CN104960673B - Suitable for the multi-functional expansible test platform of bionic flapping-wing microreactor technology - Google Patents
Suitable for the multi-functional expansible test platform of bionic flapping-wing microreactor technology Download PDFInfo
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- CN104960673B CN104960673B CN201510309989.9A CN201510309989A CN104960673B CN 104960673 B CN104960673 B CN 104960673B CN 201510309989 A CN201510309989 A CN 201510309989A CN 104960673 B CN104960673 B CN 104960673B
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Abstract
The present invention discloses a kind of multi-functional expansible test platform suitable for bionic flapping-wing microreactor technology, wherein：Microreactor technology track segment is connected with support member, and support member and microreactor technology track segment are located at surface, and sensor placing component is located at substrate lower section；Support member is fixed with the cross slide way with sliding block, substrate；Microreactor technology track segment is relatively fixed with the sliding block on the cross slide way with sliding block, and microreactor technology track segment is provided with hole for penetrating worm screw knob, and a steel wire is connected between the worm screw on same microreactor technology track segment, and steel wire is parallel to each other.All kinds of equipment related to flapping wing aircraft test are arranged on placing on sensor or around substrate below substrate.The present apparatus makes and easy to use, low cost, and can the measuring apparatus such as additional various sensors, even if there is new demand after, a small amount of increase need to be done on original basic platform, do not result in the waste for manufacturing new platform.
Description
Technical field
It is specifically a kind of each specifically designed for bionic flapping-wing microreactor technology the present invention relates to a kind of multifunctional testing platform
Plant the multi-functional expansible test platform of parameter measurement.
Background technology
As what the progress and people of science and technology were studied aircraft progressively gos deep into and to the continuous exploration of bionic field,
Nowadays the research of people has begun to march toward the bionical microreactor technology of flapping wing.Microreactor technology size is small, and all kinds of parameters are also all very
It is small, thus, corresponding supporting test platform is essential.
Not long due to studying this field time in the world at present, matched measuring table is quite few.Major part is ground
Mechanism is studied carefully when this kind of microreactor technology is studied, and always needs an individually designed test in addition flat when studying different performances every time
Platform.
In general, the price of a set of experiment test platform is from thousands of to tens of thousands of, if being designed for measurement performance
Multiple experiment porch, and wherein have the increase of many public parts and a small amount of New function, that will cause manpower with economically
Huge waste.
The content of the invention
It is each specifically designed for bionic flapping-wing microreactor technology it is an object of the invention to provide one kind for defect of the prior art
Plant the multi-functional expansible test platform of parameter measurement.Device making and easy to use, low cost, and can be additional
The measuring apparatus such as various sensors, even if there is new demand after, only need to do a small amount of increase i.e. on original basic platform
Can, do not result in the waste for manufacturing new platform.
The present invention is achieved by the following technical solutions：
A kind of multi-functional expansible test platform suitable for bionic flapping-wing microreactor technology, including：Substrate, support member,
Sensor placing component, the cross slide way with sliding block, microreactor technology track segment, worm screw knob and steel wire；Wherein：Micro- flight
Device track segment is connected with support member, and support member is connected with substrate, and substrate is connected with sensor placing component；Support member
With the top that microreactor technology track segment is located at substrate, sensor placing component is positioned at the lower section of substrate；Support member altogether by
Two kinds of part compositions, respectively one first component and two second components, the top of first component and the transverse direction with sliding block
Guide rail is fixed, and the side of left and right two is respectively fixed with a second component, and second component is fixed with substrate；Microreactor technology track segment and institute
The sliding block stated on the cross slide way with sliding block is relatively fixed, and microreactor technology track segment is provided with two holes for penetrating
Two worm screw knobs, are connected to a steel wire between two worm screw knobs on same microreactor technology track segment, steel wire hangs down
Directly in base plan direction, used as the guide rail of aircraft, mobile sliding block can adjust the position of steel wire.
Preferably, the platform further sets all kinds of equipment related to flapping wing aircraft test, and these equipment are set
On the sensor placing component or around the substrate.All kinds of equipment related to flapping-wing MAV test, refer to
The extra various kinds of sensors installed, these sensors are not directly mounted on substrate, but by One function part mistake
Cross, functional part one end install sensor, one end is arranged on substrate.
