CN208984345U - A kind of aero-engine runner inspection multifunctional belt favourable turn - Google Patents
A kind of aero-engine runner inspection multifunctional belt favourable turn Download PDFInfo
- Publication number
- CN208984345U CN208984345U CN201821847871.7U CN201821847871U CN208984345U CN 208984345 U CN208984345 U CN 208984345U CN 201821847871 U CN201821847871 U CN 201821847871U CN 208984345 U CN208984345 U CN 208984345U
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- China
- Prior art keywords
- gear
- favourable turn
- aero
- checks
- multifunctional belt
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- 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.)
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Abstract
The utility model discloses a kind of aero-engine runners to check multifunctional belt favourable turn, including tripod, fixed bandage, battery, driving motor, triple reduction gear and worm type of reduction gearing and controller；The beneficial effects of the utility model are; first; band favourable turn provides power using motor; by speed reducer deceleration torque increase to suitable revolving speed and torque; to drive the high pressure rotor of engine to rotate; be not only able to liberation worker labour, but also be able to pass through the controller control rotor positive and negative rotation and stop and speed regulation, feedback angle of rotor angle and overload protection；Secondly, band favourable turn is equipped with sound equipment, improves the work ethos state of worker by playing music, alleviates work fatigue；Finally, it is the light-weight, Portable belt of band favourable turn, easy to operate, it can preferably solve the practical problem of work on the spot.
Description
Technical field
The utility model relates to aero-engine detection device technical fields more particularly to a kind of aero-engine runner to examine
Look into multifunctional belt favourable turn.
Background technique
When past engine runner checks, special personnel is needed to rotate the low pressure rotor started by hand and turn by high pressure
The sub- manual rocking-turn high pressure rotor of rocker arm tool, and guarantee that rotor uniformly slowly rotates, inspection personnel and rotor rotate personnel
Working strength it is very big, so be easy to fatigue, especially engine rotor rotation person works' intensity is bigger, and operator
It is excessive it is tired out be easy to influence check quality, the engine runner inspection given brings very big difficulty, so using originally setting
Meter will liberate the both hands of engine rotor rotation personnel, liberate labour and productivity, reduce the labor intensity of operator
It checks on the quality and working efficiency with the runner for improving engine.
Utility model content
1. problem of the existing technology
The purpose of this utility model: propose that a kind of light-duty, quick, laborsaving, convenient aero-engine runner checks more function
It can rotary support.According to the working environment at scene and job requirement, proceeds from reality, make aero-engine runner inspection
The design of multifunctional belt favourable turn is made every effort to improve rotor laborious, time-consuming, inconvenient problem when engine runner checks, be subtracted
The burden of small flow channels inspection personnel, to improve the labor intensity that worker was checked on the quality and reduced to engine runner.To liberate work
People labour liberates the productive forces, and develops raw power.
2. technical solution
To achieve the goals above, the technical solution of the utility model is: a kind of aero-engine runner inspection is multi-functional
Band favourable turn, including tripod, fixed bandage, battery, driving motor, triple reduction gear and worm type of reduction gearing and controller；
The tripod includes supporting leg and upright bar, and the upright bar is telescopic rod, and three supporting legs are circumferentially uniform along the upright bar
Arrangement；The fixed bandage is arranged in the supporting leg bottom, and the battery is mounted in the upright bar, the driving motor setting
Portion on the battery, and be electrically connected with the battery；The triple reduction gear is arranged on the driving motor top, and
The driving motor output end is connect with the triple reduction gear input terminal；The worm type of reduction gearing is arranged in the three-level
Retarder top, and the triple reduction gear output end is connect with the worm type of reduction gearing input terminal, the controller
It is electrically connected with the battery and driving motor.
Above-mentioned aero-engine runner checks multifunctional belt favourable turn, wherein the upright bar is to be made of three telescopic joints
Three-level telescopic rod, and the two neighboring telescopic joint junction is provided with adjusting knob.
