KR20160117828A - Inspection Apparatus for Flight Data Recording Device - Google Patents
Inspection Apparatus for Flight Data Recording Device Download PDFInfo
- Publication number
- KR20160117828A KR20160117828A KR1020150045489A KR20150045489A KR20160117828A KR 20160117828 A KR20160117828 A KR 20160117828A KR 1020150045489 A KR1020150045489 A KR 1020150045489A KR 20150045489 A KR20150045489 A KR 20150045489A KR 20160117828 A KR20160117828 A KR 20160117828A
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- KR
- South Korea
- Prior art keywords
- voltage
- flight data
- data recording
- supply unit
- unit
- Prior art date
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
- G01R31/005—Testing of electric installations on transport means
- G01R31/008—Testing of electric installations on transport means on air- or spacecraft, railway rolling stock or sea-going vessels
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R13/00—Arrangements for displaying electric variables or waveforms
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R19/00—Arrangements for measuring currents or voltages or for indicating presence or sign thereof
- G01R19/165—Indicating that current or voltage is either above or below a predetermined value or within or outside a predetermined range of values
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Recording Measured Values (AREA)
Abstract
Description
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a checker for checking a flight data recorder for recording information about an airplane detected during flight of an airplane. More particularly, the present invention relates to a checker capable of providing a voltage equal to a voltage provided by an aircraft sensor to a flight data recorder for recording flight data of an aircraft, .
The contents described in this section merely provide background information on the embodiment of the present invention and do not constitute the prior art.
Accumulation of external force on the aircraft's aircraft due to repetitive aircraft operations can cause fatigue cracks in certain parts or specific parts.
In order to record the external force-related data provided to the aircraft during flight to identify a specific part where the fatigue crack occurred, the flight data recording device is provided inside the aircraft and the flight data recording device detects various kinds of external force Is installed.
The flight data recorder collects and stores the information sensed by the aircraft sensor, and the stored information is used to identify the fatigue area in connection with the external module. Using the information stored in the aircraft, it is possible to determine when the maintenance of the aircraft will be carried out, and to perform preventive maintenance and economic lifetime calculations.
Since the flight data recorder is electrically connected to various aircraft sensors and receives electrical signals, it contains complicated internal circuits and it is necessary to check the fault of the flight data recorder through precise check.
Meanwhile, there has been no conventional inspection equipment capable of performing a function check of a complicated flight data recording apparatus, so that it is difficult to detect whether the flight data recording apparatus operates normally, and there is a problem in that a new product must be acquired and used even in a simple trouble .
In order to solve such a problem, the present invention provides a flight data recorder with the same input voltage as an aircraft sensor, measures the voltage output from the flight data recorder with the provision of an input voltage, It is an object of the present invention to provide a flight data recorder checker capable of performing a self-test and a simulated flight of a flight data recorder.
The flight data recorder checker according to an embodiment of the present invention includes a device connection unit electrically connected to a flight data recorder to exchange electric signals with a flight data recorder, A power supply unit for converting the voltage of the power into a direct current voltage and supplying the direct voltage to the flight data recording apparatus through the apparatus connection unit, A voltage supply unit provided to receive a write signal voltage output from the flight data recording apparatus by an input voltage via a device connection unit and a supply switch unit provided in the voltage supply unit for supplying or blocking an input voltage to the flight data recording apparatus, And a display for displaying electrical signals flowing in and out of the device connection .; And a test terminal configured to output and measure an electric signal flowing in and out of the device connection portion.
Also, the voltage supplying unit may include an altitude speed voltage supply unit configured to supply the altitude voltage or the speed voltage generated by converting the DC voltage to the flight data recorder, and a normal speed voltage or horizontal acceleration voltage generated by converting the DC voltage, A PR voltage supply unit configured to supply a pitch speed voltage or a roll speed voltage generated by converting a direct current voltage to a flight data recording apparatus; And a deformation voltage supply unit configured to supply at least one deformation voltage generated by converting the DC voltage to the flight data recording apparatus.
The voltage receiving unit may include an altitude velocity voltage receiver configured to receive a first voltage output from the flight data recorder by an altitude voltage or a velocity voltage, A PR voltage accommodating portion provided to accommodate a third voltage output from the flight data recorder by a pitch speed voltage or a roll speed voltage; And a modified voltage accommodating portion provided to accommodate at least one fourth voltage output from the flight data recorder by the deformation voltage.
A supply dial adapted to select any one of the deformation voltages and supply the selected voltage to the flight data recording apparatus; And an acceptance dial adapted to select one of the fourth voltage and the fourth voltage to be accommodated in the flight data recording apparatus.
The flight data recorder checker according to an embodiment of the present invention may further include a takeoff and landing voltage supply unit configured to supply the takeoff and landing voltage generated by converting the direct current voltage to the flight data recorder.
In addition, the voltage supplied to the flight data recorder at the high-speed voltage supply unit, the ACC voltage supply unit, the PR voltage supply unit or the deformation voltage supply unit may have a positive voltage and a negative voltage.
Further, it may include a selection switch provided in the high-speed voltage supply unit, the ACC voltage supply unit, the PR voltage supply unit, or the deformation voltage supply unit to select either the positive voltage or the negative voltage.
In addition, the display unit includes a power display for displaying power supplied from the power supply unit to the flight data recording device via the device connection unit, a supply display for displaying an input voltage supplied from the voltage supply unit to the flight data recording device via the device connection unit, And a receiving display for displaying the recording signal voltage received from the flight data recording device through the device connection to the voltage receiving portion.
The apparatus connection unit may include a data connection terminal electrically connected to the data processing apparatus and the flight data recording apparatus to transmit the flight information stored in the flight data recording apparatus to the data processing apparatus.
According to an embodiment of the present invention, it is possible to perform the function check of the flight data recorder without performing a direct connection with the aircraft sensor, and perform the self-test of the flight data recorder.
In addition, it is possible to precisely check the flight data recording apparatus by finely adjusting the input voltage provided to the flight data recording apparatus.
Further, the information processing apparatus can be connected to the data processing apparatus to detect information stored in the flight data recording apparatus, thereby determining whether the flight data recording apparatus is operating normally.
In addition, a simulated flight environment can be created in the flight data recording device to perform data recording according to the simulated flight.
1 is a front view showing a flight data recorder checker according to an embodiment of the present invention.
2 is an enlarged front view showing in detail a portion of the checker of FIG.
Hereinafter, some embodiments of the present invention will be described in detail based on exemplary drawings. It should be noted that, in adding reference numerals to the constituent elements of the drawings, the same constituent elements are denoted by the same reference symbols as possible even if they are shown in different drawings. In the following description of the present invention, a detailed description of known functions and configurations incorporated herein will be omitted when it may make the subject matter of the present invention rather unclear.
FIG. 1 is a front view showing a flight data recorder checker according to an embodiment of the present invention, and FIG. 2 is an enlarged front view showing a part of the checker of FIG. 1 in detail.
The
The
The
The input voltage generated by the
The high voltage, the speed voltage, the normal speed voltage, the horizontal acceleration voltage, the pitch speed voltage, the roll speed voltage, or the deformation voltage may have positive and negative voltages among the input voltages generated by the
The high speed
The ACC
The PR
The deformation
The take-off and landing
The
The
The high-speed-
The ACC
The PR
The deformed
The
The
The
The display unit 600 is provided to display electric signals flowing in and out of the
The
The
The receiving
The
The
The
The
The foregoing description is merely illustrative of the technical idea of the present embodiment, and various modifications and changes may be made to those skilled in the art without departing from the essential characteristics of the embodiments. Therefore, the present embodiments are to be construed as illustrative rather than restrictive, and the scope of the technical idea of the present embodiment is not limited by these embodiments. The scope of protection of the present embodiment should be construed according to the following claims, and all technical ideas within the scope of equivalents thereof should be construed as being included in the scope of the present invention.
10: flight data recording device 20: data processing device
30: Precision Power Supply 50: Oscilloscope
100: Device connection part 200: Power supply part
300: voltage supply unit 301: high speed voltage supply unit
303: ACC voltage supply unit 305: PR voltage supply unit
307: deformation voltage supply unit 309: takeoff and landing voltage supply unit
310: supply dial 400: voltage receiving portion
401: altitude speed voltage receiving portion 403: ACC voltage receiving portion
405: PR voltage receiving portion 407: Deformation voltage receiving portion
410: reception dial 501: supply switch
503: Select switch 600:
601: Power Display 603: Supply Display
605: Acceptable display 701: Test terminal
703: Data connection terminal
Claims (9)
A power supply unit electrically connected to an external power supply to receive electric power, convert the voltage of the electric power into a direct current voltage, and supply the direct voltage to the air data recording apparatus through the device connection unit;
A voltage supply unit configured to supply the input voltage generated by converting the DC voltage to the flight data recording apparatus via the apparatus connection unit;
A voltage receiving unit arranged to receive the recording signal voltage output from the flight data recording apparatus by the input voltage through the apparatus connection unit;
A supply switch provided in the voltage supply unit to supply or block the input voltage to the flight data recording device;
A display unit for displaying the electric signal flowing in and out of the device connection unit; And
And a test terminal for outputting and measuring the electrical signal flowing in and out of the device connection portion.
An elevation speed voltage supply unit configured to supply the elevation voltage or the speed voltage generated by converting the direct current voltage to the flight data recording apparatus;
An ACC voltage supply unit configured to supply a normal acceleration voltage or a horizontal acceleration voltage generated by converting the DC voltage to the flight data recording device;
A PR voltage supply unit configured to supply a pitch speed voltage or a roll speed voltage generated by converting the DC voltage to the flight data recording apparatus; And
And a deformation voltage supplier for supplying at least one deformation voltage generated by converting the DC voltage to the flight data recording apparatus.
An elevated speed voltage receiving unit arranged to receive a first voltage outputted from the flight data recording apparatus by the elevation voltage or the speed voltage;
An ACC voltage accommodating portion provided to receive a second voltage output from the flight data recording device by the normal speed voltage or the horizontal acceleration voltage;
A PR voltage accepting unit configured to receive a third voltage output from the flight data recording apparatus by the pitch speed voltage or the roll speed voltage; And
And a deformed voltage accepting unit adapted to receive at least one or more fourth voltages output from the flight data recording apparatus by the deformation voltage.
A supply dial adapted to select any one of the deformation voltages and supply the selected voltage to the flight data recording apparatus; And
And an acceptance dial provided to select one of the fourth voltages and to receive the selected voltage in the flight data recording device.
And a takeoff and landing voltage supply unit configured to supply the take off and landing voltage generated by converting the direct current voltage to the flight data recording apparatus.
Wherein the voltage supplied to the flight data recording apparatus from the high speed voltage supply unit, the ACC voltage supply unit, the PR voltage supply unit, or the deformation voltage supply unit has a positive voltage and a negative voltage.
And a selection switch provided in the high-speed voltage supply unit, the ACC voltage supply unit, the PR voltage supply unit, or the deformation voltage supply unit to select either the positive voltage or the negative voltage. Checker.
A power display for displaying power supplied from the power supply unit to the flight data recording device via the device connection;
A supply display for displaying the input voltage supplied from the voltage supply unit to the flight data recording device via the device connection; And
And an acceptance display for displaying the recording signal voltage received from the flight data recording device through the device connection to the voltage receiving portion.
And a data connection terminal electrically connected to the data processing apparatus and the data recording apparatus to transmit the flight information stored in the data recording apparatus to the data processing apparatus.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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KR1020150045489A KR101692473B1 (en) | 2015-03-31 | 2015-03-31 | Inspection Apparatus for Flight Data Recording Device |
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KR1020150045489A KR101692473B1 (en) | 2015-03-31 | 2015-03-31 | Inspection Apparatus for Flight Data Recording Device |
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KR20160117828A true KR20160117828A (en) | 2016-10-11 |
KR101692473B1 KR101692473B1 (en) | 2017-01-04 |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111580531A (en) * | 2020-04-27 | 2020-08-25 | 瑞凯星弘(武汉)科技有限公司 | Unmanned aerial vehicle electricity testing method and device for power transmission line |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR102124877B1 (en) | 2018-10-04 | 2020-06-22 | 한국항공우주산업 주식회사 | Flight Loads Data Recorder Control Program |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR970007359A (en) * | 1995-07-26 | 1997-02-21 | 마이클 케인 | User interface for graphic display devices |
KR20050050382A (en) * | 2003-11-25 | 2005-05-31 | 한국항공우주산업 주식회사 | Aircraft automatic rudder trim control system test device |
KR20050050380A (en) * | 2003-11-25 | 2005-05-31 | 한국항공우주산업 주식회사 | Flight load data recorder bench test device |
KR20050052678A (en) * | 2003-12-01 | 2005-06-07 | 한국항공우주산업 주식회사 | Triple trim indicator testing device |
-
2015
- 2015-03-31 KR KR1020150045489A patent/KR101692473B1/en active IP Right Grant
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR970007359A (en) * | 1995-07-26 | 1997-02-21 | 마이클 케인 | User interface for graphic display devices |
KR20050050382A (en) * | 2003-11-25 | 2005-05-31 | 한국항공우주산업 주식회사 | Aircraft automatic rudder trim control system test device |
KR20050050380A (en) * | 2003-11-25 | 2005-05-31 | 한국항공우주산업 주식회사 | Flight load data recorder bench test device |
KR20050052678A (en) * | 2003-12-01 | 2005-06-07 | 한국항공우주산업 주식회사 | Triple trim indicator testing device |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111580531A (en) * | 2020-04-27 | 2020-08-25 | 瑞凯星弘(武汉)科技有限公司 | Unmanned aerial vehicle electricity testing method and device for power transmission line |
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KR101692473B1 (en) | 2017-01-04 |
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