CN105346730A - Automatic detecting and marking system of wing pit during airplane maintaining - Google Patents
Automatic detecting and marking system of wing pit during airplane maintaining Download PDFInfo
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- CN105346730A CN105346730A CN201510756405.2A CN201510756405A CN105346730A CN 105346730 A CN105346730 A CN 105346730A CN 201510756405 A CN201510756405 A CN 201510756405A CN 105346730 A CN105346730 A CN 105346730A
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Abstract
An automatic detecting and marking system of a wing pit during airplane maintaining comprises scanners, a walking frame drive device, a scanner walking frame, a working platform support, a control panel, a console, a control device, a plurality of working platform moving wheels, a wing carrying working platform, two sets of gear and rack transmission mechanisms and a marking mechanical arm. According to the automatic detecting and marking system of the wing pit during airplane maintaining, comprehensive scanning of a wing can be achieved, and data about the damage depth and area of the wing pit are obtained. The control device can process the data obtained through the scanners, all positions needing to be maintained in the scanning area are judged through calculation, marking of a computer is carried out, finally, the wing is marked with the result through the marking mechanical arm, and an important basis is provided for a maintenance engineer accordingly.
Description
Technical field
The invention belongs to aircraft maintenance technical field, particularly in a kind of aircraft maintenance wing pit automatic detection and mark system.
Background technology
In current aircraft maintenance work at home, be subject to the external force such as hail and the situation that causes occurring pit when running into wing, when keeping in repair, engineering engineer checks by visual, and then mark with hand, measure and record, and judge that this pit is the need of maintenance.Such working process not only needs to expend more manpower, and survey precision is affected by human factors comparatively large, even likely can affect the quality of aircraft maintenance.Just need the automatic detection of wing pit in a kind of aircraft maintenance in this case and the system of mark.
Summary of the invention
In order to solve the problem, the object of the present invention is to provide the automatic detection of wing pit in a kind of aircraft maintenance and the system of mark.
In order to achieve the above object, in aircraft maintenance provided by the invention wing pit automatic detection and mark system comprise at least one scanner, walker actuating device, scanner walker, workplatform bearing, control panel, control desk, control setup, multiple workplatform movable pulley, wing place workplatform, two groups of rack and pinion drive mechanisms and marker mechanical arm; Wherein, described wing places the middle part that workplatform is horizontally set on workplatform bearing; A workplatform movable pulley is installed in each bight, lower end of workplatform bearing respectively; Rack and pinion drive mechanism is made up of gear and tooth bar, and two groups of rack and pinion drive mechanisms are symmetrical arranged, and its middle rack level is arranged on a side roof part of workplatform bearing; A gear that can be meshed with corresponding tooth bar is pivotally installed respectively in the two ends of scanner walker; The outputting power mechanism of walker actuating device is connected with a gear, is moved by gear for driving scanner walker along tooth bar; Scanner is arranged on the bottom surface, middle part of scanner walker; The upper end of marker mechanical arm is fixed on the middle part of scanner walker, and lower end is provided with labelling apparatus; Control desk is arranged on the outside of workplatform bearing, and control panel and control setup are arranged on control desk, and control setup is electrically connected with the controller of scanner, walker actuating device, control panel and marker mechanical arm.
When described scanner is multiple, multiple scanner standoff distance is arranged on the bottom surface, middle part of scanner walker, to increase scanning area.
Described workplatform movable pulley is cardan wheel, and carries locking device, can realize moving freely of workplatform bearing level attitude thus, and realizes the fixing of any position.
Described marker mechanical arm is folding structure.
The automatic detection of wing pit in aircraft maintenance provided by the invention the system of mark can realize scanning wing comprehensively, and obtain the data of the wing Notch damage degree of depth and area; Described control setup can process scanner the data obtained, by calculating the whole positions judging to need repairing in scanning area, and carry out computer mark, finally utilize marker mechanical arm by result queue on wing, thus provide important foundation for engineering engineer.
Accompanying drawing explanation
Fig. 1 is the automatic detection of wing pit in aircraft maintenance provided by the invention and the system using state block diagram of mark;
Fig. 2 is the birds-eye view of the automatic detection of wing pit in aircraft maintenance provided by the invention the system of mark;
Fig. 3 is the automatic detection of wing pit in aircraft maintenance provided by the invention and the system front view of mark;
Wherein: 1, scanner, 2, walker actuating device, 3, scanner walker, 4, workplatform bearing, 5, control panel, 6, control desk, 7, control housing, 8, workplatform movable pulley, 9, wing places workplatform, 10, wing, 11, rack and pinion drive mechanism 12, marker mechanical arm.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments to the automatic detection of wing pit in aircraft maintenance provided by the invention and mark system be described in detail.Obviously, described embodiment is only the present invention's part embodiment, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not making other embodiments all obtained under creative work prerequisite, belong to the scope of protection of the invention.
As shown in Figure 1-Figure 3, in aircraft maintenance provided by the invention, the automatic detection of wing pit the system of mark comprise at least one scanner 1, walker actuating device 2, scanner walker 3, workplatform bearing 4, control panel 5, control desk 6, control setup 7, multiple workplatform movable pulley 8, wing place workplatform 9, two groups of rack and pinion drive mechanisms 11 and marker mechanical arm 12; Wherein, described wing places the middle part that workplatform 9 is horizontally set on workplatform bearing 4; A workplatform movable pulley 8 is installed in each bight, lower end of workplatform bearing 4 respectively; Rack and pinion drive mechanism 11 is made up of gear and tooth bar, and two groups of rack and pinion drive mechanisms 11 are symmetrical arranged, and its middle rack level is arranged on a side roof part of workplatform bearing 4; A gear that can be meshed with corresponding tooth bar is pivotally installed respectively in the two ends of scanner walker 3; The outputting power mechanism of walker actuating device 2 is connected with a gear, is moved by gear for driving scanner walker 3 along tooth bar; Scanner 1 is arranged on the bottom surface, middle part of scanner walker 3; The upper end of marker mechanical arm 12 is fixed on the middle part of scanner walker 3, and lower end is provided with labelling apparatus; Control desk 6 is arranged on the outside of workplatform bearing 4, and control panel 5 and control setup 7 are arranged on control desk 6, and control setup 7 is electrically connected with the controller of scanner 1, walker actuating device 2, control panel 5 and marker mechanical arm 12.
When described scanner 1 is multiple, multiple scanner 1 standoff distance is arranged on the bottom surface, middle part of scanner walker 3, to increase scanning area.
Described workplatform movable pulley 8 is cardan wheel, and carries locking device, can realize moving freely of workplatform bearing 4 level attitude thus, and realizes the fixing of any position.
Described marker mechanical arm 12 is folding structure.
Now the automatic detection of wing pit in the aircraft maintenance that provides will be invented and the System Utilization Procedure of mark is described below: when needs keep in repair wing 10, first by engineering engineer, wing 10 being placed on wing places on workplatform 9, then on control panel 5, testing inspection parameter is inputted, under the control of control setup 7, utilize walker actuating device 2 by the gear driven scanner walker 3 in rack and pinion drive mechanism 11 on tooth bar from one end of workplatform bearing 4 to the other end steadily movement, in the process, scanner 1 pair of wing 10 surface is utilized to scan, then scan-data is sent to control setup 7, by control setup 7, above-mentioned data are processed, when finding pit, suspend walker actuating device 2, the pit depth obtained according to scanner 1 immediately with timed unit 7 and area data calculate the whole positions needed repairing, the labelling apparatus of control mark mechanical arm 12 lower end stretches to pit and marks in this position afterwards, thus provide important foundation for engineering engineer, and then repeat said process, until complete whole testing process.
The above; be only preferred embodiment of the present invention; not in order to limit the present invention, every above embodiment is done according to technical spirit of the present invention any trickle amendment, equivalently replace and improve, within the protection domain that all should be included in technical solution of the present invention.
Claims (4)
1. in an aircraft maintenance wing pit automatic detection and mark system, it is characterized in that: in described aircraft maintenance wing pit automatic detection and mark system comprise: at least one scanner (1), walker actuating device (2), scanner walker (3), workplatform bearing (4), control panel (5), control desk (6), control setup (7), multiple workplatform movable pulley (8), wing places workplatform (9), two groups of rack and pinion drive mechanisms (11) and marker mechanical arm (12), wherein, described wing places the middle part that workplatform (9) is horizontally set on workplatform bearing (4), a workplatform movable pulley (8) is installed in each bight, lower end of workplatform bearing (4) respectively, rack and pinion drive mechanism (11) is made up of gear and tooth bar, and two groups of rack and pinion drive mechanisms (11) are symmetrical arranged, and its middle rack level is arranged on a side roof part of workplatform bearing (4), a gear that can be meshed with corresponding tooth bar is pivotally installed respectively in the two ends of scanner walker (3), the outputting power mechanism of walker actuating device (2) is connected with a gear, is moved by gear for driving scanner walker (3) along tooth bar, scanner (1) is arranged on the bottom surface, middle part of scanner walker (3), the upper end of marker mechanical arm (12) is fixed on the middle part of scanner walker (3), and lower end is provided with labelling apparatus, control desk (6) is arranged on the outside of workplatform bearing (4), control panel (5) and control setup (7) are arranged on control desk (6), and control setup (7) is electrically connected with the controller of scanner (1), walker actuating device (2), control panel (5) and marker mechanical arm (12).
2. in aircraft maintenance according to claim 1 wing pit automatic detection and mark system, it is characterized in that: described scanner (1) is for time multiple, multiple scanner (1) standoff distance is arranged on the bottom surface, middle part of scanner walker (3), to increase scanning area.
