CN104743133A - Lubricating maintenance device based on aircraft - Google Patents
Lubricating maintenance device based on aircraft Download PDFInfo
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- CN104743133A CN104743133A CN201510150752.0A CN201510150752A CN104743133A CN 104743133 A CN104743133 A CN 104743133A CN 201510150752 A CN201510150752 A CN 201510150752A CN 104743133 A CN104743133 A CN 104743133A
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Abstract
The invention discloses a lubricating maintenance device based on an aircraft and belongs to the technical field of applications of aircrafts. The lubricating maintenance device based on the aircraft comprises a vehicle, an aircraft body, a steering engine linkage group and an oiling device. The vehicle comprises a control station and a vehicle compartment. The aircraft body is arranged in the vehicle compartment. The control station controls the flight of the aircraft body and the oiling operation of the oiling device. The oiling device is connected with the aircraft body through the steering engine linkage group. The oiling position and the oiling angle of an oil nozzle can be adjusted by changing the posture of each steering engine in the steering engine linkage group. It is guaranteed that oiling operation is accurately and efficiently conducted through a mechanical arm and an observation mechanism. According to the lubricating maintenance device based on the aircraft, the oiling device is carried by the aircraft, oiling lubrication is conducted in the air, the limitation of a working environment is broken through, operation is easy, the safety is high, efficiency is high, and effective combination between the aircraft and the oiling device is achieved.
Description
Technical field
The present invention relates to aircraft applications technical field, more particularly, relate to a kind of lubricated maintenance equipment based on aircraft.
Background technology
A national development be unable to do without industry, and industrial expansion be unable to do without iron and steel, and the normal operation of steel iron facilities, equipment be unable to do without periodical maintenance.Operationally, can constantly rub between its moving part, movable part mating surfaces plays heat and constantly consumes lubricating oil steel piece, once lack of lubrication, movable part mating surfaces heat rolls up, and damage steel piece, causing producing running normally cannot carry out.Therefore, need regularly to safeguard steel piece, comprise maintenance and lubricated.The production facilities on ground can manually add when adding lubricating oil, or machine pump oil, but for the lubricating point that present position is higher, the tower top rotating shaft of such as rotary lighthouse, the rotating shaft etc. of aerial windmill, need to have assisted lubricated maintenance task by ladder or lift car at interpolation lubricating oil often.This lubricated maintenance mode danger is higher, complex operation, and efficiency is low, completes full maintenance cost cost higher, usually can have influence on normally carrying out of other productions in work progress.But still there is no reasonable actv. solution to improve this lubricated maintenance mode at present.
As everyone knows, rotor craft be a kind of can the small-sized unmanned aircraft of vertical takeoff and landing, its advantage is: can adapt to various environment; Possess autonomous take-off and landing ability, highly intelligent; Can fly with various attitude, as hovering, frontly to fly, side flies and inverted flight etc.Main application has: be difficult to close or very unattainable working environment; Dangerous working environment; The working environment that flight is dull; High-time working environment.But current rotor craft is applied to more takes photo by plane, captures article aspect, still not by the complete skill scheme of aircraft applications to lubricated maintenance aspect.
When implementing using aircraft to lubricate in the air, the main difficult problem that there are following three aspects: 1) how to make aircraft and oiling device combine; 2) how to operate oiling device and complete aerial oiling; 3) in oiling process, the accuracy of oiling how is ensured.Due to these difficult problems that the anabolic process of aircraft and oiling device exists, cause the technical development of this respect slow, therefore, need a set of effective scheme to solve the problems referred to above.
Summary of the invention
1. invent the technical matters that will solve
When lubricated maintenance being carried out to eminence lubricating point in view of adopting existing apparatus, danger is high, efficiency is low, oiling difficulty in partial lubrication region is larger, the invention provides a kind of lubricated maintenance equipment based on aircraft, the present invention is carrier based on automobile, carry oiling device on board the aircraft and carry out aerial oil injecting lubricating, break away from working environment restriction, simple to operate, safety is high, oiling is accurate, efficiency is high, achieves effective combination of aircraft and oiling device, makes aircraft applications technology obtain effective development in life.