Preferably, the overall shape of described substrate is rectangle, and four edges all have projection, can be used to plug expansion
The module filled；It is horizontal and vertical on substrate to be provided with a through hole at a certain distance.
Preferably, described sensor placing component, its profile is the rectangle as substrate size, four edges and base
The four edges alignment of plate, keeps a distance between substrate；Many bar grooves are carved with sensor placing component, for using bolt spiral shell
Female install sensor, and can be slided along groove.
Preferably, the first component and second component of the support member and microreactor technology track segment, these three parts
All it is the template part of the two-dimensional shapes with uniform thickness, and three's thickness is identical.
Preferably, the first component of the support member, the width of the part of the part fixed lateral guide rail is led with laterally
Rail length is consistent, and the width that the part fixes the part of substrate is consistent with the length of substrate, position and substrate that the part is placed
Side long it is parallel, alignd with the broadside of substrate.
Preferably, the first component of the support member, the center of the thickness direction of the part and the distance of substrate center
The thickness of half, cross slide way equal to the part thickness, the half sum of microreactor technology track segment thickness；Support member
Two second components are located at the right and left of first component, and vertical with first component, the top edge of the two second components and
The top edge alignment of first component.
Preferably, the microreactor technology track segment places the side of steel wire with two quarter circular arcs, and steel wire is all
From a worm screw knob, by a circular arc, then by second circular arc, second worm screw knob is finally reached.
Preferably, the outer rim installing angle degree part of the substrate, the gyration part includes two disks and two
The individual base for supporting, disc centre has a circular hole for rotating, and disk border has row's small sircle hole, certain for rotating
It is fixed after angle；There are two bar grooves, size and two length dimensions of projection one of substrate edges of this two bar groove on disk
Cause, substrate can be embedded in disk.
Preferably, the quantity of the steel wire is identical with sliding block quantity, and the quantity of worm screw knob is the twice of sliding block quantity, and
The flat shape of two parts on sliding block is symmetrical on vertical plane.
Operation principle of the invention is：Cross slide way is fixed with substrate relative position, is fixed on the microreactor technology on sliding block
Track segment is installed with steel wire, and the position of steel wire can meet the demand of microreactor technology by the mobile adjustment of sliding block.Left and right two
Mutually close part respectively has two quarter circular arcs to individual second component, steel wire from a worm screw knob, by one
Circular arc, then by second circular arc, second worm screw knob is finally reached, by such a design, between two steel wires
Minimum range can be reached within 1 millimeter, to meet the demand of small size aircraft.The median plane of the thickness direction of first component
The half for being equal to first component thickness with the distance of substrate center adds the thickness plus microreactor technology track segment thickness of cross slide way
Half, can so make the guide rail of installation microreactor technology position be located at whole platform center, facilitate the measurement of data.Substrate
It is above horizontal and vertical to be equipped with a through hole at a certain distance, can as needed select suitable logical when other parts are installed
Hole is used as the position installed.Many bar grooves are carved with plate, can be selected properly according to the need for different sensors during install sensor
Groove, for using bolt and nut install sensor, and can be slided along groove.
Preferably, the Element Design of left and right two is symmetric shape.
Compared with prior art, the present invention has following beneficial effect：
It is of the invention compared with conventional flapping-wing MAV experiment porch, make and easy to use, low cost, and energy
The measuring apparatus such as enough additional various sensors, even if there is new demand after, only need to do a small amount of on original basic platform
Increase, do not result in the waste for manufacturing new platform.
Brief description of the drawings
The detailed description made to non-limiting example with reference to the following drawings by reading, further feature of the invention,
Objects and advantages will become more apparent upon：
Fig. 1 is the integrally-built isometric drawing of a preferred embodiment of the invention；
Fig. 2 is the integrally-built front view of a preferred embodiment of the invention；
Fig. 3 is the integrally-built top view of a preferred embodiment of the invention；
Fig. 4 is the top view of the substrate of a preferred embodiment of the invention；
Fig. 5 is the top view of the sensor placing component of a preferred embodiment of the invention；
In figure：Substrate 1, sensor placing component 2, first component 3, second component 6, cross slide way 10, sliding block 4 is micro- to fly
Row device track segment 5, the steel wire 8 as microreactor technology guide rail, worm screw knob 9, the gyration part 7 of expansion.
Specific embodiment
With reference to specific embodiment, the present invention is described in detail.Following examples will be helpful to the technology of this area
Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that to the ordinary skill of this area
For personnel, without departing from the inventive concept of the premise, various modifications and improvements can be made.These belong to the present invention
Protection domain.
As shown in Figure 1, 2, 3, the present embodiment provides a kind of multi-functional expansible survey suitable for bionic flapping-wing microreactor technology
Examination platform, including：Substrate 1, sensor placing component 2, first component 3, second component 6, cross slide way 10, sliding block 4, micro- flight
Device track segment 5, steel wire 8, worm screw knob 9.Two sliding blocks 4 are installed, transverse direction of the composition with sliding block is led on cross slide way 10
Rail, cross slide way 10 is obtained with sliding block 4 by buying, both model no requirement (NR)s.
First component 3, second component 6, microreactor technology track segment 5 constitute the support member for providing aircraft guide rail, branch
Support part part is arranged on the top of substrate, and sensor placing component 2 is arranged on the lower section of substrate；
First component 3, second component 6 form a whole installed in the upper surface of substrate 1, used as the portion of connection guide rail
Part；First component 3 is used for fixed cross slide way and substrate with sliding block；
Microreactor technology track segment 5 is the part of connection sliding block, on the part and the cross slide way with sliding block
Sliding block is relatively fixed, and microreactor technology track segment 5 is provided with hole for penetrating worm screw knob 9, same microreactor technology guide rail
A steel wire is connected between worm screw knob 9 on part 5, steel wire is parallel to each other, and is used as the guide rail of microreactor technology, it is mobile
Sliding block can adjust the spacing between steel wire.
In the present embodiment, except cross slide way 10, sliding block 4, steel wire 8, outside worm screw knob 9, remaining material all uses acrylic
Plate, is processed using laser cutting, and figure is two-dimensional sheet.
As shown in Fig. 2 in one embodiment, second component 6 has two, and first component 3 is one, and three's composition is complete
Support member, wherein first component 3 are used to fix sliding block 4, and two second components 6 are used to fix substrate 1.Sensor placing component
2 underfaces for being arranged on substrate 1.Microreactor technology track segment 5 is connected and justified margin with sliding block.
Described first component 3, second component 6, microreactor technology track segment 5 are all the two-dimensional shapes with uniform thickness
Template part, and three's thickness is identical, and second component 6, microreactor technology track segment 5 are symmetrical on Platform center.
The first component 3, the width of the part of the part fixed lateral guide rail 10 is consistent with the length of cross slide way 10, should
The width that part fixes the part of substrate 1 is consistent with the length of substrate 1, and the position that the part is placed is parallel with the side long of substrate 1,
Broadside with substrate 1 aligns；Distance of the median plane of the thickness direction of the part apart from the center of substrate 1 is equal to the component thickness
Half, the thickness of cross slide way 10, the half of the thickness of second component 6, the half sum of the thickness of microreactor technology track segment 5；
Second component 6, microreactor technology track segment 5 installation site for top edge and the sliding block 4 of support member top edge and align.
Described sensor placing component 2, its profile is the rectangle as substrate size, four edges and substrate 1
Four edges are alignd, and a distance is kept between substrate 1, do not need strict control；It is carved with sensor placing component 2 many
Bar groove, for using bolt and nut install sensor, and can slide along groove.Groove without specifying, can be according to conventional
Demand be adjusted.
In the present embodiment, sensor placing component 2 is identical with the profile of substrate 1, sensor placing component 2 and substrate 1
Vertical range is 10 centimetres.
In the present embodiment, the material that guide rail is used is steel wire.
As shown in Fig. 2 two two ends of steel wire 8 respectively through the edge of microreactor technology track segment 5 quadrant it
Afterwards, extend at worm screw knob 9, and it is connected, Wire pulling can be made by rotary worm knob 9.
As shown in figure 4, in the present embodiment：Described substrate 1, overall shape is rectangle, and four edges all have protuberance
Point, can be used to plug the module of expansion.Projection does not set specific length, its length can according to the total length of substrate and
Demands of individuals are designed.It is horizontal and vertical on substrate that a diameter of through hole of 6 millimeters is equipped with every 25 millimeters.
As shown in figure 5, there is the groove that a plurality of width is 4 millimeters in the present embodiment on sensor placing component 2.
As shown in figure 3, in the present embodiment, the distance of the median plane of first component 3 apart from the center of substrate 1 is first component 3
The half of thickness adds the thickness of guide rail plus the half of the thickness of microreactor technology track segment 5.
Such as Fig. 1, shown in 2, the outer rim of substrate 1 is mounted with the device of a set of expansion --- the extra gyration part 7 for expanding.
In the present embodiment, gyration part 7 includes two big disks and two bases for being used for support, and disc centre has one
Individual circular hole be used for rotate, disk border has row's small sircle hole, for turning an angle after be fixed.There are two on disk
Groove, the size of this two bar groove is consistent with the length dimension of two projections in edge of substrate 1, and substrate can be embedded in disk.
The application method of the platform is present embodiments provided, application method is：After installed above, slidably sliding block 4,
Change the distance between two steel wires, meet demand of the different micro- flapping wing bionic Aircrafts to guide rail.According to different measurement need
Ask, can fix different sensors with bolts and nuts on sensor placing component 2.If the shifting of aircraft need to be measured
Dynamic state, then can install laser displacement sensor, and measured immediately below guide rail on part 2.If desired survey
The lift of aircraft is measured, then the matched cantilever beam of size design that can be according to circular hole on substrate is measured.If
Need measure aircraft yawing or pitching moment, then can according to test lift identical method, on substrate pacify
Two cantilever beams are filled to measure.If desired any of the above parameter when testing flying vehicle is along angle of inclination flight, then only need
On the basis of more than, by rotating disk, and insertion bolt and nut is fixed in row's aperture, you can keep whole platform
Inclined state, is easy to study various parameters of micro- flapping wing bionic Aircraft on bevel direction.
The quantity of the steel wire 8 is identical with sliding block quantity, and the quantity of worm screw knob 9 is the twice of sliding block quantity.At other
In embodiment, steel wire, sliding block, the quantity of worm screw knob can set as needed.
Specific embodiment of the invention is described above.It is to be appreciated that the invention is not limited in above-mentioned
Particular implementation, those skilled in the art can within the scope of the claims make various deformations or amendments, this not shadow
Sound substance of the invention.
Claims (9)
1. a kind of multi-functional expansible test platform suitable for bionic flapping-wing microreactor technology, it is characterised in that including：Substrate, branch
Support part part, sensor placing component, the cross slide way with sliding block, microreactor technology track segment, worm screw knob and steel wire；Its
In：Microreactor technology track segment is connected with support member, and support member is connected with substrate, substrate and sensor placing component phase
Even；Support member and microreactor technology track segment are located at the top of substrate, and sensor placing component is located at the lower section of substrate；Support
Part is made up of two kinds of parts altogether, respectively one first component and two second components, the top of first component with carry
The cross slide way of sliding block is fixed, and the side of left and right two is respectively fixed with a second component, and second component is fixed with substrate；Microreactor technology is led
Rail part is relatively fixed with the sliding block on the cross slide way with sliding block, and microreactor technology track segment is provided with two
Hole is used to penetrate two worm screw knobs, and a steel is connected between two worm screw knobs on same microreactor technology track segment
Silk, steel wire is used perpendicular to base plan direction as the guide rail of aircraft, and mobile sliding block can adjust the position of steel wire；
The outer rim installing angle degree part of the substrate, the gyration part is used for what is supported including two disks and two
Base, disc centre has a circular hole for rotating, and disk border has row's small sircle hole, for turning an angle after consolidated
It is fixed；There are two bar grooves, the length dimension of two projections of size and substrate edges of this two bar groove is consistent, can be embedding by substrate on disk
In entering disk.