3. in aircraft maintenance according to claim 1 wing pit automatic detection and mark system, it is characterized in that: described workplatform movable pulley (8) is cardan wheel, and carry locking device, moving freely of workplatform bearing (4) level attitude can be realized thus, and realize the fixing of any position.
4. in aircraft maintenance according to claim 1 wing pit automatic detection and mark system, it is characterized in that: described marker mechanical arm (12) is folding structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510756405.2A CN105346730B (en) | 2015-11-06 | 2015-11-06 | The automatic detection of wing pit and the system for marking in a kind of aircraft maintenance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510756405.2A CN105346730B (en) | 2015-11-06 | 2015-11-06 | The automatic detection of wing pit and the system for marking in a kind of aircraft maintenance |
Publications (2)
| Publication Number | Publication Date |
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| CN105346730A true CN105346730A (en) | 2016-02-24 |
| CN105346730B CN105346730B (en) | 2017-07-04 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201510756405.2A Expired - Fee Related CN105346730B (en) | 2015-11-06 | 2015-11-06 | The automatic detection of wing pit and the system for marking in a kind of aircraft maintenance |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108482642A (en) * | 2018-03-07 | 2018-09-04 | 华北水利水电大学 | Aerial survey unmanned plane wing repairs frame and its restorative procedure |
| CN108516102A (en) * | 2018-04-28 | 2018-09-11 | 中电科芜湖钻石飞机制造有限公司 | Flexible universal aircraft supporting tool |
| CN109557170A (en) * | 2018-12-03 | 2019-04-02 | 中国人民解放军国防科技大学 | SQUID-based wing detection system and detection method thereof |
| CN110040114A (en) * | 2019-05-16 | 2019-07-23 | 何佰胜 | A kind of automobile intelligent maintenance spray robot and auto repair method |
| CN112258336A (en) * | 2020-10-21 | 2021-01-22 | 安徽亘浩机械设备制造有限公司 | Workpiece processing flow mark management system and device |
Citations (5)
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| US20020072297A1 (en) * | 1999-12-08 | 2002-06-13 | Steven Kennerknecht | Automated method and apparatus for aircraft surface finishing |
| CN202798906U (en) * | 2012-09-12 | 2013-03-13 | 广州中国科学院沈阳自动化研究所分所 | Scanner based on Cartesian coordinate robot technology |
| CN203535124U (en) * | 2013-10-14 | 2014-04-09 | 浙江大学 | Scanning mechanism of electromagnetic compatible scanner |
| US20140305217A1 (en) * | 2013-04-12 | 2014-10-16 | The Boeing Company | Apparatus for Automated Rastering of an End Effector Over an Airfoil-Shaped Body |
| CN204228138U (en) * | 2014-11-25 | 2015-03-25 | 宁夏共享模具有限公司 | A kind of industrial robot for large parts dimensional measurement |
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2015
- 2015-11-06 CN CN201510756405.2A patent/CN105346730B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020072297A1 (en) * | 1999-12-08 | 2002-06-13 | Steven Kennerknecht | Automated method and apparatus for aircraft surface finishing |
| CN202798906U (en) * | 2012-09-12 | 2013-03-13 | 广州中国科学院沈阳自动化研究所分所 | Scanner based on Cartesian coordinate robot technology |
| US20140305217A1 (en) * | 2013-04-12 | 2014-10-16 | The Boeing Company | Apparatus for Automated Rastering of an End Effector Over an Airfoil-Shaped Body |
| CN203535124U (en) * | 2013-10-14 | 2014-04-09 | 浙江大学 | Scanning mechanism of electromagnetic compatible scanner |
| CN204228138U (en) * | 2014-11-25 | 2015-03-25 | 宁夏共享模具有限公司 | A kind of industrial robot for large parts dimensional measurement |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108482642A (en) * | 2018-03-07 | 2018-09-04 | 华北水利水电大学 | Aerial survey unmanned plane wing repairs frame and its restorative procedure |
| CN108516102A (en) * | 2018-04-28 | 2018-09-11 | 中电科芜湖钻石飞机制造有限公司 | Flexible universal aircraft supporting tool |
| CN108516102B (en) * | 2018-04-28 | 2023-09-26 | 中电科芜湖钻石飞机制造有限公司 | Flexible general aircraft support tool |
| CN109557170A (en) * | 2018-12-03 | 2019-04-02 | 中国人民解放军国防科技大学 | SQUID-based wing detection system and detection method thereof |
| CN110040114A (en) * | 2019-05-16 | 2019-07-23 | 何佰胜 | A kind of automobile intelligent maintenance spray robot and auto repair method |
| CN112258336A (en) * | 2020-10-21 | 2021-01-22 | 安徽亘浩机械设备制造有限公司 | Workpiece processing flow mark management system and device |
| CN112258336B (en) * | 2020-10-21 | 2024-04-16 | 安徽亘浩机械设备制造有限公司 | Workpiece processing flow mark management system and device |
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| Publication number | Publication date |
|---|---|
| CN105346730B (en) | 2017-07-04 |
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