Above-mentioned aero-engine runner checks multifunctional belt favourable turn, wherein between the driving motor and the upright bar
It is provided with universal regulator.
Above-mentioned aero-engine runner checks multifunctional belt favourable turn, wherein the triple reduction gear includes first double-deck
Gear, the second double-layer gear and output gear；The gear wheel of first double-layer gear is connect with driving motor output shaft, and first
The pinion gear of double-layer gear is connect with the gear wheel of the second double-layer gear, the pinion gear and the output of second double-layer gear
Gear connection, the output gear are connect with the worm type of reduction gearing.
Above-mentioned aero-engine runner checks multifunctional belt favourable turn, wherein the first double-layer gear, the second double-layer gear and
Output gear is roller gear.
Above-mentioned aero-engine runner checks multifunctional belt favourable turn, wherein the gear wheel of first double-layer gear and
Pinion gear gear ratio is 20:47.
Above-mentioned aero-engine runner checks multifunctional belt favourable turn, wherein the gear wheel of second double-layer gear and
Pinion gear gear ratio is 12:59.
Above-mentioned aero-engine runner checks multifunctional belt favourable turn, wherein further includes feedback turbine and feedback worm screw, institute
It states feedback turbine setting to connect in the triple reduction gear bottom surface, and with the output gear, the feedback worm screw input terminal
It is connect with the feedback turbine, input terminal is connect with the controller.
Above-mentioned aero-engine runner checks multifunctional belt favourable turn, wherein is arranged between the supporting leg and the upright bar
There is floor, and the floor is hinged respectively at the supporting leg and upright bar.
Above-mentioned aero-engine runner checks multifunctional belt favourable turn, wherein further includes sound equipment, the sound equipment is arranged in institute
It states on upright bar peripheral wall, and is electrically connected with the battery and controller.
3. beneficial effect
In conclusion the utility model has the beneficial effects that:
(1) band favourable turn provides power using motor, by speed reducer deceleration torque increase to suitable revolving speed and torque, thus
The high pressure rotor rotation for driving engine, is not only able to the labour of liberation worker, but also is able to pass through the controller control and turns
Sub- positive and negative rotation and stop and speed regulation, feedback angle of rotor angle and overload protection；
(2) band favourable turn is equipped with sound equipment, improves the work ethos state of worker by playing music, alleviates work fatigue；
(3) the light-weight, Portable belt of band favourable turn, easy to operate, can preferably solve the practical problem of work on the spot.
Detailed description of the invention
Fig. 1 is the front view that the utility model aero-engine runner checks multifunctional belt favourable turn.
Fig. 2 is the side view that the utility model aero-engine runner checks multifunctional belt favourable turn.
Fig. 3 is the cross-sectional view that the utility model aero-engine runner checks multifunctional belt favourable turn A-A.
Specific embodiment
The embodiments of the present invention that the following is further explained with reference to the attached drawings.
It refers to shown in attached drawing 1 and attached drawing 3, a kind of aero-engine runner inspection multifunctional belt favourable turn, including tripod
1, fixed bandage 2, battery 3, driving motor 4, triple reduction gear 5 and worm type of reduction gearing 6 and controller 7；The tripod 1
Including supporting leg 101 and upright bar 102, the upright bar 102 is telescopic rod, and three supporting legs 101 are circumferential along the upright bar 102
It is evenly arranged；The fixed bandage 2 is arranged in 101 bottom of supporting leg, and the battery 3 is mounted in the upright bar 102, institute
The setting of driving motor 4 is stated to be electrically connected on 3 top of battery, and with the battery 3；The triple reduction gear 5 is arranged in institute
4 top of driving motor is stated, and 4 output end of the driving motor is connect with 5 input terminal of triple reduction gear；The worm gear snail
Bar retarder 6 is arranged on 5 top of triple reduction gear, and 5 output end of the triple reduction gear subtracts with the worm and gear
Fast 6 input terminal of device connection, the controller 7 are electrically connected with the battery 3 and driving motor 4.
