CN207516037U - A kind of propeller parameter automatic testing device - Google Patents
A kind of propeller parameter automatic testing device Download PDFInfo
- Publication number
- CN207516037U CN207516037U CN201721431208.4U CN201721431208U CN207516037U CN 207516037 U CN207516037 U CN 207516037U CN 201721431208 U CN201721431208 U CN 201721431208U CN 207516037 U CN207516037 U CN 207516037U
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- shaft coupling
- frame
- suction box
- power motor
- load
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Abstract
The utility model discloses a kind of propeller parameter automatic testing device, structure includes：Fixed frame, mounting bracket, power motor, test device, gear frame, heat radiation rack, suction box, drive link, rotation slurry, shaft coupling, axle position frame, testing gears, sensor, rotor, load gear bar, load frame, load gear bar is located at the inside of power motor and is matched with power motor, shaft coupling is located at the lateral surface of load gear bar and coordinates with the activity of load gear bar, axle position frame is located at the right side of shaft coupling and is fixedly connected with shaft coupling, sensor is located at the right of shaft coupling and is connected with shaft coupling, a kind of propeller parameter automatic testing device of the utility model, after upper test device, propeller, which can be reached, can automatically be tested the parameter of the motor of active force when being worked, so as to the service condition of motor, and cause the more intelligentized purpose of device.
Description
Technical field
The utility model is a kind of propeller parameter automatic testing device, belongs to propeller field.
Background technology
Boost motor is a pair of of the solid-propellant booster rocket for providing thrust in two minutes before launching for space shuttle, peace
Mounted in external tank both sides.
Screw propeller abbreviation propeller.Propeller is mounted on the cardan shaft below ships and light boats stern waterline, by host
Cardan shaft is driven to rotate together, water from the suction plane of blade is sucked, from the discharge of discharge face, utilizes the reaction force propelling ship of water
Ship advances.Propeller is divided into fixed pitch propeller and adjustable pitch propeller.
Prior art discloses application No. is：201520600575.7 a kind of releasable diver both hands, be easy to latent
Water person's underwater operation, the underwater scooter for reducing diver's fatigue and life danger, including two inside pushing away for waterproof construction
Into device babinet, battery and the motor being connect with battery are separately installed in the propeller babinet, in the propeller babinet
Interior rear end is provided with the propeller being connect with motor output shaft, close to the space in outside is hollow grid in the propeller babinet
Structure, arc groove is equipped in the inboard of the propeller babinet, is located on the propeller babinet fixed at arc groove notch
Have adhesive band, be also equipped in the propeller babinet battery low-electricity quantity warning device being connect respectively with battery and positioning with
Track device, but the propeller of the prior art can not automatically be tested the parameter of the motor of active force when being worked, from
And can not motor service condition, and can not so that device is more intelligent.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of propeller automatically testing parameters dress
It puts, the parameter of the motor of active force can not automatically be tested with solving propeller when being worked, thus can not electricity
The service condition of machine, and can not cause the more intelligentized problem of device.
To achieve these goals, the utility model is to realize by the following technical solutions：A kind of propeller parameter
Automatic testing equipment, structure include：Fixed frame, mounting bracket, power motor, test device, gear frame, heat radiation rack, suction box,
Drive link, rotation slurry, the fixed frame are located at the upper surface of suction box and are mechanically connected with suction box, and the mounting bracket is located at
The top of fixed frame and be integrated with fixed frame, the power motor be fixedly mounted on the upper surface of mounting bracket and
The inside of Embedded test device is matched therewith, and the test device is located at the upper surface of gear frame and connects with gear frame machinery
It connects, the gear frame is located at the right side of suction box and is connected with suction box, and the heat radiation rack is located at the outside of suction box
It face and is fixedly connected with suction box.
The test device is equipped with shaft coupling, axle position frame, testing gears, sensor, rotor, load gear bar, load frame,
The load gear bar is located at the inside of power motor and is matched with power motor, and the shaft coupling is located at load gear bar
Lateral surface and coordinate with the activity of load gear bar, the axle position frame is located at the right side of shaft coupling and fixed with shaft coupling
Connection, the sensor are located at the right of shaft coupling and are connected with shaft coupling, and the testing gears are located at load gear bar
Lateral surface and be integrated with load gear bar, the rotor be set on testing gears inside, the load frame position
It is connected in the right side of shaft coupling and with shaft coupling.
Further, the drive link is located at the inside of suction box and is meshed with the gear in suction box.
Further, the power motor be fixedly mounted on mounting bracket upper surface and the inside of Embedded test device with
It is gap-matched.
Further, the rotation slurry is integrated positioned at the left side of drive link and with drive link.
Further, the load gear bar is located at the inside of power motor and with power motor using cooperation.
Further, different shaft coupling there are three being set in the test device.
Further, the test device is made of metal material.
Further, the rotation slurry is made of metal material.
Advantageous effect
A kind of propeller parameter automatic testing device of the utility model, after upper test device, can reach propulsion
Device can automatically be tested the parameter of the motor of active force when being worked, so as to the service condition of motor,
And cause the more intelligentized purpose of device.
Description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon：
Fig. 1 is a kind of structure diagram of propeller parameter automatic testing device of the utility model.
Fig. 2 is the structure diagram of the utility model test device.
In figure：Fixed frame -1, mounting bracket -2, power motor -3, test device -4, gear frame -5, heat radiation rack -6, water suction
Case -7, drive link -8, rotation slurry -9, shaft coupling -401, axle position frame -402, testing gears -403, sensor -404, rotor -
405th, load gear bar -406, load frame -407.
Specific embodiment
To be easy to understand technical means, creative features, achievable purpose and effectiveness of the utility model, below
With reference to specific embodiment, the utility model is expanded on further.
It please refers to Fig.1, Fig. 2, the utility model provides a kind of propeller parameter automatic testing device technical solution：Its structure
Including：Fixed frame 1, mounting bracket 2, power motor 3, test device 4, gear frame 5, heat radiation rack 6, suction box 7, drive link 8, rotation
Slurry 9, the fixed frame 1 is located at the upper surface of suction box 7 and is mechanically connected with suction box 7, and the mounting bracket 2 is located at fixed frame
It 1 top and is integrated with fixed frame 1, the power motor 3 is fixedly mounted on the upper surface of mounting bracket 2 and embedding
The inside for entering test device 4 is matched therewith, the test device 4 be located at the upper surface of gear frame 5 and with the machinery of gear frame 5
Connection, the gear frame 5 are located at the right side of suction box 7 and are connected with suction box 7, and the heat radiation rack 6 is located at suction box 7
Lateral surface and be fixedly connected with suction box 7.
The test device 4 is equipped with shaft coupling 401, axle position frame 402, testing gears 403, sensor 404, rotor 405, bears
Rack 406, load frame 407 are carried, the load gear bar 406 is located at the inside of power motor 3 and matches with power motor 3
It closes, the shaft coupling 401 is located at the lateral surface of load gear bar 406 and coordinates with 406 activity of load gear bar, the axle position
Frame 402 is located at the right side of shaft coupling 401 and is fixedly connected with shaft coupling 401, and the sensor 404 is located at shaft coupling 401
Right and be connected with shaft coupling 401, the testing gears 403 be located at the lateral surface of load gear bar 406 and with it is negative
It carries rack 406 to be integrated, the rotor 405 is set on the inside of testing gears 403, and the load frame 407 is located at connection
The right side of axis device 401 and be connected with shaft coupling 401, the drive link 8 be located at the inside of suction box 7 and with suction box 7
Interior gear is meshed, and the power motor 3 is fixedly mounted on the upper surface of mounting bracket 2 and the inside of Embedded test device 4
It is gap-matched with it, the rotation slurry 9 is located at the left side of drive link 8 and is integrated with drive link 8, described
Load gear bar 406 is located at the inside of power motor 3 and with power motor 3 using coordinating, and the test device 4 is equipped with three
A different shaft coupling 401, the test device 4 are made of metal material, and the rotation slurry 9 is made of metal material.
Test device 4 described in the utility model is referred to using sensor come the rotation of the rotor inside testing gears
Rate, so as to detect the performance of motor.
It is carrying out in use, first so that power motor 3 operationalizes, the load gear bar 406 inside power motor 3 carries out
Rotation, and the rotation for the testing gears 403 being located on its surface is driven, while the rotor rotation inside testing gears 403, it passes
Sensor 404 tests the rate of the rotation of rotor, and shows, while auxiliary material rack 406 is to underdrive so that suction box
7 sucking flows, and using the 9 rotation draining of rotation slurry, complete to push, can thus reach propeller energy when being worked
It is enough automatically to be tested the parameter of the motor of active force, so as to the service condition of motor, and cause device more
Intelligentized purpose.
