CN109548250A - A kind of landing light, taxiing light debugging calibration system and method - Google Patents
A kind of landing light, taxiing light debugging calibration system and method Download PDFInfo
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- CN109548250A CN109548250A CN201811363971.7A CN201811363971A CN109548250A CN 109548250 A CN109548250 A CN 109548250A CN 201811363971 A CN201811363971 A CN 201811363971A CN 109548250 A CN109548250 A CN 109548250A
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B47/00—Circuit arrangements for operating light sources in general, i.e. where the type of light source is not relevant
- H05B47/10—Controlling the light source
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Abstract
The invention discloses a kind of landing light, taxiing light debugging calibration system and methods, including interface mounting base, laser generator and master control set；Interface mounting base is mounted on landing light by adjustment means, on taxiing light lampshade, and laser generator includes first microprocessor and the driver connecting respectively with the first microprocessor, laser generator, Angle Measurement Module and first communication module；Laser generator is connect with driver, and master control set includes the second microprocessor and the second communication module and human-computer interaction module that connect with the second microprocessor, and Angle Measurement Module and laser generator are fixedly installed.The present invention makes calibration personnel that need not must select night, and without opening landing light, taxiing light can be carried out landing light, the light setting of taxiing light and calibration, while also avoid the drawbacks of operator is burnt by landing light, taxiing light light.
Description
Technical field
The present invention relates to the engineering debugging in aeronautical manufacture, aviation operation to ensure equipment technical field, and in particular to a kind of
Landing light, taxiing light debugging calibration system and method.
Background technique
The prior art needs manually to be calibrated and adjusted completely when carrying out landing light, taxiing light debugging and calibration
The setting angle of whole landing light, taxiing light, to be allowed to meet the requirement of design installation index.Debugging calibration method is selected at night
Between by aircraft haul out hangar outside, make aircraft keep it is land park posture, by front of plane nose 10 meters perpendicular to
The aircraft plane of symmetry places a screen (debugging can be using white wall as screen indoors), checks the center light of landing light or taxiing light
Beam should irradiate in scheduled region on the screen, if needing operator to ascend a height repeated multiple times adjust not in region
The elasticity of land lamp or taxiing light mounting screw makes the corresponding region of landing light, the taxiing light central light beam irradiation aircraft plane of symmetry
It is interior.This work is first is that requirement must carry out in dark conditions, therefore can only select to carry out in night-environment, and need
Manually adjustment, operator frequently ascend a height operation repeatedly, and falling risk is relatively high, require all to compare to meteorological condition such as wind speed
Height, calibration difficulty are big.
Summary of the invention
Based on the deficiencies of the prior art, the purpose of the present invention is providing a kind of landing light, taxiing light debugging calibration system
While system, the calibration method of a kind of landing light, taxiing light debugging calibration system is additionally provided, is realized by the System and method for
At any time, the calibration of the landing light, taxiing light of any meteorological condition, and reduce calibration difficulty.
The technical solution of the present invention is as follows:
A kind of landing light, taxiing light debug calibration system, it is characterised in that: including interface mounting base, laser generator and
Master control set；
The interface mounting base is mounted on landing light by adjustment means, on taxiing light lampshade, and the adjustment means are used for
Landing light, taxiing light are adjusted relative to land lamp/taxiing light lampshade position；
The laser generator includes first microprocessor and the driver connecting respectively with the first microprocessor, swashs
Optical generator, Angle Measurement Module and first communication module；
The driver is arranged in interface mounting base, and the laser generator is connect with the driver, and can be by institute
State driver driving rotation, the central light beam and landing of the laser generator at least one laser beam during rotation
The central light beam coincidence of lamp, taxiing light；
The master control set includes the second microprocessor and the second communication module connecting with the second microprocessor and man-machine
Interactive module, the first communication module and the second communication module communicate to connect, and the second communication module is used for the
Under the control of two microprocessors, information is sent to the driver, the driver driving laser generator is made to do Laser emission
The adjustment in direction guarantees on the lasing central and beam reception screen of laser generator adjusted by the label of calibration
Position is overlapped；
The Angle Measurement Module and the laser generator are fixedly installed, and the Angle Measurement Module is for measuring laser
The angle rotated during generator adjustment, and the angle information of measurement is transferred at the first micro process or the second microprocessor
Reason, show that landing light, taxiing light answer adjusting parameter information.