The upright bar 102 is the three-level telescopic rod being made of three telescopic joints 103, and the two neighboring telescopic joint
103 junctions are provided with adjusting knob 8, and by changing the length of the upright bar 102, can expand band favourable turn uses model
It encloses.
Universal regulator 9 is provided between the driving motor 4 and the upright bar 102, the universal regulator 9 allows institute
State between driving motor 4 and upright bar 102 that there are certain angular deviations.
The triple reduction gear 5 includes the first double-layer gear 501, the second double-layer gear 502 and output gear 503；It is described
The gear wheel of first double-layer gear 501 and driving motor 4 export axis connection, the pinion gear of the first double-layer gear 501 with second pair
The gear wheel connection of layer gear 502, the pinion gear of second double-layer gear 502 is connect with the output gear 503, described defeated
Gear 503 is connect with the worm type of reduction gearing 6 out.
First double-layer gear 501, the second double-layer gear 502 and output gear 503 are roller gear, and it is tired to be both able to satisfy contact
Labor intensity and bending fatigue strength, but it is economical convenient for design and manufacture.
The gear wheel and pinion gear gear ratio of first double-layer gear 501 are 20:47, have both met face fatigue
Intensity and compact-sized requirement, and meet the criterion of economy and easy processing.
The gear wheel and pinion gear gear ratio of second double-layer gear 502 are 12:59, have both met face fatigue
Intensity and compact-sized requirement, and meet the criterion of economy and easy processing.
It further include feedback turbine 10 and feedback worm screw 11, the feedback turbine 10 is arranged in 5 bottom surface of triple reduction gear,
And it is connect with the output gear 503,11 input terminal of feedback worm screw is connect with the feedback turbine 10, input terminal and institute
The connection of controller 7 is stated, by the feedback turbine 10 and feedback worm screw 11, corner to be made a connection can be fed back to the control
Device 7, to realize the accurate and Real-time Feedback of corner.
Floor 12 is provided between the supporting leg 101 and the upright bar 102, and the floor 12 is respectively at the branch
Leg 101 and upright bar 102 are hinged, are capable of fixing the angle between the supporting leg 101 and upright bar 102 by the floor 12.
Further include sound equipment 13, the sound equipment 13 is arranged on 102 peripheral wall of upright bar, and with the battery 3 and control
Device 7 is electrically connected, and the sound equipment is conducive to improve work quality, relieves fatigue, and improves work ethos state.
Application method:
When the battery 3 with favourable turn is closed, the driving motor 4 converts electrical energy into mechanical energy and generates torque, leads to
It crosses drive three-level speed reducer 5 described in 4 input shaft of driving motor to rotate, 5 output shaft of three-level speed reducer and the worm gear
Worm reducer 6 connects, and rotates the worm type of reduction gearing 6, and the worm screw turbine wheel shaft is connected by spline and square joint
It connects, the high pressure rotor of aero-engine is driven to rotate.
Above-described is only the preferred embodiment of the utility model, is not intended to limit the patent model of the utility model
It encloses, any equivalent structural transformation made using the contents of the description of this utility model, directly or indirectly uses and be attached to other
The technical field of Related product, is also included in the patent protection scope of the utility model.
Claims (10)
1. a kind of aero-engine runner checks multifunctional belt favourable turn, it is characterised in that: including tripod (1), fixed bandage
(2), battery (3), driving motor (4), triple reduction gear (5) and worm type of reduction gearing (6) and controller (7)；Three foot
Frame (1) includes supporting leg (101) and upright bar (102), and the upright bar (102) is telescopic rod, and three supporting legs (101) are along institute
Upright bar (102) is stated to be arranged circumferentially；Fixed bandage (2) setting is in the supporting leg (101) bottom, battery (3) peace
In the upright bar (102), the driving motor (4) is arranged on the battery (3) top, and electric with the battery (3)
Connection；The triple reduction gear (5) is arranged on the driving motor (4) top, and the driving motor (4) output end and institute
State the connection of triple reduction gear (5) input terminal；The worm type of reduction gearing (6) is arranged on the triple reduction gear (5) top, and
And triple reduction gear (5) output end is connect with the worm type of reduction gearing (6) input terminal, the controller (7) and institute
State battery (3) and driving motor (4) electrical connection.
2. a kind of aero-engine runner according to claim 1 checks multifunctional belt favourable turn, it is characterised in that: described vertical
Bar (102) is the three-level telescopic rod being made of three telescopic joints (103), and the two neighboring telescopic joint (103) junction
It is provided with adjusting knob (8).
3. a kind of aero-engine runner according to claim 1 checks multifunctional belt favourable turn, it is characterised in that: the drive
Universal regulator (9) are provided between dynamic motor (4) and the upright bar (102).
4. a kind of aero-engine runner according to claim 1 checks multifunctional belt favourable turn, it is characterised in that: described three
Grade retarder (5) includes the first double-layer gear (501), the second double-layer gear (502) and output gear (503)；Described first pair
Layer gear (501) gear wheel and driving motor (4) export axis connection, the pinion gear of the first double-layer gear (501) with second pair
The gear wheel connection of layer gear (502), the pinion gear of second double-layer gear (502) are connect with the output gear (503),
The output gear (503) connect with the worm type of reduction gearing (6).
5. a kind of aero-engine runner according to claim 4 checks multifunctional belt favourable turn, it is characterised in that: first pair
Layer gear (501), the second double-layer gear (502) and output gear (503) are roller gear.
6. a kind of aero-engine runner according to claim 4 checks multifunctional belt favourable turn, it is characterised in that: described the
The gear wheel and pinion gear gear ratio of pair of lamina gear (501) are 20:47.
7. a kind of aero-engine runner according to claim 4 checks multifunctional belt favourable turn, it is characterised in that: described the
The gear wheel and pinion gear gear ratio of two double-layer gears (502) are 12:59.
8. a kind of aero-engine runner according to claim 4 checks multifunctional belt favourable turn, it is characterised in that: further include
Turbine (10) and feedback worm screw (11) are fed back, the feedback turbine (10) is arranged in the triple reduction gear (5) bottom surface, and with
Output gear (503) connection, feedback worm screw (11) input terminal are connect with the feedback turbine (10), input terminal and institute
State controller (7) connection.
9. a kind of aero-engine runner according to claim 1 checks multifunctional belt favourable turn, it is characterised in that: the branch
It is provided between leg (101) and the upright bar (102) floor (12), and the floor (12) is respectively at the supporting leg (101)
It is hinged with upright bar (102).
10. a kind of aero-engine runner according to claim 1 checks multifunctional belt favourable turn, it is characterised in that: also wrap
Include sound equipment (13), the sound equipment (13) is arranged on the upright bar (102) peripheral wall, and with the battery (3) and controller (7)
Electrical connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821847871.7U CN208984345U (en) | 2018-11-11 | 2018-11-11 | A kind of aero-engine runner inspection multifunctional belt favourable turn |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821847871.7U CN208984345U (en) | 2018-11-11 | 2018-11-11 | A kind of aero-engine runner inspection multifunctional belt favourable turn |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208984345U true CN208984345U (en) | 2019-06-14 |
Family
ID=66790743
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821847871.7U Expired - Fee Related CN208984345U (en) | 2018-11-11 | 2018-11-11 | A kind of aero-engine runner inspection multifunctional belt favourable turn |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208984345U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109141895A (en) * | 2018-11-11 | 2019-01-04 | 陈铭通 | A kind of aero-engine runner inspection multifunctional belt favourable turn |
-
2018
- 2018-11-11 CN CN201821847871.7U patent/CN208984345U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109141895A (en) * | 2018-11-11 | 2019-01-04 | 陈铭通 | A kind of aero-engine runner inspection multifunctional belt favourable turn |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190614 Termination date: 20191111 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |