CN107630939A - The continuous component of gear coupling torque load multi-location maintenance - Google Patents
The continuous component of gear coupling torque load multi-location maintenance Download PDFInfo
- Publication number
- CN107630939A CN107630939A CN201610568918.5A CN201610568918A CN107630939A CN 107630939 A CN107630939 A CN 107630939A CN 201610568918 A CN201610568918 A CN 201610568918A CN 107630939 A CN107630939 A CN 107630939A
- Authority
- CN
- China
- Prior art keywords
- module
- induction module
- torsional forces
- gear coupling
- continuous component
- 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
Landscapes
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
The continuous component of gear coupling torque load multi-location maintenance, including a body (1), moment of torsion induction module (2), running induction module (3), load induction module (4), management module (5) are set on body (1), during operation, moment of torsion induction module (2) senses fuselage torsional forces numerical value, operate induction module (3) sensing fuselage function situation, load induction module (4) induction machine bears lotus, management module (5) processing integrated information；Limitation setting module (6) is set on moment of torsion induction module (2), sets the torsional forces numerical value of OK range；Multiple spot is set on running induction module (3), and with reference to module (7), torsional forces produces frequently position when setting is run；Reminding module (8) is set in management module (5), when sensing that torsional forces numerical value is excessive, sends prompting；By controlling load condition, torsional forces situation, avoid part from being damaged, safeguard body parts.
Description
Technical field
The present invention relates to a kind of gear coupling.
Background technology
Gear coupling is a kind of part for making driving shaft, driven shaft rotate, transmit torsional forces jointly, has buffering, subtracts
Shake, improve the advantages that shafting, some defects in gear coupling operation in terms of moment of torsion also be present, torsional forces is crossed conference and made
It is damaged into body parts.
The content of the invention
The purpose of the present invention, which is that, provides a kind of effective gear coupling torque load multi-location maintenance continuous component.
What the present invention was realized in.The continuous component of gear coupling torque load multi-location maintenance, including a body,
Moment of torsion induction module, running induction module, load induction module, management module be set on body, during operation, moment of torsion induction module
Sense fuselage torsional forces numerical value, running induction module sensing fuselage function situation, load induction module induction machine is born lotus, managed
Resume module integrated information.
The continuous component of gear coupling torque load multi-location maintenance, limitation setting module is set on moment of torsion induction module,
The torsional forces numerical value of OK range is set according to load quantity.
The continuous component of gear coupling torque load multi-location maintenance, multiple spot reference module is set on running induction module,
Torsional forces produces frequently position during setting operation.
The continuous component of gear coupling torque load multi-location maintenance, sets reminding module in management module, when sensing
When torsional forces numerical value is excessive, prompting is sent.
The continuous component of gear coupling torque load multi-location maintenance, reminding module send the mode of prompting for sound or
LED is shown.
The above-mentioned continuous component of gear coupling torque load multi-location maintenance, by controlling load condition, torsional forces situation, keeps away
Exempt from part to be damaged, safeguard body parts.
Brief description of the drawings
Accompanying drawing is the structural representation of the continuous component of gear coupling torque load multi-location maintenance.
Label is respectively in figure：1- bodies, 2- moments of torsion induction module, 3- runnings induction module, 4- loads induction module, 5-
Management module, 6- limitations setting module, 7- multiple spots are with reference to module, 8- reminding modules.
Embodiment
Embodiment：As shown in drawings.The continuous component of gear coupling torque load multi-location maintenance, including a body (1),
Moment of torsion induction module (2), running induction module (3), load induction module (4), management module (5), fortune are set on body (1)
During row, moment of torsion induction module (2) sensing fuselage torsional forces numerical value, running induction module (3) sensing fuselage function situation, load sense
Module (4) induction machine is answered to bear lotus, management module (5) processing integrated information.
The continuous component of gear coupling torque load multi-location maintenance, limitation setting mould is set on moment of torsion induction module (2)
Block (6), the torsional forces numerical value of OK range is set according to load quantity.
The continuous component of gear coupling torque load multi-location maintenance, multiple spot is set on running induction module (3) with reference to mould
Block (7), torsional forces produces frequently position when setting is run.
The continuous component of gear coupling torque load multi-location maintenance, reminding module (8) is set in management module (5), when
When sensing that torsional forces numerical value is excessive, prompting is sent.
The continuous component of gear coupling torque load multi-location maintenance, reminding module (8) send the mode of prompting for sound or
Person LED is shown.
The above-mentioned continuous component of gear coupling torque load multi-location maintenance, by controlling load condition, torsional forces situation, keeps away
Exempt from part to be damaged, safeguard body parts.
Claims (5)
1. the continuous component of gear coupling torque load multi-location maintenance, it is characterised in that including a body (1), in body (1)
Upper setting moment of torsion induction module (2), running induction module (3), load induction module (4), management module (5), during operation, moment of torsion
Induction module (2) senses fuselage torsional forces numerical value, running induction module (3) sensing fuselage function situation, load induction module (4)
Induction machine bears lotus, management module (5) processing integrated information.
2. the continuous component of gear coupling torque load multi-location maintenance according to claim 1, it is characterised in that in moment of torsion
Limitation setting module (6) is set on induction module (2), the torsional forces numerical value of OK range is set according to load quantity.
3. the continuous component of gear coupling torque load multi-location maintenance according to claim 1, it is characterised in that operating
Multiple spot is set on induction module (3), and with reference to module (7), torsional forces produces frequently position when setting is run.
4. the continuous component of gear coupling torque load multi-location maintenance according to claim 1, it is characterised in that managing
Reminding module (8) is set in module (5), when sensing that torsional forces numerical value is excessive, sends prompting.
5. the continuous component of gear coupling torque load multi-location maintenance according to claim 4, it is characterised in that prompting mould
The mode that block (8) sends prompting shows for sound or LED.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610568918.5A CN107630939A (en) | 2016-07-18 | 2016-07-18 | The continuous component of gear coupling torque load multi-location maintenance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610568918.5A CN107630939A (en) | 2016-07-18 | 2016-07-18 | The continuous component of gear coupling torque load multi-location maintenance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107630939A true CN107630939A (en) | 2018-01-26 |
Family
ID=61111683
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610568918.5A Pending CN107630939A (en) | 2016-07-18 | 2016-07-18 | The continuous component of gear coupling torque load multi-location maintenance |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107630939A (en) |
-
2016
- 2016-07-18 CN CN201610568918.5A patent/CN107630939A/en active Pending
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107630939A (en) | The continuous component of gear coupling torque load multi-location maintenance | |
| CN201344244Y (en) | Sectional type bull gear | |
| CN205204065U (en) | Screw conveyer's stand wear and tear device | |
| CN105645072A (en) | Automatically-controlled conveying belt | |
| CN205766199U (en) | A kind of overall upset feeding gas pawl | |
| EP1882632A3 (en) | Machine for producing groups of roll products. | |
| CN108061033A (en) | Prevent coaxial Corrective control module in hydraulic gear pump gap | |
| CN107290984A (en) | Pipeline-type emulsifying machine mechanical seal operates attending device | |
| CN107870007A (en) | A kind of gearbox drive twin shaft operation degree of balance accessory part | |
| CN108126967A (en) | Refuse ore reclaiming machine test run spatial load forecasting point position adjustment module | |
| CN102430695A (en) | Manufacture method of highly-novel round-link chain | |
| CN107796219A (en) | Bench vehicle type electrical resistance furnace running bottom plate purging servicing unit | |
| CN201389911Y (en) | Automatic turning device of stripe bricks | |
| CN204371910U (en) | A kind of hoist machine taper shaft | |
| CN105921405A (en) | Classifier helix lifting positioner based on operation status | |
| CN107218810A (en) | A kind of intermediate frequency furnace lining sintering work regulatory component | |
| CN206003754U (en) | A kind of silicon wafer conveying mechanism | |
| CN107304764A (en) | The cavity pressure deviation of gear pump or so two reduces module | |
| CN107892209A (en) | A kind of assembling machine pulling force control friction prevention module | |
| CN107839285A (en) | The four post hydraulic presses pressure unidirectionally controlled component of workpiece manipulation | |
| CN107934065A (en) | Cartoning sealing machine clip nail operation stroke deficiency activity adjustment module | |
| CN107838381A (en) | Shell core machine shooting cylinder operating position fixing aids in clamping controller | |
| CN108033225A (en) | Belt bucket elevator roller lateral deviation preventing mean | |
| CN107627022A (en) | Cold welding tower connects operation and connects section overload preventing mean | |
| CN107934259A (en) | Pneumatic vibrator is based on hopper material path workpiece coordination component |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180126 |
|
| WD01 | Invention patent application deemed withdrawn after publication |