WO2023137887A1 - 一种飞机发动机风扇叶片清洗润滑系统 - Google Patents

一种飞机发动机风扇叶片清洗润滑系统 Download PDF

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Publication number
WO2023137887A1
WO2023137887A1 PCT/CN2022/086871 CN2022086871W WO2023137887A1 WO 2023137887 A1 WO2023137887 A1 WO 2023137887A1 CN 2022086871 W CN2022086871 W CN 2022086871W WO 2023137887 A1 WO2023137887 A1 WO 2023137887A1
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Prior art keywords
cleaning
lubricating
blade
aircraft engine
lubrication
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PCT/CN2022/086871
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English (en)
French (fr)
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牛国臣
高庆吉
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中国民航大学
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Publication of WO2023137887A1 publication Critical patent/WO2023137887A1/zh

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B08CLEANING
    • B08BCLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
    • B08B3/00Cleaning by methods involving the use or presence of liquid or steam
    • B08B3/04Cleaning involving contact with liquid
    • B08B3/10Cleaning involving contact with liquid with additional treatment of the liquid or of the object being cleaned, e.g. by heat, by electricity or by vibration
    • B08B3/12Cleaning involving contact with liquid with additional treatment of the liquid or of the object being cleaned, e.g. by heat, by electricity or by vibration by sonic or ultrasonic vibrations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25HWORKSHOP EQUIPMENT, e.g. FOR MARKING-OUT WORK; STORAGE MEANS FOR WORKSHOPS
    • B25H3/00Storage means or arrangements for workshops facilitating access to, or handling of, work tools or instruments
    • B25H3/02Boxes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25HWORKSHOP EQUIPMENT, e.g. FOR MARKING-OUT WORK; STORAGE MEANS FOR WORKSHOPS
    • B25H5/00Tool, instrument or work supports or storage means used in association with vehicles; Workers' supports, e.g. mechanics' creepers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16NLUBRICATING
    • F16N7/00Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated
    • F16N7/30Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated the oil being fed or carried along by another fluid
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