2. technical scheme
For achieving the above object, technical scheme provided by the invention is:
A kind of lubricated maintenance equipment based on aircraft of the present invention, comprise automobile, aircraft body, steering wheel linkage groups and oiling device, described automobile comprises control radio station and railway carriage, and be provided with aircraft body in railway carriage, described aircraft body is connected with oiling device by steering wheel linkage groups; Described control radio station controls the flight of aircraft body and the oiling operation of oiling device.
As further improvement of the present invention, described steering wheel linkage groups comprises the first steering wheel being fixed on aircraft body bottom portion, the second steering wheel be connected with the rotating shaft of the first steering wheel, around the 3rd steering wheel that the second steering wheel fork rotates, the 4th steering wheel rotated around the 3rd steering wheel fork and the 5th steering wheel be fixed on the 4th steering wheel, the rotating shaft of described 5th steering wheel is fixed with loading plate, and described oiling device is fixed on loading plate.
As further improvement of the present invention, described steering wheel linkage groups is also connected with manipulator, this manipulator clamping device to be lubricated.
As further improvement of the present invention, described manipulator comprises gear steering wheel, driving wheel, flower wheel, supporting rod and connecting rod, described gear steering wheel is fixed on the downside of loading plate, the rotating shaft of gear steering wheel is connected with driving wheel, described flower wheel is arranged on the downside of loading plate, and driving wheel and flower wheel engaged transmission; Driving wheel and flower wheel are hinged with supporting rod respectively, hinged in the middle part of described connecting rod one end and supporting rod, the connecting rod other end by pin and loading plate jag hinged.
As further improvement of the present invention, described oiling device comprises squirt can and oil nozzle controls steering wheel, and oil nozzle controls the connecting rod of steering wheel and is connected with the oil nozzle valve of squirt can.
As further improvement of the present invention, described aircraft body is provided with sampling mechanism, in this sampling mechanism, is provided with pick up camera.
As further improvement of the present invention, described aircraft body is electrically connected by cable rope and control radio station.
As further improvement of the present invention, be provided with winding mechanism in described railway carriage, described cable rope is wrapped in the rotating shaft of this winding mechanism.
As further improvement of the present invention, described railway carriage top is provided with tooth bar, and the top cover of railway carriage is provided with gear, is controlled the top cover folding of railway carriage by the engaged transmission of wheel and rack.
3. beneficial effect
Adopt technical scheme provided by the invention, compared with prior art, there is following beneficial effect:
(1) a kind of lubricated maintenance equipment based on aircraft of the present invention, by steering wheel linkage groups, oiling device is connected with aircraft body, the feature of aircraft maneuverability is utilized to break away from the restriction of working environment to lubricated maintenance work, the attitude of each steering wheel in steering wheel linkage groups constantly can be changed in after oiling, and then the oiling position of adjustment oil nozzle, achieve effective combination of aircraft and oiling device, simple to operate, time saving and energy saving, safety is high;
(2) a kind of lubricated maintenance equipment based on aircraft of the present invention, steering wheel linkage groups is connected with manipulator, by the gear servos control driving wheel in manipulator and flower wheel engaged transmission, and then drive supporting rod open or clamp, utilize this supporting rod to clamp the device treating oil injecting lubricating, make oil nozzle not depart from oiling point; Aircraft body is also provided with sampling mechanism, real-time monitored pick up camera shooting picture, aircraft can be flown to assigned address quickly and accurately, and ensure the accuracy of oiling;
(3) a kind of lubricated maintenance equipment based on aircraft of the present invention, automobile is provided with and controls radio station, and aircraft body and this control radio station are electrically connected by cable rope, contribute to the flying power improving aircraft body on the one hand, for outdoor long working provides safeguard; Contribute to the quick transmission of signal on the other hand, avoid producing signal delay phenomenon;
(4) a kind of lubricated maintenance equipment based on aircraft of the present invention, winding mechanism is provided with in railway carriage, this winding mechanism can perform the action of corresponding release, rolling cable rope according to the lifting signal of aircraft body, degree of automation is high, and it is rational in infrastructure, easy to carry, be convenient to promote the use of.
Accompanying drawing explanation
Fig. 1 is the structural representation of a kind of lubricated maintenance equipment based on aircraft of the present invention;
Fig. 2 is the connection diagram of oiling device and aircraft body in the present invention;
Fig. 3 is the structural representation of steering wheel linkage groups in the present invention;
Fig. 4 is the structural representation of manipulator in the present invention;
Fig. 5 is the structural representation of sampling mechanism in the present invention.
Label declaration in schematic diagram: 1, automobile; 2, railway carriage; 3, cable rope; 4, aircraft body; 41, main oar duct; 42, auxiliary propeller; 43, auxiliary oar support; 44, auxiliary oar mounting rod; 45, sampling mechanism; 46, alighting gear; 5, steering wheel linkage groups; 51, the first steering wheel; 52, the second steering wheel; 53, the 3rd steering wheel; 54, the 4th steering wheel; 55, the 5th steering wheel; 56, loading plate; 6, manipulator; 61, gear steering wheel; 62, driving wheel; 63, flower wheel; 64, supporting rod; 65, connecting rod; 66, pin; 7, oiling device; 71, squirt can; 72, oil nozzle controls steering wheel.
Detailed description of the invention
For understanding content of the present invention further, the present invention is described in detail in conjunction with the accompanying drawings and embodiments.
Embodiment 1
Referring to Fig. 1, a kind of lubricated maintenance equipment based on aircraft of the present embodiment, primarily of compositions such as automobile 1, aircraft body 4, steering wheel linkage groups 5 and oiling devices 7.Automobile 1 comprises control radio station and railway carriage 2, and be provided with aircraft body 4 in railway carriage 2, oiling device 7 is connected with aircraft body 4 by steering wheel linkage groups 5, and aircraft body 4 is electrically connected by cable rope 3 and control radio station.The present embodiment is carrier based on automobile 1, and this automobile 1 is general-utility car, also can be by the unmanned vehicle of people's remote control, Figure 1 shows that unmanned vehicle.Aircraft body 4 can be assisted to carry out lubricated maintenance operation out of doors by automobile 1, contribute to the flying power improving aircraft body on the one hand, for outdoor long working provides safeguard; Directly controlling the flight of aircraft body 4 and the oiling operation of oiling device 7 by controlling radio station on the other hand, carrying out short-range signal transmission, contributing to the quick transmission of signal, avoid producing signal delay phenomenon.
Referring to Fig. 2, the aircraft body 4 of the present embodiment comprises main screw, main oar duct 41, auxiliary propeller 42 and alighting gear 46.Main screw is arranged in main oar duct 41, and main screw is upper and lower two paddle structure.Described main oar duct 41 is connected mutually with the overall architecture of aircraft body 4, is fixed with 4 auxiliary oar supports 43 on the downside of main oar duct 41, and auxiliary propeller 42 is connected with auxiliary oar support 43 by auxiliary oar mounting rod 44.Described auxiliary oar support 43 is provided with rotating shaft, and this rotating shaft its rotation of electric machine control by auxiliary oar support 43 is installed, described auxiliary oar mounting rod 44 is rotationally connected by rotating shaft and auxiliary oar support 43, and its slewing area is 0 ~ 120 °.When being in 0 ° of position, auxiliary oar mounting rod 44 is positioned on the omnibearing line of main oar duct 41, and auxiliary propeller 42 is in this position and main screw collaborative work; When turning to 120 ° of positions, auxiliary oar mounting rod 44 is hidden on the downside of main oar duct 41, auxiliary propeller 42 is also positioned on the downside of main oar duct 41 simultaneously, aircraft body 4 relies on main screw to complete lifting action, this state is mainly enabled when aircraft body 4 rises or drops in railway carriage 2, is convenient to transport and carries.In order to make aircraft body 4 can safe falling, and ensure the stationarity in transportation, the bottom bracket of aircraft body 4 is provided with circular alighting gear 46.The unmanned plane structure that the present embodiment adopts can provide larger lift, and energy consumption is less; The stationarity of hovering, flight can be ensured by four small-sized auxiliary propellers 42, avoid rocking when oiling operation, improve lubricated maintenance operating efficiency.
Referring to Fig. 2 and Fig. 3, steering wheel linkage groups 5 in the present embodiment comprises the first steering wheel 51 be fixed on bottom aircraft body 4, the second steering wheel 52 be connected with the rotating shaft of the first steering wheel 51, around the 3rd steering wheel 53 that the second steering wheel 52 fork rotates, the 4th steering wheel 54 rotated around the 3rd steering wheel 53 fork and the 5th steering wheel 55 be fixed on the 4th steering wheel 54, the rotating shaft of the 5th steering wheel 55 is fixed with loading plate 56, and described oiling device 7 is fixed on loading plate 56.Oiling device 7 up-and-down movement in perpendicular can be made by the second steering wheel 52, the 3rd steering wheel 53 and the 4th steering wheel 54, oiling device 7 can be made to rotate by the 5th steering wheel 55, the attitude of each steering wheel in steering wheel linkage groups 5 can be controlled by controlling radio station, and then realize the adjustment oil nozzle position of oiling device 7 and the object of oiling angle.
Oiling device 7 in the present embodiment comprises squirt can 71 and oil nozzle controls steering wheel 72, and oil nozzle controls the connecting rod of steering wheel 72 and is connected with the oil nozzle valve of squirt can 71, then can handle the folding of oil nozzle valve by controlling radio station.
Referring to Fig. 4, steering wheel linkage groups 5 in the present embodiment is also connected with manipulator 6, this manipulator 6 comprises gear steering wheel 61, driving wheel 62, flower wheel 63, supporting rod 64 and connecting rod 65, gear steering wheel 61 is fixed on the downside of loading plate 56, the rotating shaft of gear steering wheel 61 is connected with driving wheel 62, described flower wheel 63 is arranged on the downside of loading plate 56, and driving wheel 62 and flower wheel 63 engaged transmission.Driving wheel 62 and flower wheel 63 are hinged with supporting rod 64 respectively, and hinged in the middle part of described connecting rod 65 one end and supporting rod 64, connecting rod 65 other end is hinged by pin 66 and loading plate 56 jag.Wherein: there are teeth 1/3rd circular arc sector of driving wheel 62 and flower wheel 63, to limit the folding scope of supporting rod 64.When driving wheel 62 rotates to side, opening between supporting rod 64 becomes large, on the contrary then openings get smaller.After oil nozzle being aimed at lubricating point in oiling process, pinion steering wheel 61 rotates, and supporting rod 64 clamps device to be lubricated, then starts oiling, can effectively avoid answering oil nozzle to rock, and improves the accuracy of oil nozzle oiling.In addition, the folding end of supporting rod 64 is provided with striped, to increase the friction between contact surface, improves the steadiness of clamping.
Referring to Fig. 5, the aircraft body 4 of the present embodiment is also provided with sampling mechanism 45, this sampling mechanism 45 is fixed on auxiliary oar support 43, and is positioned at the same side with oiling device 7.Pick up camera is provided with in this sampling mechanism 45, by the anglec of rotation of each steering wheel in adjustment sampling mechanism 45, pick up camera can be made the oil nozzle track up of oiling device 7, by cable rope 3, picture signal is delivered to control radio station also to show on a display screen, oil nozzle position and the oiling angle of oiling device 7 is adjusted in real time, to ensure lubricated maintenance work carrying out rapidly and efficiently according to photographic images.
Bottom the railway carriage 2 of the present embodiment, winding mechanism is housed, described cable rope 3 is wrapped in the rotating shaft of this winding mechanism, this winding mechanism is electrically connected with control radio station, can, according to the lifting signal release of aircraft body 4 or rolling cable rope 3, this equipment be reached increasingly automated.Described railway carriage 2 top is provided with tooth bar, and the top cover of railway carriage 2 is provided with gear, and the gear on top cover, by servos control, controls the folding of railway carriage 2 top cover by the engaged transmission of wheel and rack.
During concrete use, opened by railway carriage 2 top cover by controlling radio station, main screw rotates, aircraft body 4 is risen in railway carriage 2, then control auxiliary oar mounting rod 44 and turn to 0 ° of position, auxiliary propeller 42 is started working, and aircraft body 4 carries oiling device 7 smooth flight; Then pick up camera in sampling mechanism 45 is started, shooting picture is observed from read-out, control steering wheel linkage groups 5 to trail, after determining position, oil nozzle aims at oiling position, and the supporting rod 64 of driving device hand 6 clamps attending device to be lubricated, and aircraft body 4 is in sustained hover, start oil nozzle and control steering wheel 72, start oiling.After oiling operation completes, control aircraft body 4 fly back above railway carriage 2 by controlling radio station, auxiliary propeller 42 quits work, and forward on the downside of main oar duct 41, control steering wheel linkage groups 5 to rotate simultaneously, each steering wheel fork is amounted to, then drops in railway carriage 2 by aircraft body 4, top cover closes.In the present embodiment, aircraft body 4 and oiling device 7 actv. combine, and simple to operate, efficiency is high, and safety is high, is convenient to promote the use of.
Schematically above be described the present invention and embodiment thereof, this description does not have restricted, and also just one of the embodiments of the present invention shown in accompanying drawing, actual structure is not limited thereto.So, if those of ordinary skill in the art enlightens by it, when not departing from the invention aim, designing the frame mode similar to this technical scheme and embodiment without creationary, all should protection scope of the present invention be belonged to.
Claims (9)
1. the lubricated maintenance equipment based on aircraft, it is characterized in that: comprise automobile (1), aircraft body (4), steering wheel linkage groups (5) and oiling device (7), described automobile (1) comprises control radio station and railway carriage (2), be provided with aircraft body (4) in railway carriage (2), described aircraft body (4) is connected with oiling device (7) by steering wheel linkage groups (5); Described control radio station controls the flight of aircraft body (4) and the oiling operation of oiling device (7).
2. a kind of lubricated maintenance equipment based on aircraft according to claim 1, it is characterized in that: described steering wheel linkage groups (5) comprises the first steering wheel (51) being fixed on aircraft body (4) bottom, the second steering wheel (52) be connected with the rotating shaft of the first steering wheel (51), around the 3rd steering wheel (53) that the second steering wheel (52) fork rotates, the 4th steering wheel (54) rotated around the 3rd steering wheel (53) fork and the 5th steering wheel (55) be fixed on the 4th steering wheel (54), the rotating shaft of described 5th steering wheel (55) is fixed with loading plate (56), described oiling device (7) is fixed on loading plate (56).
3. a kind of lubricated maintenance equipment based on aircraft according to claim 2, is characterized in that: described steering wheel linkage groups (5) is also connected with manipulator (6), and this manipulator (6) clamps device to be lubricated.
4. a kind of lubricated maintenance equipment based on aircraft according to claim 3, it is characterized in that: described manipulator (6) comprises gear steering wheel (61), driving wheel (62), flower wheel (63), supporting rod (64) and connecting rod (65), described gear steering wheel (61) is fixed on loading plate (56) downside, the rotating shaft of gear steering wheel (61) is connected with driving wheel (62), described driving wheel (62) and flower wheel (63) engaged transmission; Driving wheel (62) and flower wheel (63) are hinged with supporting rod (64) respectively, described connecting rod (65) one end and supporting rod (64) middle part hinged, connecting rod (65) other end is hinged by pin (66) and loading plate (56) jag.