The utility model, which solves propeller, can not automatically be surveyed the parameter of the motor of active force when being worked
Examination, so as to can not motor service condition, and can not cause the more intelligentized problem of device, the utility model passes through upper
Being combined with each other for component is stated, can reach propeller can carry out the parameter of the motor of active force automatically when being worked
Test so as to the service condition of motor, and causes the more intelligentized purpose of device, described in detail below:
The load gear bar 406 is located at the inside of power motor 3 and is matched with power motor 3, the shaft coupling
401 are located at the lateral surface of load gear bar 406 and coordinate with 406 activity of load gear bar, and the axle position frame 402 is located at shaft coupling
The right side of device 401 and be fixedly connected with shaft coupling 401, the sensor 404 be located at the right of shaft coupling 401 and with connection
Axis device 401 is connected, and the testing gears 403 are located at the lateral surface of load gear bar 406 and are one with load gear bar 406
Body structure, the rotor 405 are set on the inside of testing gears 403, and the load frame 407 is located at the right side of shaft coupling 401 simultaneously
And it is connected with shaft coupling 401.
The basic principle of the utility model and main feature and the advantages of the utility model has been shown and described above, for
For those skilled in the art, it is clear that the utility model is not limited to the details of above-mentioned exemplary embodiment, and without departing substantially from this
In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent requirements of the claims
All changes are embraced therein.Any reference numeral in claim should not be considered as to the involved right of limitation
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in each embodiment can also be properly combined, forms those skilled in the art
The other embodiment being appreciated that.
Claims (6)
1. a kind of propeller parameter automatic testing device, structure include：Fixed frame（1）, mounting bracket（2）, power motor（3）、
Test device（4）, gear frame（5）, heat radiation rack（6）, suction box（7）, drive link（8）, rotation slurry（9）, the fixed frame（1）Position
In suction box（7）Upper surface and and suction box（7）Mechanical connection, the mounting bracket（2）Positioned at fixed frame（1）Top simultaneously
And and fixed frame（1）It is integrated, the power motor（3）It is fixedly mounted on mounting bracket（2）Upper surface and insertion
Test device（4）Inside be matched therewith, the test device（4）Positioned at gear frame（5）Upper surface and and gear frame
（5）Mechanical connection, the gear frame（5）Positioned at suction box（7）Right side and and suction box（7）It is connected, the heat dissipation
Frame（6）Positioned at suction box（7）Lateral surface and and suction box（7）It is fixedly connected, it is characterised in that：
The test device（4）Equipped with shaft coupling（401）, axle position frame（402）, testing gears（403）, sensor（404）, rotor
（405）, load gear bar（406）, load frame（407）, the load gear bar（406）Positioned at power motor（3）Inside simultaneously
And and power motor（3）It matches, the shaft coupling（401）Positioned at load gear bar（406）Lateral surface and with load tooth
Take turns bar（406）Activity cooperation, the axle position frame（402）Positioned at shaft coupling（401）Right side and and shaft coupling（401）It is fixed
Connection, the sensor（404）Positioned at shaft coupling（401）Right and and shaft coupling（401）It is connected, the testing gears
（403）Positioned at load gear bar（406）Lateral surface and with load gear bar（406）It is integrated, the rotor
（405）Set on testing gears（403）Inside, the load frame（407）Positioned at shaft coupling（401）Right side and and shaft coupling
（401）It is connected.
2. a kind of propeller parameter automatic testing device according to claim 1, it is characterised in that：The drive link（8）
Positioned at suction box（7）Inside and and suction box（7）Interior gear is meshed.
3. a kind of propeller parameter automatic testing device according to claim 1, it is characterised in that：The power motor
（3）It is fixedly mounted on mounting bracket（2）Upper surface and Embedded test device（4）Inside be gap-matched with it.
4. a kind of propeller parameter automatic testing device according to claim 1, it is characterised in that：The rotation slurry（9）
Positioned at drive link（8）Left side and and drive link（8）It is integrated.
5. a kind of propeller parameter automatic testing device according to claim 1, it is characterised in that：The load gear bar
（406）Positioned at power motor（3）Inside and and power motor（3）Using cooperation.
6. a kind of propeller parameter automatic testing device according to claim 1, it is characterised in that：The test device
（4）On set there are three different shaft couplings（401）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721431208.4U CN207516037U (en) | 2017-10-31 | 2017-10-31 | A kind of propeller parameter automatic testing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721431208.4U CN207516037U (en) | 2017-10-31 | 2017-10-31 | A kind of propeller parameter automatic testing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207516037U true CN207516037U (en) | 2018-06-19 |
Family
ID=62536654
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721431208.4U Active CN207516037U (en) | 2017-10-31 | 2017-10-31 | A kind of propeller parameter automatic testing device |
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| Country | Link |
|---|---|
| CN (1) | CN207516037U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107664582A (en) * | 2017-10-31 | 2018-02-06 | 天津昊野科技有限公司 | A kind of propeller parameter automatic testing device |
-
2017
- 2017-10-31 CN CN201721431208.4U patent/CN207516037U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107664582A (en) * | 2017-10-31 | 2018-02-06 | 天津昊野科技有限公司 | A kind of propeller parameter automatic testing device |
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