Definitions

  • the invention belongs to the technical field of aviation equipment, in particular to an aircraft engine fan blade cleaning and lubricating system.
  • Aircraft engaged in flying activities also known as aircraft, are divided into two categories: lighter-than-air aircraft and heavier-than-air aircraft.
  • the former rely on air static buoyancy to lift into the air, such as balloons, airships, etc., while the latter rely on aerodynamic force generated by relative motion with the air, such as airplanes and helicopters.
  • the present invention provides a cleaning and lubricating system for aircraft engine fan blades, which avoids the traditional manual cleaning and lubrication of engine fan blades, which has the problems of high labor intensity, poor cleaning effect, uneven lubrication, and the disadvantages of cleaning and lubricating solvents that damage human health.
  • an aircraft engine fan blade cleaning and lubrication system including a blade storage vehicle and a cleaning and lubrication device installed on one side of the blade storage vehicle.
  • a lubrication station in the cleaning and lubrication equipment.
  • the positioning mechanism includes a positioning guide rail, and two adjustment plates are provided on the lower surface of the blade storage cart.
  • the storage device includes a rotating disk, a ratchet wheel is provided at the bottom end of the rotating disk, and a flange shaft is sleeved on the bottom end of the ratchet wheel, and several top posts are arranged on the upper surface of the rotating disk.
  • the loading and unloading station includes a bottom plate, a clamping mechanism is provided on the upper surface of the bottom plate, and an electromagnet connecting block is fixedly connected to one end of the clamping mechanism.
  • the mobile robot includes two Y-axis guide rails.
  • the two Y-axis guide rails are arranged on the upper surface of the cleaning and lubricating equipment.
  • the upper surface of the two Y-axis guide rails is provided with an X-axis guide rail.
  • One side of the X-axis guide rail is provided with a Z-axis guide rail.
  • the ultrasonic cleaning station includes an ultrasonic cleaning box, the upper surface of the ultrasonic cleaning box is provided with a shim fixture, the outer wall of the cleaning and lubricating equipment is provided with multiple groups of observation windows, both ends of the shim fixture are fixedly connected with a guide rod cylinder, and the bottom end of the conduit cylinder is fixedly connected with the lower surface of the inner wall of the cleaning and lubrication equipment, and a vibrator generator is arranged in the ultrasonic cleaning box.
  • the mechanical cleaning station includes a cleaning water tank, a rotating cylinder is installed in the cleaning water tank, the output end of the rotating cylinder is fixedly connected with a rotating arm, one end of the rotating arm is provided with a cleaning special-shaped groove, and the upper surface of the cleaning special-shaped groove is provided with a blade clamping groove.
  • the lubricating station includes a mechanical arm installation plate, an industrial robot is installed on the lower surface of the mechanical arm installation, a sprinkler irrigation installation plate is fixedly connected to the frame of the cleaning and lubrication equipment, and several lubrication spray cans are arranged on the upper surface of the sprinkler irrigation installation plate.
  • a part box is fixedly connected to the left end of the blade storage vehicle, and several shim holding mechanisms are arranged on the upper surface of the part box, and a shim block is arranged inside the shim holding mechanism.
  • the device uses the storage device on the blade storage vehicle to facilitate the transportation of the disassembled engine blades to the explosion-proof workshop. After docking with the cleaning and lubrication equipment, the automatic cleaning, testing and lubrication operations can be carried out.
  • the blade storage vehicle is equipped with positioning guide rails, which is convenient for docking with the cleaning and lubrication device. , to provide better protection for engine flight safety.
  • the device uses ultrasonic cleaning to clean the three workpieces of the aircraft engine fan blades, and the disassembled parts of the blade caulking block and the caulking piece. Vibrator generators are installed on the bottom, left and right sides of the ultrasonic equipment to improve its cleaning effect. Secondly, the cleaning of the dovetail base area of the blades is done mechanically. The rotating arm is driven by the rotating air and the cleaning special-shaped groove connected to the rotating arm is synchronously controlled to reciprocate the dovetail base area of the engine blade to complete the mechanical cleaning operation.
  • the device can use the standard aviation material of the lubricating spray can for lubrication.
  • the lubricating station can grab the lubricating spray can and complete the lubrication task through the action of the industrial robot, the lubricating spray can and the spray can mounting plate. It has the technical advantages of strong lubrication uniformity and high lubrication efficiency.
  • Fig. 1 is the three-dimensional structure schematic diagram of the present invention
  • Fig. 2 is a schematic diagram of enlarged structure at A place in Fig. 1 of the present invention
  • Fig. 3 is the top view structure schematic diagram of the present invention.
  • Fig. 4 is a schematic diagram of the enlarged structure at B in Fig. 3 of the present invention.
  • Blade storage vehicle 1. Blade storage vehicle; 2. Cleaning and lubricating equipment; 3. Positioning mechanism; 31. Positioning guide rail; 32. Adjusting plate; 4. Storage device; 41. Rotary disc; 42. Flange shaft; 43. Ratchet; 44. Top column; 5. Loading and unloading station; 64. Servo motor; 7. Ultrasonic cleaning station; 72. Ultrasonic cleaning box; 73. Observation window; 74. Shim fixture; 75. Guide rod cylinder; Gap block; 11. Parts box; 12. Gap holding mechanism.
  • An aircraft engine fan blade cleaning and lubricating system as shown in Figures 1-4 includes a blade storage vehicle 1 and a cleaning and lubrication device 2 provided on one side of the blade storage vehicle 1.
  • the upper surface of the blade storage vehicle 1 is provided with a storage device 4.
  • the lower surface of the blade storage vehicle 1 is provided with a positioning mechanism 3.
  • the right side of the upper surface of the blade storage vehicle 1 is provided with a loading and unloading station 5.
  • the upper surface of the cleaning and lubrication equipment 2 is provided with a mobile robot 6.
  • Position 7, the lubricating station 8 is arranged in the cleaning and lubricating equipment 2 .
  • the operator When in use, the operator first transports the disassembled engine blades to the explosion-proof workshop through the blade storage vehicle 1, and connects with the cleaning and lubrication equipment 2, and transfers the blades to be cleaned to the mechanical cleaning station 9, the ultrasonic cleaning station 7 and the lubrication station 8 through the mobile robot 6 respectively.
  • the positioning mechanism 3 includes a positioning guide rail 31, and two adjustment plates 32 are provided on the lower surface of the blade storage vehicle 1;
  • the blade storage vehicle 1 can be pushed onto the positioning guide rail 31 to complete docking with the cleaning and lubricating equipment 2 .
  • the storage device 4 includes a rotating disc 41, the bottom end of the rotating disc 41 is provided with a ratchet 43, and the bottom end of the ratchet 43 is sleeved with a flange shaft 42, and the upper surface of the rotating disc 41 is provided with several push posts 44;
  • the loading and unloading station 5 assembles the aircraft engine blades and the clamping mechanism 53, and places them on the top column 44 of the rotating disk 41.
  • the flange shaft 42 and the ratchet wheel 43 complete the pushing and rotating of the rotating disk 41.
  • the storage device 4 can store 24 blades at a time, that is, a set of engine blades.
  • the loading and unloading station 5 includes a bottom plate 52, the upper surface of the bottom plate 52 is provided with a clamping mechanism 53, and one end of the clamping mechanism 53 is fixedly connected with an electromagnet connecting block 51;
  • the electromagnet connecting block 51 can be used to fix it, and it is convenient to disassemble and take the blade at any time.
  • the frame mobile robot 6 includes two Y-axis guide rails 62, the two Y-axis guide rails 62 are arranged on the upper surface of the cleaning and lubricating equipment 2, and the upper surface of the two Y-axis guide rails 62 is provided with an X-axis guide rail 63, and one side of the X-axis guide rail 63 is provided with a Z-axis guide rail 61, and the tail of the Z-axis guide rail 61 is provided with an electromagnet, and one end of the X-axis guide rail 63 is fixedly connected to a servo motor 64;
  • the servo motor 64, the electromagnet and the Z-axis guide rail 61 are used to transfer the workpiece to be cleaned to the cleaning and lubricating station 8 under the connection and cooperation of the X-axis guide rail 63 and the Y-axis guide rail 62 .
  • the ultrasonic cleaning station 7 includes an ultrasonic cleaning box 71, the upper surface of the ultrasonic cleaning box 71 is provided with a shim fixture 73, the outer wall of the cleaning and lubricating equipment 2 is provided with multiple sets of observation windows 72, both ends of the shim fixture 73 are fixedly connected with a guide rod cylinder 74, and the bottom end of the guide cylinder is fixedly connected with the lower surface of the inner wall of the cleaning and lubrication equipment 2, and a vibrator generator is arranged in the ultrasonic cleaning box 71.
  • the operator places the shim on the shim holder 73, places the shim block 10 to be cleaned and the shim holder 73 on the guide rod cylinder 74 support through the observation window 72, and the guide rod cylinder 74 descends into the ultrasonic cleaning box 71 for ultrasonic cleaning.
  • the mechanical cleaning station 9 includes a cleaning water tank 93.
  • a rotating cylinder 91 is installed in the cleaning water tank 93.
  • the output end of the rotating cylinder 91 is fixedly connected to a rotating arm 92.
  • One end of the rotating arm 92 is provided with a cleaning special-shaped groove 94, and the upper surface of the cleaning special-shaped groove 94 is provided with a blade clamping groove 95.
  • the engine blade is placed in the blade slot 95, the cleaning solution is injected into the cleaning water tank 93, the rotating cylinder 91 drives the rotating arm 92, controls the cleaning special-shaped groove 94 connected with the rotating arm 92, and reciprocates the dovetail base area of the engine blade to complete the mechanical cleaning operation.
  • the lubricating station 8 includes a mechanical arm mounting plate 81, an industrial robot 82 is installed on the lower surface of the mechanical arm installation, a sprinkling irrigation mounting plate is fixedly connected to the frame of the cleaning and lubrication equipment 2, and several lubricating spray cans 84 are arranged on the upper surface of the sprinkling irrigation mounting plate.
  • the lubricating station 8 grabs the lubricating spray can 84 to complete the lubrication task through the action of the industrial robot 82, the lubricating spray can 84 and the spray can mounting plate 83, and the lubricating spray can 84 can use a molybdenum disulfide spray can.
  • the left end of the blade storage vehicle 1 is fixedly connected with a parts box 11 , and the upper surface of the parts box 11 is provided with several shim holding mechanisms 12 , and a shim block 10 is arranged inside the shim holding mechanisms 12 .
  • the shim holding mechanism 12 is used to store the shim workpiece to be cleaned, the shim block 10 is placed on the empty plate at the rear of the blade storage cart 1, and the parts box 11 provided at one end of the blade storage cart 1 is convenient for operators to store equipment.
  • a first feature being "on” or “under” a second feature may include that the first and second features are in direct contact, and may also include that the first and second features are not in direct contact but are in contact with another feature between them.
  • the first feature is "above” the second feature; “above” and “above” include that the first feature is directly above and obliquely above the second feature, or simply means that the level of the first feature is higher than that of the second feature.
  • the first feature is “below” the second feature; “below” and “under” include that the first feature is directly below and obliquely below the second feature, or simply means that the first feature is less horizontally than the second feature.

Abstract

一种飞机发动机风扇叶片清洗润滑系统,包括叶片存储车(1)和叶片存储车(1)一侧设置的清洗润滑设备(2),叶片存储车(1)的上表面设置有存储装置(4),叶片存储车(1)的下表面设置有定位机构(3);通过叶片存储车(1)上的存储装置(4),方便将拆卸后的发动机叶片运送至防爆车间,与清洗润滑设备(2)对接后即可进行自动化清洗、检测和润滑作业,叶片存储车(1)上设有定位导轨(31),便于与清洗润滑设备(2)对接,存储车(1)整体高度低,不会遮挡操作人员视线,同时利用工业机器人(6)抓取叶片至作业区域,可以自动化清洗、检测和润滑作业流程,该系统自动化程度更高、清洗和润滑效果更好,可以有效解放人力,提高作业的质量和效率,为发动机飞行安全提供更好保障。

Description

一种飞机发动机风扇叶片清洗润滑系统 技术领域
本发明属于航空设备技术领域,特别是涉及一种飞机发动机风扇叶片清洗润滑系统。
背景技术
从事飞行活动的飞行器,也称航空器,分为轻于空气的航空器和重于空气的航空器两类,前者依靠空气静浮力升空,如气球、飞艇等,后者依靠与空气作相对运动产生的空气动力升空,如飞机、直升机等,按照是否载人,可以分为有人机和无人机,飞机在日常维护时,需要对其发动机风扇叶片进行清洗。
传统的人工清洗、润滑发动机风扇叶片的方式,具有劳动强度大、清洗效果不佳、润滑不均匀,以及清洗、润滑溶剂损害人体健康的弊端,目前还没有能够代替人工清洗润滑航空发动机叶片作业的设备,为此我们提出了一种飞机发动机风扇叶片清洗润滑系统解决上述问题。
发明内容
为了克服现有技术的不足,本发明提供一种飞机发动机风扇叶片清洗润滑系统,避免了传统的人工清洗、润滑发动机风扇叶片的方式,具有劳动强度大、清洗效果不佳、润滑不均匀,以及清洗、润滑溶剂损害人体健康的弊端的问题。
为解决上述技术问题,本发明提供如下技术方案:一种飞机发动机风扇叶片清洗润滑系统,包括叶片存储车和叶片存储车一侧设置的清洗润滑设备,所述叶片存储车的上表面设置有存储装置,所述叶片存储车的下表面设置有定位机构,所述叶片存储车的上表面右侧设置有装卸工位,所述清洗润滑设备的上表面设置有衔架移动式机器人,所述清洗润滑设备靠近叶片存储车的一侧设置有机械清洗工位,所述清洗润滑设备内安装有超声波清洗工位,所述清洗润滑设备内设置有润滑工位。
作为本发明的一种优选技术方案,所述定位机构包括定位导轨,所述叶片存储车的下表面设置有两个调节板。
作为本发明的一种优选技术方案,所述存储装置包括旋转盘,所述旋转盘的底端设置有棘轮,且棘轮的底端套接有法兰轴,所述旋转盘的上表面设置有若干个顶柱。
作为本发明的一种优选技术方案,所述装卸工位包括底板,所述底板的上表面设置有夹持机构,所述夹持机构的一端固定连接有电磁铁连接块。
作为本发明的一种优选技术方案,所述衔架移动式机器人包括两个Y轴导轨,两个Y轴导轨设置在清洗润滑设备的上表面架体上,两个Y轴导轨的上表面设置有X轴导轨,所述X轴导轨的一侧设置有Z轴导轨,所述Z轴导轨尾部设置有电磁铁,所述X轴导轨的一端固定连接有伺服电机。
作为本发明的一种优选技术方案,所述超声波清洗工位包括超声波清洗箱,所述超声波清洗箱的上表面设置有填隙片夹具,所述清洗润滑设备的外壁设置有多组观察窗,所述填隙片夹具的两端均固定连接有导杆气缸,且导管气缸的底端与清洗润滑设备内壁的下表面固定连接,所述超声波清洗箱内安置有振子发生器。
作为本发明的一种优选技术方案,所述机械清洗工位包括清洗水槽,所述清洗水槽内安装有旋转气缸,所述旋转气缸的输出端固定连接有旋转臂,所述旋转臂的一端设置有清洁异形槽,所述清洁异形槽的上表面设置有叶片卡槽。
作为本发明的一种优选技术方案,所述润滑工位包括机械臂安装板,所述机械臂安装的下表面安装有工业机器人,所述清洗润滑设备的架体上固定连接有喷灌安装板,所述喷灌安装板的上表面设置有若干个润滑喷罐。
作为本发明的一种优选技术方案,所述叶片存储车的左端固定连接有零件箱,所述零件箱的上表面设置有若干个填隙片加持机构,所述填隙片加持机构内设置有填隙块。
与现有技术相比,本发明能达到的有益效果是:
1、该装置通过叶片存储车上的存储装置,方便将拆卸后的发动机叶片运送至防爆车间,与清洗润滑设备对接后即可进行自动化清洗、检测和润滑作业流程,在叶片存储车设有定位导轨,便于与清洗润滑装置对接,存储车整体高度低,不会遮挡操作人员视线,同时利 用工业机器人抓取叶片至作业区域,则可以自动化清洗、检测和润滑作业流程,该系统自动化程度更高、清洗和润滑效果更好,可以有效解放人力,提高作业的质量和效率,为发动机飞行安全提供更好保障。
2、该装置通过针对飞机发动机风扇叶片待清洗三个工件,对叶片填隙块和填隙片的拆卸件,采用超声波清洗方式进行清洁,超声波设备底部、左侧和右侧均安置有振子发生器,提高其清洗效果,其次,对叶片燕尾基座区域的清洗采用机械的方式,通过旋转气带动旋转臂并同步控制与旋转臂连接的清洁异形槽,对发动机叶片燕尾基座区域往复运动,完成机械清洗作业。
3、该装置可以根据维修工卡标准,润滑需要使用润滑喷罐标准航材,润滑工位通过工业机器人、润滑喷罐和喷罐安装板的作用,可以抓取润滑喷罐完成润滑任务,具有润滑均匀度强、润滑效率高的技术优势。
附图说明
图1为本发明的立体结构示意图;
图2为本发明的图1中A处放大结构示意图;
图3为本发明的俯视结构示意图;
图4为本发明的图3中B处放大结构示意图。
其中:1、叶片存储车;2、清洗润滑设备;3、定位机构;31、定位导轨;32、调节板;4、存储装置;41、旋转盘;42、法兰轴;43、棘轮;44、顶柱;5、装卸工位;51、电磁铁连接块;52、底板; 53、夹持机构;6、衔架移动式机器人;61、Z轴导轨;62、Y轴导轨;63、X轴导轨;64、伺服电机;7、超声波清洗工位;72、超声波清洗箱;73、观察窗;74、填隙片夹具;75、导杆气缸;8、润滑工位;82、机械臂安装板;82、工业机器人;83、喷罐安装板;84、润滑喷罐;9、机械清洗工位;91、旋转气缸;92、旋转臂;93、清洗水槽;94、清洁异形槽;95、叶片卡槽;10、填隙块;11、零件箱;12、填隙片加持机构。
具体实施方式
为了使本发明实现的技术手段;创作特征;达成目的与功效易于明白了解,下面结合具体实施例,进一步阐述本发明,但下述实施例仅仅为本发明的优选实施例,并非全部。基于实施方式中的实施例,本领域技术人员在没有做出创造性劳动的前提下所获得其它实施例,都属于本发明的保护范围。下述实施例中的实验方法,如无特殊说明,均为常规方法,下述实施例中所用的材料;试剂等,如无特殊说明,均可从商业途径得到。
实施例
如图1-图4所示的一种飞机发动机风扇叶片清洗润滑系统,包括叶片存储车1和叶片存储车1一侧设置的清洗润滑设备2,叶片存储车1的上表面设置有存储装置4,叶片存储车1的下表面设置有定位机构3,叶片存储车1的上表面右侧设置有装卸工位5,清洗润滑设备2的上表面设置有衔架移动式机器人6,清洗润滑设备2靠近叶片存储车1的一侧设置有机械清洗工位9,清洗润滑设备2内安装有 超声波清洗工位7,清洗润滑设备2内设置有润滑工位8。
使用时,首先由作业人员通过叶片存储车1将拆卸后的发动机叶片运送至防爆车间,并且与清洗润滑设备2相对接,通过衔架移动式机器人6将待清洗的叶片分别传送至机械清洗工位9、超声波清洗工位7和润滑工位8,由机械清洗工位9和超声波工位对叶片进行充分清洗后,再通过润滑工位8中的工业机器人82,操作润滑喷罐84进行自动润滑。
在其他实施例中,定位机构3包括定位导轨31,叶片存储车1的下表面设置有两个调节板32;
通过其设计,可以将叶片存储车1推送至定位导轨31上即可与清洗润滑设备2完成对接。
在其他实施例中,存储装置4包括旋转盘41,旋转盘41的底端设置有棘轮43,且棘轮43的底端套接有法兰轴42,旋转盘41的上表面设置有若干个顶柱44;
通过该设计,装卸工位5装配完飞机发动机叶片和夹持机构53,放置在旋转盘41的顶柱44上,法兰轴42和棘轮43完成旋转盘41的推动旋转,存储装置4一次可存储24片叶片,即一组发动机叶片。
在其他实施例中,装卸工位5包括底板52,底板52的上表面设置有夹持机构53,夹持机构53的一端固定连接有电磁铁连接块51;
通过该设计,在旋转打开夹持机构53对叶片进行夹持时,通过电磁铁连接块51即可以对其进行固定,且方便随时拆卸拿取叶片。
在其他实施例中,衔架移动式机器人6包括两个Y轴导轨62, 两个Y轴导轨62设置在清洗润滑设备2的上表面架体上,两个Y轴导轨62的上表面设置有X轴导轨63,X轴导轨63的一侧设置有Z轴导轨61,Z轴导轨61尾部设置有电磁铁,X轴导轨63的一端固定连接有伺服电机64;
通过该设计,利用伺服电机64、电磁铁和Z轴导轨61,在X轴导轨63和Y轴导轨62的连接配合下,负责将待清洗工件传送至清洗和润滑工位8。
在其他实施例中,超声波清洗工位7包括超声波清洗箱71,超声波清洗箱71的上表面设置有填隙片夹具73,清洗润滑设备2的外壁设置有多组观察窗72,填隙片夹具73的两端均固定连接有导杆气缸74,且导管气缸的底端与清洗润滑设备2内壁的下表面固定连接,超声波清洗箱71内安置有振子发生器。
通过该设计,操作人员将填隙片安置在填隙片夹具73上,通过观察窗72将待清洗的填隙块10、填隙片夹具73放置在导杆气缸74支架上,导杆气缸74下降至超声波清洗箱71中进行超声波清洗作业。
在其他实施例中,机械清洗工位9包括清洗水槽93,清洗水槽93内安装有旋转气缸91,旋转气缸91的输出端固定连接有旋转臂92,旋转臂92的一端设置有清洁异形槽94,清洁异形槽94的上表面设置有叶片卡槽95。
通过该设计,发动机叶片放置在叶片卡槽95内,清洗水槽93中注入清洗溶液,旋转气缸91带动旋转臂92,控制与旋转臂92连接的清洁异形槽94,对发动机叶片燕尾基座区域往复运动,完成机械 清洗作业。
在其他实施例中,润滑工位8包括机械臂安装板81,机械臂安装的下表面安装有工业机器人82,清洗润滑设备2的架体上固定连接有喷灌安装板,喷灌安装板的上表面设置有若干个润滑喷罐84。
通过该设计,润滑工位8通过工业机器人82、润滑喷罐84和喷罐安装板83的作用,抓取润滑喷罐84完成润滑任务,而润滑喷罐84可以采用二硫化钼喷罐。
在其他实施例中,叶片存储车1的左端固定连接有零件箱11,零件箱11的上表面设置有若干个填隙片加持机构12,填隙片加持机构12内设置有填隙块10。
通过该设计,填隙片加持机构12用于存放待清洗填隙片工件、填隙块10放置在叶片存储车1尾部空板盘上,叶片存储车1一端设置的零件箱11,便于操作人员存放设备。
在本发明中,除非另有明确的规定和限定,第一特征在第二特征之“上”或之“下”可以包括第一和第二特征直接接触,也可以包括第一和第二特征不是直接接触而是通过它们之间的另外的特征接触。而且,第一特征在第二特征“之上”;“上方”和“上面”包括第一特征在第二特征正上方和斜上方,或仅仅表示第一特征水平高度高于第二特征。第一特征在第二特征“之下”;“下方”和“下面”包括第一特征在第二特征正下方和斜下方,或仅仅表示第一特征水平高度小于第二特征。
以上显示和描述了本发明的基本原理;主要特征和本发明的优 点。本行业的技术人员应该了解,本发明不受上述实施例的限制,上述实施例和说明书中描述的仅为本发明的优选例,并不用来限制本发明,在不脱离本发明精神和范围的前提下,本发明还会有各种变化和改进,这些变化和改进都落入要求保护的本发明范围内。本发明要求保护范围由所附的权利要求书及其等效物界定。

Claims (9)

  1. 一种飞机发动机风扇叶片清洗润滑系统,包括叶片存储车(1)和叶片存储车(1)一侧设置的清洗润滑设备(2),其特征在于:所述叶片存储车(1)的上表面设置有存储装置(4),所述叶片存储车(1)的下表面设置有定位机构(3),所述叶片存储车(1)的上表面右侧设置有装卸工位(5),所述清洗润滑设备(2)的上表面设置有衔架移动式机器人(6),所述清洗润滑设备(2)靠近叶片存储车(1)的一侧设置有机械清洗工位(9),所述清洗润滑设备(2)内安装有超声波清洗工位(7),所述清洗润滑设备(2)内设置有润滑工位(8)。
  2. 根据权利要求1所述的一种飞机发动机风扇叶片清洗润滑系统,其特征在于:所述定位机构(3)包括定位导轨(31),所述叶片存储车(1)的下表面设置有两个调节板(32)。
  3. 根据权利要求1所述的一种飞机发动机风扇叶片清洗润滑系统,其特征在于:所述存储装置(4)包括旋转盘(41),所述旋转盘(41)的底端设置有棘轮(43),且棘轮(43)的底端套接有法兰轴(42),所述旋转盘(41)的上表面设置有若干个顶柱(44)。
  4. 根据权利要求1所述的一种飞机发动机风扇叶片清洗润滑系统,其特征在于:所述装卸工位(5)包括底板(52),所述底板(52)的上表面设置有夹持机构(53),所述夹持机构(53)的一端固定连接有电磁铁连接块(51)。
  5. 根据权利要求1所述的一种飞机发动机风扇叶片清洗润滑系 统,其特征在于:所述衔架移动式机器人(6)包括两个Y轴导轨(62),两个Y轴导轨(62)设置在清洗润滑设备(2)的上表面架体上,两个Y轴导轨(62)的上表面设置有X轴导轨(63),所述X轴导轨(63)的一侧设置有Z轴导轨(61),所述Z轴导轨(61)尾部设置有电磁铁,所述X轴导轨(63)的一端固定连接有伺服电机(64)。
  6. 根据权利要求1所述的一种飞机发动机风扇叶片清洗润滑系统,其特征在于:所述超声波清洗工位(7)包括超声波清洗箱(71),所述超声波清洗箱(71)的上表面设置有填隙片夹具(73),所述清洗润滑设备(2)的外壁设置有多组观察窗(72),所述填隙片夹具(73)的两端均固定连接有导杆气缸(74),且导管气缸的底端与清洗润滑设备(2)内壁的下表面固定连接,所述超声波清洗箱(71)内安置有振子发生器。
  7. 根据权利要求1所述的一种飞机发动机风扇叶片清洗润滑系统,其特征在于:所述机械清洗工位(9)包括清洗水槽(93),所述清洗水槽(93)内安装有旋转气缸(91),所述旋转气缸(91)的输出端固定连接有旋转臂(92),所述旋转臂(92)的一端设置有清洁异形槽(94),所述清洁异形槽(94)的上表面设置有叶片卡槽(95)。
  8. 根据权利要求1所述的一种飞机发动机风扇叶片清洗润滑系统,其特征在于:所述润滑工位(8)包括机械臂安装板(81),所述机械臂安装的下表面安装有工业机器人(82),所述清洗润滑设备(2)的架体上固定连接有喷灌安装板(83),所述喷灌安装板(83) 的上表面设置有若干个润滑喷罐(84)。
  9. 根据权利要求1所述的一种飞机发动机风扇叶片清洗润滑系统,其特征在于:所述叶片存储车(1)的左端固定连接有零件箱(11),所述零件箱(11)的上表面设置有若干个填隙片加持机构(12),所述填隙片加持机构(12)内设置有填隙块(10)。
PCT/CN2022/086871 2022-01-20 2022-04-14 一种飞机发动机风扇叶片清洗润滑系统 WO2023137887A1 (zh)