5. a kind of lubricated maintenance equipment based on aircraft according to any one of claim 2 to 4, it is characterized in that: described oiling device (7) comprises squirt can (71) and oil nozzle controls steering wheel (72), the connecting rod that oil nozzle controls steering wheel (72) is connected with the oil nozzle valve of squirt can (71).
6. a kind of lubricated maintenance equipment based on aircraft according to claim 5, is characterized in that: described aircraft body (4) is provided with sampling mechanism (45), and this sampling mechanism is provided with pick up camera in (45).
7. a kind of lubricated maintenance equipment based on aircraft according to claim 6, is characterized in that: described aircraft body (4) is electrically connected by cable rope (3) and control radio station.
8. a kind of lubricated maintenance equipment based on aircraft according to claim 7, is characterized in that: described railway carriage is provided with winding mechanism in (2), and described cable rope (3) is wrapped in the rotating shaft of this winding mechanism.
9. a kind of lubricated maintenance equipment based on aircraft according to claim 8, it is characterized in that: described railway carriage (2) top is provided with tooth bar, the top cover of railway carriage (2) is provided with gear, is controlled the top cover folding of railway carriage (2) by the engaged transmission of wheel and rack.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510150752.0A CN104743133B (en) | 2015-03-31 | 2015-03-31 | Lubricating maintenance device based on aircraft |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510150752.0A CN104743133B (en) | 2015-03-31 | 2015-03-31 | Lubricating maintenance device based on aircraft |
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| CN104743133A true CN104743133A (en) | 2015-07-01 |
| CN104743133B CN104743133B (en) | 2017-02-01 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201510150752.0A Active CN104743133B (en) | 2015-03-31 | 2015-03-31 | Lubricating maintenance device based on aircraft |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105539877A (en) * | 2015-12-20 | 2016-05-04 | 赵世龙 | Aerial tanker maintenance auxiliary vehicle |
| CN110576981A (en) * | 2019-08-19 | 2019-12-17 | 沈阳宝通门业有限公司 | Adjustable inclination angle type vertical tail dock working platform |
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| CN104215640A (en) * | 2014-08-18 | 2014-12-17 | 南京航空航天大学 | Wind-generator blade defect damage inspection method and inspection system based on unmanned helicopter |
| CN204507291U (en) * | 2015-03-31 | 2015-07-29 | 马鞍山市赛迪智能科技有限公司 | A kind of lubricated maintenance equipment based on aircraft |
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Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
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| DE19808777A1 (en) * | 1998-03-03 | 1999-09-09 | Quaas | Annular free flight body used as carrier for observation and measurement systems |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN105539877A (en) * | 2015-12-20 | 2016-05-04 | 赵世龙 | Aerial tanker maintenance auxiliary vehicle |
| CN110576981A (en) * | 2019-08-19 | 2019-12-17 | 沈阳宝通门业有限公司 | Adjustable inclination angle type vertical tail dock working platform |
| CN110576981B (en) * | 2019-08-19 | 2024-04-30 | 沈阳宝通门业有限公司 | Inclination-adjustable vertical tail dock working platform |
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| Publication number | Publication date |
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| CN104743133B (en) | 2017-02-01 |
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Effective date of registration: 20191225 Address after: 211100 science and technology innovation center, No.18, Tiancheng Road, Binjiang Economic Development Zone, Jiangning District, Nanjing City, Jiangsu Province Patentee after: Nanjing Liangma Geographic Information Technology Co., Ltd Address before: 243000 Anhui city of Ma'anshan province high tech Zone at 1669 North Road Huo sparkle Building No. 2 Patentee before: MA'ANSHAN SAIDI INTELLIGENT TECHNOLOGY CO., LTD. |
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