Further, the driver uses servo drive motor.
Further, the adjustment means use mounting screw, and screw hole, the interface installation are provided in interface mounting base
Seat is flexibly connected by mounting screw with landing light, taxiing light lampshade.
Further, the driver is fixedly mounted in the interface mounting base, fixed on the outside of the interface mounting base
3 installation ribs are evenly equipped with, the laser generator includes installing component and can the relatively described installation under driver driving
The laser generator ontology of component rotation, the installing component are mounted on the installation rib by screw.
Further, the structure of the interface mounting base, shape are consistent with landing light/taxiing light lampshade, laser generator
Center is mounted in interface mounting base perpendicular to the position of arc lampshade normal.
Further, the first communication module uses WIFI module, and corresponding, the second communication module also uses
WIFI module.
Further, the human-computer interaction module includes the display screen connecting with second microprocessor.
Further, the human-computer interaction module further includes being connect with second microprocessor for emitting laser hair
The remote control transmitter of raw device switching signal and turn signal, corresponding, the first microprocessor is connected with for receiving laser
The receiver of remote-control sytem of generator switching signal and turn signal, second microprocessor, which is also connected with, issues remote control transmitter
The control lever of order is provided with key module in the control lever.
A kind of calibration method of landing light, taxiing light debugging calibration system, which is characterized in that the method includes the steps:
Interface mounting base connect by adjusting screw with landing light, taxiing light lampshade, connect indirectly with fuselage by S1, and
It will be fixedly mounted in interface mounting base with the driver of laser generator and Angle Measurement Module, calibrate laser generator
The direction of initial transmissions light beam, the transmitting of the central light beam and landing light, taxiing light that emit laser generator in initial position
The center of light beam is overlapped；
S2 leads to if the light beam of laser generator transmitting cannot be irradiated to the position of landing light, the setting of taxiing light aiming screen
Device of overdriving drives laser generator rotation, when the light beam of laser generator transmitting is irradiated to the setting position of aiming screen,
Order is issued to the driver by the second microprocessor, enables the laser generator stop operating, stop emitting laser light
Beam, meanwhile, the laser generator measured is transferred to first micro- place relative to the angle of the rotation of initial position by angular transducer
Device or the second microprocessor are managed, is handled by the first microprocessor or the second microprocessor analysis, show that each adjusting screw is answered
The distance of adjustment；
S3, the adjusting screw that staff obtains according to S2 should adjust apart from adjusting screw.
Further, the method for calibrating the direction of the initial transmissions light beam of laser generator includes:
One piece of screen is arranged in S11 before landing light, taxiing light；
S12 opens landing light, taxiing light, on the screen the center of marker beam, closes landing light, taxiing light；
S13 opens laser generator, checks the light beam of laser beam point of irradiation on the screen and landing light, taxiing light
Whether the center of point of irradiation is overlapped, if not being overlapped, laser generator rotation is controlled by master control set, until being overlapped；
S14, laser generator position data are reset.
The invention has the benefit that system and method be mainly used for simulate landing light, taxiing light luminous beam according to
The direction movement of operator's control exports rotation information to driver by master control set, and controller controls laser generator
Rotation, after rotation reaches target point, rotational angle data are sent to first microprocessor or second micro- by angular-rate sensor
Then processor calculates landing light, the length of angle and adjusting screw that taxiing light needs to adjust, make calibration personnel need not must
Night must be selected, without opening landing light, taxiing light can be carried out landing light, the light setting of taxiing light and calibration, simultaneously
Also avoid the drawbacks of operator is burnt by landing light, taxiing light light.
Detailed description of the invention
Fig. 1 is the interface mounting base of the specific embodiment of the invention and the structural schematic diagram of laser generator.
Specific embodiment
As shown in Figure 1, a kind of landing light, taxiing light debug calibration system, including interface mounting base 1, laser generator and
Master control set, the interface mounting base 1 are mounted on landing light by adjustment means 2, on taxiing light lampshade, are connected indirectly to fuselage
On, the adjustment means 2 are for adjusting position of the interface mounting base relative to fuselage, and the adjustment means 2 of the present embodiment are using peace
Cartridge screw is equipped with spring washer, has locking wire insurance hole on head of screw, finishes for adjusting between the mounting screw and airframe structure
Afterwards, screw is fixed after playing insurance with fuse.Screw hole is provided in interface mounting base 1, the interface mounting base 1 passes through installation
Screw is flexibly connected with landing light, taxiing light lampshade, spring shim and fuselage.Adjustment means 2 can also be adjustable using bolt etc.
Section height or length, and can add the gasket of given thickness after adjusting and adjust landing light, taxiing light established angle to realize
The purpose of degree.The embodiment of the present invention interface mounting base use hollow, flat cylindrical annular seating, flat shape, structure with
Landing light, taxiing light lampshade are consistent.
The laser generator include first microprocessor and the driver being connect respectively with the first microprocessor 3,
Laser generator 4, Angle Measurement Module and first communication module, the driver 3 is fixedly mounted on the annular seating, described
The outside fixation of annular seating is evenly equipped with 3 installation ribs 11, and the laser generator includes installing component and can be in the driver
The laser generator ontology that the relatively described installing component is freely rotated under driving, the installation site of laser generator ontology should ensure that
Free movement in this left and right of laser generator, upper and lower 15 ° of angular ranges, no interference, structure, shape and the landing of interface mounting base
Lamp/taxiing light lampshade is consistent, and center is equipped with laser generator, the installing component perpendicular to the position of arc lampshade normal
It is fixedly mounted on the installation rib by screw, installing component can be an installation tripod, and three feet of tripod are distinguished
It is fixed with 3 installation ribs, the middle part of tripod is connect by a universal joint with laser generator ontology, and driver uses servo
The driving precision of motor, servo motor is high, is well suited for accurate rotation and adjusts, and first microprocessor is using common processing chip
It can be achieved with, such as C51 family chip and its necessary peripheral circuit.
The Angle Measurement Module is fixed with the laser generator ontology, and with the rotation of the laser generator ontology
And rotate, angle measurement unit uses angular transducer, the master control set include the second microprocessor and with it is described second micro-
The second communication module and human-computer interaction module of processor connection.
Similarly, the second microprocessor can be achieved with using common processing chip, such as outside C51 family chip and its necessity
Enclose circuit.The first communication module and the second communication module communicate to connect.The first communication module uses WIFI mould
Block, corresponding, the second communication module also uses WIFI module.
The human-computer interaction module includes the display screen connecting with second microprocessor.
The human-computer interaction module further includes being connect with second microprocessor for emitting laser generator switch
The remote control transmitter of signal, laser zero adjustment signal and turn signal, corresponding, the first microprocessor connection is useful
In the receiver of remote-control sytem for receiving laser generator switching signal, laser zero adjustment signal and turn signal, described second is micro-
Processor is also connected with laser switch and zero adjustment key module, the control lever that order is issued to remote control transmitter, described
Key module is provided in control lever.The setting of remote control transmitter and receiver of remote-control sytem and remote-control lever is distant using maturation in the market
Control control technology.
When calibrating landing light, taxiing light by this system, the light beam and landing light, cunning of the transmitting of default conditions laser generator
Portable lighter light beam is overlapped, if because non-overlapping problem occur in the reasons such as landing light, taxiing light manufacturing process difference or defect, it can be by such as
Lower method is calibrated (zeroing): S11, and installation landing light, taxiing light debug calibration system；S12, before landing light, taxiing light
One piece 1 square metre of curtain is arranged in face 1-2 meters of place；S13, unlatching landing light, taxiing light, the center of marker beam,
Close landing light, taxiing light；S14 opens laser generator, checks point of irradiation and landing light, cunning of the laser beam on curtain
Whether the light beam irradiation dot center of portable lighter is overlapped, if not being overlapped, controls laser by the laser generator control-rod of master control set
Generator movement, until being overlapped；S15 presses aligning key on master controller, and beam deviation data can be recorded at this time, swashs
Optical generator position data is reset, and the angle information of the angular transducer of the position is set as initial information, then passes through control lever
To the second microprocessor, the second microprocessor issues instructions to remote-transmitter for the order of input manipulation laser generator ontology rotation
Device, remote control transmitter issue signal, and after receiver of remote-control sytem receives control signal, control signal is inputed to first micro- place
Device is managed, control driver driving laser generator ontology rotates after first microprocessor carries out processor to signal, meanwhile, pass through
The angle information of angular transducer record rotation, when laser pickoff receives the signal of laser generator ontology sending just
Afterwards, it notifies that the second microprocessor, the second microprocessor are locked, and locking signal is issued first by second communication module
Communication module, first communication module, which receives, determines that the position of the angular transducer is set for last bit after the information, meanwhile, by the
One microprocessor is set by initial, the last bit of angle or rotation information calculates whether each mounting screw should adjust or should adjust
Length or first microprocessor the change information of the angle monitor of angular transducer and initial position message and last bit are set it is logical
It crosses first communication module transmission and second communication module is transferred to the second microprocessor, which is calculated by the second microprocessor
Whether screw should adjust, or the length that should be adjusted.
A kind of calibration method of landing light, taxiing light debugging calibration system, which is characterized in that the method includes the steps:
Interface mounting base connect by adjusting screw with landing light, taxiing light lampshade, connect indirectly with fuselage by S1, and
It will be fixedly mounted in interface mounting base with the driver of laser generator and Angle Measurement Module, meanwhile, adjustment laser hair
Raw device is to initial 0, and because the structure, shape, radian of interface mounting base are consistent with landing light, taxiing light lampshade, center is vertical
Laser generator is installed in the position of lampshade normal, at this time the light beam of the axis direction of laser emitting and landing light, taxiing light
Center line be overlapped, the as initial position of laser generator.If because of originals such as landing light, taxiing light manufacturing process difference or defects
Because there is non-overlapping problem, can be calibrated by the following method (zeroing): S11 installs landing light, taxiing light debugging calibration system
System；One piece 1 square metre of curtain is arranged in 1-2 meters of the place before landing light, taxiing light S12；S13 opens landing light, slides
Landing light, taxiing light are closed in lamp, the center of marker beam；S14 opens laser generator, checks laser beam in curtain
On the light beam irradiation dot center of point of irradiation and landing light, taxiing light whether be overlapped, if not being overlapped, pass through the laser of master control set
Generator control-rod controls laser generator movement, until being overlapped；S15 presses the aligning key on master control set, and light beam is inclined at this time
Difference data can be recorded, and laser generator position data is reset；
S2 leads to if the light beam of laser generator transmitting cannot be irradiated to the position of landing light, the setting of taxiing light aiming screen
Device of overdriving drives laser generator rotation, when the light beam of laser generator transmitting is irradiated to the setting position of screen, passes through
Second microprocessor issues order to the driver, and the laser generator is enabled to stop operating, and stops transmitting laser beam, together
When, angular transducer by the laser generator measured relative to the angle of the rotation of initial position be transferred to first microprocessor or
Second microprocessor is handled by the first microprocessor or the second microprocessor analysis, obtains what each adjusting screw should adjust
Distance；
S3, the adjusting screw that staff obtains according to S2 should adjust apart from adjusting screw, the adjustment length of screw is pressed
It can be converted into tune number of full circle according to specification, the screw pitch of screw, most ringlet number can be as accurate as 1/4 circle.
In the systems and methods, the position of laser generator setting should tail landing light according to aircraft, left and right landing
Suitable adjustment is done in the position of lamp and left and right taxiing light, and the present embodiment laser pickoff can be replaced according to the adjustment demand of different lamps pacifies
The debugging calibration process of each lamp and the embodiment of laser generator installation site is set forth below in holding position:
1, tail landing light adjustment method and step
Tail landing light is mounted on vertical fin leading edge.Debugging step is as follows:
A) so that aircraft is kept land and park posture.
B) perpendicular to the aircraft plane of symmetry in front of plane nose 10 meters, 5.69 meters away from ground (if aircraft lifts tune
Examination, aircraft is liftoff L, then beam center should be away from ground L+5.69 meter) one target cross of setting, which is two wide
The rectangle yellow of 5cm, long 50cm or red adhesive sticker at right angles intersect, and crosspoint is central point.
C) landing light, taxiing light debugging calibration system are installed, i.e., by interface mounting base by adjusting screw and landing light, cunning
The connection of portable lighter lampshade, connect with fuselage indirectly, and will be fixedly mounted with the driver of laser generator and Angle Measurement Module
In interface mounting base.
D) carry out light beam alignment (zeroing): 1) 1-2 meters of place is arranged one piece 1 square metre before landing light, taxiing light
Curtain；2) landing light, taxiing light are opened, landing light, taxiing light are closed in the center of marker beam；3) laser hair is opened
Raw device, checks whether point of irradiation of the laser beam on curtain is overlapped with the light beam of landing light, taxiing light irradiation dot center, if not
It is overlapped, laser generator movement is controlled by the laser generator control-rod on master controller, until being overlapped；4) main control is pressed
Aligning key on device, beam deviation data can be recorded at this time, and laser generator position data is reset.
E) laser generator switch on master controller is placed in on-position, whether is the light beam of inspection laser generator transmitting
It is irradiated in the region that cross hairs central point radius is 30cm, if not having, the control lever manipulated on master controller sends out laser
Raw device rotation presses behaviour when the light beam of laser generator transmitting is irradiated in the region that cross hairs central point radius is 30cm
Resolving button on vertical pole, the specific adjustment that master controller calculates each screw of three adjusting screws of the landing light immediately are high
Information is spent, and is shown by the display screen on master controller.
F) landing light, taxiing light debugging calibration system are removed, that is, removes interface mounting base, laser generator and angle measurement
The driver of module adjusts three adjusting screws, debugging knot by the calibration data that landing light, taxiing light debugging calibration system are shown
Beam.
2, left and right landing light adjustment method and step
Left and right landing light is mounted on the outer nose of wing of left and right machine, and two lamps are symmetrically installed about the aircraft axis of symmetry.Debugging step
It is as follows:
A) so that aircraft is kept land and park posture.
B) apart from 12.6 meters of aircraft plane of symmetry or so in front of plane nose 10 meters；1.38 meters away from ground (if fly
Machine lifts debugging, aircraft is liftoff L, then beam center should be away from ground L+1.38 meters) target cross, the cross is respectively set
Will is two wide 5cm, and the rectangle yellow of long 50cm or red adhesive sticker at right angles intersect, and crosspoint is central point.
C) landing light, taxiing light debugging calibration system are installed, i.e., by interface mounting base by adjusting screw and landing light, cunning
The connection of portable lighter lampshade, connect with fuselage indirectly, and will be fixedly mounted with the driver of laser generator and Angle Measurement Module
In interface mounting base.
D) carry out light beam alignment (zeroing): 1) 1-2 meters of place is arranged one piece 1 square metre before landing light, taxiing light
Curtain；2) landing light, taxiing light are opened, landing light, taxiing light are closed in the center of marker beam；3) laser hair is opened
Raw device, checks whether point of irradiation of the laser beam on curtain is overlapped with the light beam of landing light, taxiing light irradiation dot center, if not
It is overlapped, laser generator movement is controlled by the laser generator control-rod on master controller, until being overlapped；4) main control is pressed
Aligning key on device, beam deviation data can be recorded at this time, and laser generator position data is reset.
E) laser generator switch on master controller is placed in on-position, whether is the light beam of inspection laser generator transmitting
It is irradiated in the region that cross hairs central point radius is 30cm, if not having, the control lever manipulated on master controller sends out laser
Raw device rotation presses behaviour when the light beam of laser generator transmitting is irradiated in the region that cross hairs central point radius is 30cm
Resolving button on vertical pole, the specific adjustment that master controller calculates each screw of three adjusting screws of the landing light immediately are high
Information is spent, and is shown by the display screen on master controller.
F) landing light, taxiing light debugging calibration system are removed, that is, removes interface mounting base, laser generator and angle measurement
The driver of module adjusts three adjusting screws, debugging knot by the calibration data that landing light, taxiing light debugging calibration system are shown
Beam.
3, left and right taxiing light range of exposures testing procedure
Left and right taxiing light is mounted on the outer nose of wing of left and right machine, and two lamps are symmetrically installed about the aircraft axis of symmetry.Testing procedure
It is as follows:
A) so that aircraft is kept land and park posture.
B) since the size of test site limits, apart from the aircraft plane of symmetry 12.6 in front of plane nose 10 meters
Rice；4.25 meters away from ground, and in the position by laser pickoff setting.If (aircraft lifts debugging, aircraft is liftoff L, then in light beam
The heart should be away from ground L+4.25 meters) target cross is respectively set, which is two wide 5cm, the rectangle of long 50cm
Yellow or red adhesive sticker at right angles intersect, and crosspoint is central point.
C) landing light, taxiing light debugging calibration system are installed, i.e., by interface mounting base by adjusting screw and landing light, cunning
The connection of portable lighter lampshade, connect with fuselage indirectly, and will be fixedly mounted with the driver of laser generator and Angle Measurement Module
In interface mounting base.
D) carry out light beam alignment (zeroing): 1) 1-2 meters of place is arranged one piece 1 square metre before landing light, taxiing light
Curtain；2) landing light, taxiing light are opened, landing light, taxiing light are closed in the center of marker beam；3) laser hair is opened
Raw device, checks whether point of irradiation of the laser beam on curtain is overlapped with the light beam of landing light, taxiing light irradiation dot center, if not
It is overlapped, laser generator movement is controlled by the laser generator control-rod on master controller, until being overlapped；4) main control is pressed
Aligning key on device, beam deviation data can be recorded at this time, and laser generator position data is reset.
E) laser generator switch on master controller is placed in on-position, whether is the light beam of inspection laser generator transmitting
It is irradiated in the region that cross hairs central point radius is 30cm, if not having, the control lever manipulated on master controller sends out laser
Raw device rotation presses behaviour when the light beam of laser generator transmitting is irradiated in the region that cross hairs central point radius is 30cm
Resolving button on vertical pole, the specific adjustment that master controller calculates each screw of three adjusting screws of the landing light immediately are high
Information is spent, and is shown by the display screen on master controller.
F) landing light, taxiing light debugging calibration system are removed, that is, removes interface mounting base, laser generator and angle measurement
The driver of module adjusts three adjusting screws, debugging knot by the calibration data that landing light, taxiing light debugging calibration system are shown
Beam.
It should be noted that described above is presently preferred embodiments of the present invention, the invention is not limited to above-mentioned
Embodiment all should belong to protection scope of the present invention as long as it reaches technical effect of the invention with identical means.
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Claims (10)
1. a kind of landing light, taxiing light debug calibration system, it is characterised in that: including interface mounting base, laser generator and master
Control device；
The interface mounting base is mounted on landing light by adjustment means, on taxiing light lampshade, and the adjustment means are for adjusting
The position of landing light, taxiing light relative to landing light, taxiing light lampshade；
The laser generator includes first microprocessor and the driver connecting respectively with the first microprocessor, laser hair
Raw device, Angle Measurement Module and first communication module；
The driver is arranged in interface mounting base, and the laser generator is connect with the driver, and can be by the drive
Dynamic device driving rotation, the laser generator during rotation the central light beam of at least one laser beam and landing light,
The central light beam of taxiing light is overlapped；
The master control set includes the second microprocessor and the second communication module connecting with the second microprocessor and human-computer interaction
Module, the first communication module and the second communication module communicate to connect, and the second communication module is used for micro- second
Under the control of processor, information is sent to the driver, the driver driving laser generator is made to do Laser emission direction
Adjustment, guarantee laser generator adjusted lasing central and beam reception screen on by calibration mark position
It is overlapped；
The Angle Measurement Module and the laser generator are fixedly installed, and the Angle Measurement Module is for measuring laser
The angle rotated during device adjustment, and the angle information of measurement is transferred to the first micro process or the second microprocessor processes,
Show that landing light, taxiing light answer adjusting parameter information.
2. landing light as described in claim 1, taxiing light debug calibration system, it is characterised in that: the driver is used and watched
Take driving motor.
3. landing light as described in claim 1, taxiing light debug calibration system, it is characterised in that: the adjustment means use
Mounting screw, screw hole is provided in interface mounting base, and the interface mounting base passes through mounting screw and landing light, taxiing light lampshade
It is flexibly connected.
4. landing light as claimed in claim 3, taxiing light debug calibration system, it is characterised in that: the fixed peace of the driver
In the interface mounting base, fixation is evenly equipped with 3 installation ribs on the outside of the interface mounting base, and the laser generator includes
Installing component and the laser generator ontology that can be rotated under driver driving relative to the installing component, the mounting portion
Part is mounted on the installation rib by screw.
5. landing light as claimed in claim 4, taxiing light debug calibration system, it is characterised in that: the interface mounting base
Structure, shape are consistent with landing light/taxiing light lampshade, and laser generator is mounted in interface mounting base center perpendicular to arc
The position of lampshade normal.
6. landing light as described in claim 1, taxiing light debug calibration system, it is characterised in that: the first communication module
Corresponding using WIFI module, the second communication module also uses WIFI module.
7. landing light as described in claim 1, taxiing light debug calibration system, it is characterised in that: the human-computer interaction module
Including the display screen being connect with second microprocessor.
8. landing light as described in claim 1, taxiing light debug calibration system, it is characterised in that: the human-computer interaction module
It further include being connect with second microprocessor for emitting the remote-transmitter of laser generator switching signal and turn signal
Device, corresponding, the remote control that the first microprocessor is connected with for receiving laser generator switching signal and turn signal connects
Device is received, second microprocessor is also connected with the control lever for issuing order to remote control transmitter, is provided in the control lever
Key module.
9. such as the described in any item landing lights of claim 1-8, the calibration method of taxiing light debugging calibration system, feature exists
In, the method includes the steps:
Interface mounting base connect by adjusting screw with landing light, taxiing light lampshade, connect indirectly with fuselage, and will be attached by S1
There are laser generator and the driver of Angle Measurement Module to be fixedly mounted in interface mounting base, calibrates the initial of laser generator
The direction for emitting light beam, the transmitting light beam of the central light beam and landing light, taxiing light that emit laser generator in initial position
Center be overlapped；
S2 passes through drive if the light beam of laser generator transmitting cannot be irradiated to the position of landing light, the setting of taxiing light aiming screen
Dynamic device driving laser generator rotation passes through when the light beam of laser generator transmitting is irradiated to the setting position of aiming screen
Second microprocessor issues order to the driver, enables the laser generator stop operating, stops emitting laser beam, together
When, angular transducer by the laser generator measured relative to the angle of the rotation of initial position be transferred to first microprocessor or
Second microprocessor is handled by the first microprocessor or the second microprocessor analysis, obtains what each adjusting screw should adjust
Distance；
S3, the adjusting screw that staff obtains according to S2 should adjust apart from adjusting screw.
10. the calibration method of landing light as claimed in claim 9, taxiing light debugging calibration system, which is characterized in that calibration swashs
The method in the direction of the initial transmissions light beam of optical generator includes:
One piece of screen is arranged in S11 before landing light, taxiing light；
S12 opens landing light, taxiing light, on the screen the center of marker beam, closes landing light, taxiing light；
S13 opens laser generator, checks the light beam irradiation of the point of irradiation and landing light, taxiing light of laser beam on the screen
Whether the center of point is overlapped, if not being overlapped, laser generator rotation is controlled by master control set, until being overlapped；
S14, laser generator position data are reset.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811363971.7A CN109548250B (en) | 2018-11-16 | 2018-11-16 | Landing lamp and taxi lamp debugging and calibrating system and method |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201811363971.7A CN109548250B (en) | 2018-11-16 | 2018-11-16 | Landing lamp and taxi lamp debugging and calibrating system and method |
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| CN109548250B CN109548250B (en) | 2020-05-15 |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
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| CN110212442A (en) * | 2019-06-27 | 2019-09-06 | 国网湖南省电力有限公司 | Switchgear and its circuit breaker trolley position detecting device and application method |
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| CN110769579A (en) * | 2019-10-15 | 2020-02-07 | 广东熠日照明科技有限公司 | Method for controlling multiple lamps individually |
| CN112357110A (en) * | 2020-09-22 | 2021-02-12 | 成都飞机工业（集团）有限责任公司 | Aircraft taxiing lamp installation angle calibration system and method based on laser positioning principle |
| CN112888119A (en) * | 2021-01-07 | 2021-06-01 | 杭州重芯力科技有限公司 | Intelligent light interaction method and device based on data processing and electronic equipment |
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