22‧‧‧ Relay
3‧‧‧Output Module
31‧‧‧display unit
32‧‧‧ Prompt Unit
33‧‧‧data unit
4‧‧‧ Power Module
41‧‧‧Power pack
42‧‧‧Disconnector
5‧‧‧control module
L1‧‧‧Navigation Light
L2‧‧‧Warning light
L3‧‧‧left floor lamp
L4‧‧‧right floor lamp
L5‧‧‧Front floor lamp
L6‧‧‧ Taxilight
L7‧‧‧ Strobe Light

[Figure 1] A system block diagram of a preferred embodiment of the present invention.
[Fig. 2] A diagram of the operation and display panel of this preferred embodiment.
[Figure 3] A partially enlarged view as shown in Figure 2.

Claims (8)

An aircraft navigation light simulation system includes:
A teaching module, the teaching module generates several light switching signals;
A test module has a plurality of switch units and a plurality of relays, and the plurality of switch units switch the plurality of relays to generate a plurality of light test signals;
An output module having a display unit coupled to the teaching module and the several relays, the display unit switching a plurality of lights according to the plurality of light switching signals and the plurality of light test signals; and a power module , Electrically connecting the teaching module and the test module to provide the power required to generate the light switching signal and the light test signal. According to the aircraft navigation light simulation system described in the first patent application scope, wherein the output module has a prompt unit, the prompt unit is coupled to the test module, and the prompt unit issues a reminder based on the plurality of light test signals. signal. The aircraft navigation light simulation system according to item 1 of the scope of the patent application, wherein the output module has a data unit, and the data unit measures and displays the working voltage and working current of the output module in real time. According to the aircraft navigation light simulation system described in item 1 of the scope of patent application, wherein the power module is electrically connected to a plurality of circuit breakers by a plurality of power groups, and the plurality of circuit breakers are electrically connected to the teaching module. And the quiz module. According to the aircraft navigation light simulation system described in any one of claims 1 to 4, the invention further includes a control module, which is coupled to the output module and the power module respectively. The aircraft navigation light simulation system according to item 5 of the scope of patent application, wherein the control module is coupled to the display unit of the output module by a main switch. According to the aircraft navigation light simulation system described in item 5 of the patent application scope, wherein the control module is coupled to the prompt unit of the output module by a prompt switch. According to the aircraft navigation light simulation system described in item 5 of the scope of patent application, wherein the control module is coupled to the power modules of the power module by a plurality of power switches, respectively.