2. the multi-functional expansible test platform suitable for bionic flapping-wing microreactor technology according to claim 1, its feature
It is：The platform further sets all kinds of equipment related to flapping wing aircraft test, and these equipment are arranged on the sensing
On device placing component or around the substrate.
3. the multi-functional expansible test platform suitable for bionic flapping-wing microreactor technology according to claim 2, its feature
It is：All kinds of equipment related to flapping wing aircraft test is arranged on the sensor placing component by retaining element
Or around the substrate, its shape is identical with the installation requirements of sensor in the part of install sensor for retaining element, install
The groove of the position installed on its shape of part on sensor placing component and sensor placing component or through hole
Shaped position is identical.
4. the multi-functional expansible test platform suitable for bionic flapping-wing microreactor technology according to claim 1, its feature
It is：The overall shape of described substrate is rectangle, and four edges all have projection, the module for plugging expansion；Base
It is horizontal and vertical on plate to be provided with a through hole at a certain distance.
5. the multi-functional expansible test platform suitable for bionic flapping-wing microreactor technology according to claim 4, its feature
It is：Described sensor placing component, its profile is the four edges of the rectangle as substrate size, four edges and substrate
Alignment, keeps a distance between substrate；Many bar grooves are carved with sensor placing component, for installing sensing using bolt and nut
Device, and can be slided along groove.
6. the multi-functional expansible test suitable for bionic flapping-wing microreactor technology according to claim any one of 1-5 is flat
Platform, it is characterised in that：The first component and second component of the support member and microreactor technology track segment, are all have uniformly
The template part of the two-dimensional shapes of thickness, and thickness is identical.
7. the multi-functional expansible test suitable for bionic flapping-wing microreactor technology according to claim any one of 1-5 is flat
Platform, it is characterised in that：The first component of the support member, the width and cross slide way of the part of the part fixed lateral guide rail
Length is consistent, and the width that the part fixes the part of substrate is consistent with the length of substrate, position and the substrate of part placement
Side long is parallel, is alignd with the broadside of substrate.
8. the multi-functional expansible test platform suitable for bionic flapping-wing microreactor technology according to claim 7, its feature
It is：The first component of the support member, the center of the thickness direction of the part is equal to the part with the distance of substrate center
The half of thickness, the thickness of cross slide way, the half sum of microreactor technology track segment thickness；Two second of support member
Part is located at the right and left of first component, and vertical with first component, top edge and the first component of the two second components
Top edge aligns.
9. the multi-functional expansible test platform suitable for bionic flapping-wing microreactor technology according to claim 8, its feature
It is：The side that described microreactor technology track segment places steel wire has two quarter circular arcs, and steel wire is all from a snail
Bar knob sets out, and by a circular arc, then by second circular arc, finally reaches second worm screw knob.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201510309989.9A CN104960673B (en) | 2015-06-08 | 2015-06-08 | Suitable for the multi-functional expansible test platform of bionic flapping-wing microreactor technology |
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| CN201510309989.9A CN104960673B (en) | 2015-06-08 | 2015-06-08 | Suitable for the multi-functional expansible test platform of bionic flapping-wing microreactor technology |
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| CN104960673B true CN104960673B (en) | 2017-06-13 |
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Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639379A (en) * | 2018-06-29 | 2018-10-12 | 长沙市云智航科技有限公司 | A kind of aircraft rotor component test device |
| CN109927932B (en) * | 2018-09-18 | 2021-06-29 | 山东大学 | Adjustable flapping wing aircraft force measuring platform and installation and use method thereof |
| CN109204884B (en) * | 2018-11-22 | 2020-08-18 | 电子科技大学 | Miniature flapping-wing aircraft experimental platform and flight data acquisition method based on same |
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| WO2011142864A2 (en) * | 2010-02-11 | 2011-11-17 | President And Fellows Of Harvard College | Passive torque balancing in a high-frequency oscillating system |
| CN102338690A (en) * | 2011-05-20 | 2012-02-01 | 西北工业大学 | Three-freedom-degree flapping-wing comprehensive experiment platform |
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