JPH01123998U - - Google Patents
Info
- Publication number
- JPH01123998U JPH01123998U JP1894988U JP1894988U JPH01123998U JP H01123998 U JPH01123998 U JP H01123998U JP 1894988 U JP1894988 U JP 1894988U JP 1894988 U JP1894988 U JP 1894988U JP H01123998 U JPH01123998 U JP H01123998U
- Authority
- JP
- Japan
- Prior art keywords
- aircraft
- running
- inspection workbench
- aircraft inspection
- workbench
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000007689 inspection Methods 0.000 claims description 11
- 238000012423 maintenance Methods 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 1
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Description
図面は本考案の実施態様を例示し、第1図は駐
機位置における航空機および航空機点検作業台の
概略を示す平面図、第2図は走行装置の側面図、
第3図は制御装置のブロツク図である。
1……航空機、2……ガイドライン、3……航
空機点検作業台、4……機首、5……床面、6…
…走行装置、7……作業台、8……操舵車輪、9
……走行車輪、10……センサー、11……制御
装置、16……操舵モータ、17……走行モータ
、23……中央演算処理装置、24,25,27
,28……サーボアンプ、26,29……位置決
めコントローラ、30,31,32,33……エ
ンコーダ、E……偏心誤差、X―X……駐機基準
線。
The drawings illustrate embodiments of the present invention; FIG. 1 is a plan view schematically showing an aircraft and an aircraft inspection workbench in a parked position; FIG. 2 is a side view of the traveling device;
FIG. 3 is a block diagram of the control device. 1... Aircraft, 2... Guideline, 3... Aircraft inspection workbench, 4... Nose, 5... Floor, 6...
... Traveling device, 7 ... Workbench, 8 ... Steering wheel, 9
... Traveling wheel, 10 ... Sensor, 11 ... Control device, 16 ... Steering motor, 17 ... Traveling motor, 23 ... Central processing unit, 24, 25, 27
, 28... Servo amplifier, 26, 29... Positioning controller, 30, 31, 32, 33... Encoder, E... Eccentricity error, X-X... Parking reference line.
Claims (1)
び整備を行なう航空機点検作業台において、該航
空機点検作業台の前後いずれか一側に設けられ、
互いに独立して操舵モータにより走行角度を制御
される左右1対のゴムタイヤ製操舵車輪と、前記
航空機点検作業台の他側に設けられ、互いに独立
して走行モータにより走行速度を制御される左右
1対のゴムタイヤ製走行車輪と、前記航空機点検
作業台の左右いずれか一側の前後部に設けられ、
床面に駐機基準線に平行して敷設されたガイドラ
インを検出する複数個のセンサーと、前記航空機
点検作業台に設けられ、前記センサーの検出値お
よび前記航空機の前記駐機基準線に対する偏心誤
差を受けて、前記各操舵車輪の走行角度および前
記各走行車輪の走行速度の演算情報を発する中央
演算処理装置と、前記各演算情報を受けてパルス
信号に変換し、これら各パルス信号をサーボアン
プを介して対応する前記各モータに入力すること
により前記各車輪を1個づつ独立に制御する位置
決めコントローラと、前記各モータの回転数を積
算して前記各サーボアンプに負帰還するエンコー
ダとからなる制御装置とを具備してなり、前記航
空機点検作業台を前記機首に適合するように走行
させることを特徴とする航空機点検作業台の走行
装置。 In an aircraft inspection workbench adapted to the nose of an aircraft for inspection and maintenance of the aircraft, provided on either the front or rear side of the aircraft inspection workbench,
A pair of left and right steering wheels made of rubber tires whose running angles are controlled independently by steering motors; and a pair of left and right steering wheels, which are provided on the other side of the aircraft inspection platform and whose running speeds are controlled independently by running motors. a pair of running wheels made of rubber tires, and provided at the front and rear of either the left or right side of the aircraft inspection workbench,
a plurality of sensors for detecting guidelines laid on the floor parallel to the parking reference line; and a plurality of sensors provided on the aircraft inspection workbench; a central processing unit that receives the calculation information and outputs calculation information of the running angle of each of the steered wheels and the running speed of each of the steering wheels; a central processing unit that receives the calculation information and converts it into a pulse signal; a positioning controller that independently controls each wheel one by one by inputting input to the corresponding motor via the servo amplifier; and an encoder that integrates the number of rotations of each motor and provides negative feedback to each servo amplifier. 1. A traveling device for an aircraft inspection workbench, comprising: a control device; the traveling device for an aircraft inspection workbench is configured to make the aircraft inspection workbench move so as to fit the nose of the aircraft;
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1894988U JPH01123998U (en) | 1988-02-16 | 1988-02-16 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1894988U JPH01123998U (en) | 1988-02-16 | 1988-02-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH01123998U true JPH01123998U (en) | 1989-08-23 |
Family
ID=31234039
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1894988U Pending JPH01123998U (en) | 1988-02-16 | 1988-02-16 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH01123998U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH01123997U (en) * | 1988-02-16 | 1989-08-23 |
-
1988
- 1988-02-16 JP JP1894988U patent/JPH01123998U/ja active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH01123997U (en) * | 1988-02-16 | 1989-08-23 |
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