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Families Citing this family (1)

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Publication number Priority date Publication date Assignee Title
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Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203803843U (zh) * 2014-05-07 2014-09-03 北京北宇机械设备有限公司 旋转喷淋超声波清洗机
CN205668808U (zh) * 2016-05-16 2016-11-02 机械科学研究总院先进制造技术研究中心 一种适用于等离子切割的自动化钢板分拣整理机器人
CN111168636A (zh) * 2020-03-04 2020-05-19 福州鹰高电子有限公司 一种石英钟组装用工具存取装置及方法
US20200355091A1 (en) * 2019-05-09 2020-11-12 Rolls-Royce Plc Washing tool, washing system and a method of washing
CN112845477A (zh) * 2021-01-22 2021-05-28 南京迪沃航空技术有限公司 一种飞机发动机叶片用清洁流水线及清洁方法
CN114042695A (zh) * 2022-01-13 2022-02-15 中国民航大学 一种飞机发动机风扇叶片清洗润滑设备
CN114054457A (zh) * 2022-01-13 2022-02-18 中国民航大学 一种叶片存储车装置
CN114082710A (zh) * 2022-01-20 2022-02-25 中国民航大学 一种飞机发动机风扇叶片清洗润滑系统

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010045869A1 (de) * 2010-08-03 2012-02-23 Mtu Aero Engines Gmbh Reinigung einer Turbomaschinenstufe
DE102016206246A1 (de) * 2016-04-14 2017-10-19 Lufthansa Technik Ag Verfahren und Vorrichtung zur Reinigung von Turbinenschaufeln
CN110053785A (zh) * 2019-04-18 2019-07-26 中国民航大学 一种飞机发动机风扇叶片清洗与喷涂装置
CN210253267U (zh) * 2019-05-20 2020-04-07 四川省自贡市海川实业有限公司 航空发动机叶片清洗用固定装置
CN214816683U (zh) * 2021-04-15 2021-11-23 北京航臻科技有限公司 一种用于自动化加工航空发动机叶片的夹具

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203803843U (zh) * 2014-05-07 2014-09-03 北京北宇机械设备有限公司 旋转喷淋超声波清洗机
CN205668808U (zh) * 2016-05-16 2016-11-02 机械科学研究总院先进制造技术研究中心 一种适用于等离子切割的自动化钢板分拣整理机器人
US20200355091A1 (en) * 2019-05-09 2020-11-12 Rolls-Royce Plc Washing tool, washing system and a method of washing
CN111168636A (zh) * 2020-03-04 2020-05-19 福州鹰高电子有限公司 一种石英钟组装用工具存取装置及方法
CN112845477A (zh) * 2021-01-22 2021-05-28 南京迪沃航空技术有限公司 一种飞机发动机叶片用清洁流水线及清洁方法
CN114042695A (zh) * 2022-01-13 2022-02-15 中国民航大学 一种飞机发动机风扇叶片清洗润滑设备
CN114054457A (zh) * 2022-01-13 2022-02-18 中国民航大学 一种叶片存储车装置
CN114082710A (zh) * 2022-01-20 2022-02-25 中国民航大学 一种飞机发动机风扇叶片清洗润滑系统

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
ZHU, TONG: "Research on Optimization of Aircraft Engine Fan Blade Cleaning Parameters", CHINA MASTER'S THESES FULL-TEXT DATABASE, 15 January 2021 (2021-01-15) *

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