CN204642165U - Miniature self-service mechanomotive force size digital test compound table - Google Patents
Miniature self-service mechanomotive force size digital test compound table Download PDFInfo
- Publication number
- CN204642165U CN204642165U CN201520350265.4U CN201520350265U CN204642165U CN 204642165 U CN204642165 U CN 204642165U CN 201520350265 U CN201520350265 U CN 201520350265U CN 204642165 U CN204642165 U CN 204642165U
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- landing platform
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- unmanned plane
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Abstract
The utility model discloses miniature self-service mechanomotive force size digital test compound table, comprise fixed way and unmanned plane, it is characterized in that: described fixed way is provided with landing platform and vertical fixed link, vertical fixed link one end is vertically mounted on fixed way, the other end is installed above-mentioned landing platform, unmanned plane is placed on landing platform upper surface, this landing platform is placed with draw piece device and the sensor being connected unmanned plane, vertical fixed link is provided with the survey meter for testing digital push-pull effort, this survey meter is fixed on vertical fixed link, and draw piece device is through above-mentioned landing platform, its one end is connected with survey meter upper end, the other end is connected with sensor.The miniature self-service mechanomotive force size digital test compound table that the utility model obtains, has structure simple, measures intuitive and convenient and by digitized display, the little accuracy rate of measured error is higher.
Description
Technical field
The utility model relates to a kind of mechanical measuring device, particularly miniature self-service mechanomotive force size digital test compound table.
Background technology
Robot airplane is called for short " unmanned plane ", is the not manned aircraft utilizing radio robot to handle with the process controller provided for oneself.Without driving compartment on machine, but the equipment such as autopilot, process controller is installed.On ground, naval vessels or machine tool command and control station personnel by equipment such as radars, it is followed the tracks of, locates, remote control, remote measurement and digital communication.Can take off as conventional airplane under radio telecommand or launch with booster rocket, also can be taken to by machine tool and throw in flight in the air.During recovery, the available mode automatic Landing the same with conventional airplane landing mission, also reclaims by remote control parachute or block, can Reusability repeatedly, be widely used in aerial reconnaissance, supervision, communication, antisubmarine, electro countermeasure etc.
Driving engine is the power resources of unmanned plane, and therefore the quality of engine quality is directly connected to the quality of unmanned plane, and this tests driving engine, to reach requirement before installation driving engine with regard to needs.
Utility model content
The purpose of this utility model be in order to solve above-mentioned the deficiencies in the prior art provide a kind of structure simple, measure miniature self-service mechanomotive force size digital test compound table accurately.
To achieve these goals, miniature self-service mechanomotive force size digital test compound table designed by the utility model, comprise fixed way and unmanned plane, it is characterized in that: described fixed way is provided with landing platform and vertical fixed link, vertical fixed link one end is vertically mounted on fixed way, the other end is installed above-mentioned landing platform, unmanned plane is placed on landing platform upper surface, this landing platform is placed with draw piece device and the electronics debugger being connected unmanned plane, vertical fixed link is provided with the survey meter for testing digital push-pull effort, this survey meter is fixed on vertical fixed link, and draw piece device is through above-mentioned landing platform, its one end is connected with survey meter upper end, the other end is connected with unmanned plane.
Preferably, described fixed way is also provided with the mechanism for testing of the pulling force for measuring horizontality, this mechanism for testing comprises sliding track mechanism, digital measuring apparatus and for measured driving engine, sliding track mechanism is provided with and can makees along it measurement driving engine slidably reciprocated, digital measuring apparatus is fixedly connected with sliding track mechanism.
Preferably, described driving engine is including but not limited to turbine engine, duct driving engine, genemotor and oily power engine.
Preferably, described engine rear end portion is also connected with electronic governor.
The miniature self-service mechanomotive force size digital test compound table that the utility model obtains, has following characteristics:
1, being provided with can landing platform under plumbness, can be used for testing power size and the Maximum Loading Capacity of vertical lift unmanned plane, test, computer immediately monitoring data, be convenient to analyze in conjunction with digital push-pull effort measuring instrument;
2, this fixed way also has the size of the horizontal push-and-pull strength can testing turbine engine, duct driving engine, genemotor and oily power engine, by computer immediately monitoring data, then data analysis is contrasted;
In sum its to have structure simple, measure intuitive and convenient and by digitized display, the little accuracy rate of measured error is higher.
Accompanying drawing explanation
Fig. 1 is the structural representation of miniature self-service mechanomotive force size digital test compound table.
In figure: fixed way 1, unmanned plane 2, survey meter 3, vertically fixed link 4, landing platform 5, sensor 6, draw piece device 7, digital measuring apparatus 10, driving engine 11, sliding track mechanism 12.
Detailed description of the invention
Below in conjunction with drawings and Examples, the utility model is further illustrated.
Embodiment:
As shown in Figure 1, the miniature self-service mechanomotive force size digital test compound table that the utility model provides, comprise fixed way 1 and unmanned plane 2, described fixed way 1 is provided with landing platform 5 and vertical fixed link 4, vertical fixed link 4 one end is vertically mounted on fixed way 1, the other end is installed above-mentioned landing platform 5, unmanned plane 2 is placed on landing platform 5 upper surface, this landing platform 5 is placed with draw piece device 7 and the electronic governor 6 being connected unmanned plane, electronic governor 6 can to adjustment friction speed, be convenient to test different power sizes, vertical fixed link 4 is provided with the survey meter 3 for testing digital push-pull effort, this survey meter 3 is fixed on vertical fixed link 4, and draw piece device 7 is through above-mentioned landing platform 5, namely through hole is had at landing platform vertical component effect, above-mentioned draw piece device is had to pass, draw piece device 7 comprises stay cord, its one end is connected with survey meter 3 upper end, the other end is connected with unmanned plane 2.Being provided with can landing platform 5 under plumbness, can be used for testing power size and the Maximum Loading Capacity of vertical lift unmanned plane 2, test, computer immediately monitoring data, be convenient to analyze in conjunction with digital push-pull effort measuring instrument.
Further, described fixed way 1 is also provided with the mechanism for testing of the pulling force for measuring horizontality, this mechanism for testing comprises sliding track mechanism 12, digital measuring apparatus 10 and for measured driving engine 11, described driving engine 11 is including but not limited to turbine engine, duct driving engine, genemotor and oily power engine, sliding track mechanism 12 is provided with and can makees along it measurement driving engine slidably reciprocated, digital measuring apparatus 10 is fixedly connected with sliding track mechanism 12.This fixed way has the size of the horizontal push-and-pull strength can testing turbine engine, duct driving engine, genemotor and oily power engine, by computer immediately monitoring data, then data analysis is contrasted; Described engine rear end portion is also connected with electronic governor 13, for controlling the pulling force of the driving engine under friction speed.
Miniature self-service mechanomotive force size digital test compound table obtained above is described further: the power size of test vertical lift unmanned plane and Maximum Loading Capacity, it first starts unmanned plane by its work, enter measuring state, owing to having installed survey meter, its power utilizing driving engine to produce is transmitted by draw piece device, survey meter can show corresponding data.
The size of horizontal push-and-pull strength, fire an engine enters test phase, under engine action can on sliding track mechanism before and after linear slide, be used for test pulling force, when driving engine is counter starch time test rear end pressure to test thrust.
For the utility model person of an ordinary skill in the technical field; without departing from the concept of the premise utility; its framework form can be flexible and changeable; just make some simple deduction or replace, all should be considered as belonging to the scope of patent protection that claims of being submitted to by the utility model are determined.
Claims (4)
1. a miniature self-service mechanomotive force size digital test compound table, comprise fixed way and unmanned plane, it is characterized in that: described fixed way is provided with landing platform and vertical fixed link, vertical fixed link one end is vertically mounted on fixed way, the other end is installed above-mentioned landing platform, unmanned plane is placed on landing platform upper surface, this landing platform is placed with draw piece device and the electronics debugger being connected unmanned plane, vertical fixed link is provided with the survey meter for testing digital push-pull effort with sensor, this survey meter is fixed on vertical fixed link, and draw piece device is through above-mentioned landing platform, its one end is connected with survey meter upper end, the other end is connected with unmanned plane.
2. miniature self-service mechanomotive force size digital test compound table according to claim 1, it is characterized in that: the mechanism for testing described fixed way being also provided with the pulling force for measuring horizontality, this mechanism for testing comprises sliding track mechanism, digital measuring apparatus and for measured driving engine, sliding track mechanism is provided with and can makees along it measurement driving engine slidably reciprocated, digital measuring apparatus is fixedly connected with sliding track mechanism.
3. miniature self-service mechanomotive force size digital test compound table according to claim 2, is characterized in that: described driving engine is including but not limited to turbine engine, duct driving engine, genemotor and oily power engine.
4. the miniature self-service mechanomotive force size digital test compound table according to Claims 2 or 3, is characterized in that: described engine rear end portion is also connected with electronic governor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520350265.4U CN204642165U (en) | 2015-05-28 | 2015-05-28 | Miniature self-service mechanomotive force size digital test compound table |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520350265.4U CN204642165U (en) | 2015-05-28 | 2015-05-28 | Miniature self-service mechanomotive force size digital test compound table |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204642165U true CN204642165U (en) | 2015-09-16 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520350265.4U Expired - Fee Related CN204642165U (en) | 2015-05-28 | 2015-05-28 | Miniature self-service mechanomotive force size digital test compound table |
Country Status (1)
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| CN (1) | CN204642165U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106286014A (en) * | 2016-11-14 | 2017-01-04 | 冯增瑞 | A kind of ducted fan Engine Block Test device |
| CN109795715A (en) * | 2019-02-16 | 2019-05-24 | 天津大学 | A kind of universal aircraft Three Degree Of Freedom and single-degree-of-freedom posture comprehensive debugging platform |
| CN110116821A (en) * | 2019-05-24 | 2019-08-13 | 农业农村部南京农业机械化研究所 | A kind of test equipment and method for quickly testing electronic multi-rotor unmanned aerial vehicle maximum take-off weight |
-
2015
- 2015-05-28 CN CN201520350265.4U patent/CN204642165U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106286014A (en) * | 2016-11-14 | 2017-01-04 | 冯增瑞 | A kind of ducted fan Engine Block Test device |
| CN106286014B (en) * | 2016-11-14 | 2017-12-01 | 王梦梦 | A kind of ducted fan Engine Block Test device |
| CN109795715A (en) * | 2019-02-16 | 2019-05-24 | 天津大学 | A kind of universal aircraft Three Degree Of Freedom and single-degree-of-freedom posture comprehensive debugging platform |
| CN109795715B (en) * | 2019-02-16 | 2023-10-13 | 天津大学 | Three-degree-of-freedom and single-degree-of-freedom gesture comprehensive debugging platform of general aircraft |
| CN110116821A (en) * | 2019-05-24 | 2019-08-13 | 农业农村部南京农业机械化研究所 | A kind of test equipment and method for quickly testing electronic multi-rotor unmanned aerial vehicle maximum take-off weight |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150916 Termination date: 20200528 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |