CN108106813B - A kind of airplane skin material wind detection device - Google Patents
A kind of airplane skin material wind detection device Download PDFInfo
- Publication number
- CN108106813B CN108106813B CN201810007871.4A CN201810007871A CN108106813B CN 108106813 B CN108106813 B CN 108106813B CN 201810007871 A CN201810007871 A CN 201810007871A CN 108106813 B CN108106813 B CN 108106813B
- Authority
- CN
- China
- Prior art keywords
- wind
- fixedly mounted
- small
- circular
- sized
- 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.)
- Active
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
- G01M9/06—Measuring arrangements specially adapted for aerodynamic testing
Abstract
The invention discloses a kind of airplane skin material wind detection devices, including pedestal, the pedestal is equipped with material rotating mechanism, the material rotating mechanism is equipped with square groove, servo motor, shaft coupling, rotation axis, spherical placing table, circular groove, electric telescopic rod, fixing axle, small-sized fixing bearing, connection sheet, connecting plate, hold plate, sheathing material, the pedestal is equipped with wind-force testing agency, the wind-force testing agency is equipped with supporting leg, circular non-opaque channel, wind sensor, circular open, support column, taper intake stack, spray wind spray head, wind deflector, circular hole, air blower, blast pipe, small-sized wind power generator structure collectively forms, the small-sized wind power generator structure is equipped with fixed frame, fixed link, small generator, small-sized wind wheel, small-sized fan blade, inverter, battery, natural wind power generation mechanism is total With what is constituted, the base upper surface side is equipped with controller.The invention has the advantages that of simple structure and strong practicability.
Description
Technical field
The present invention relates to aeronautical material field, especially a kind of airplane skin material wind detection device.
Background technique
Aircraft, due to excessive velocities, causes wind-force excessive to the pressure of its outer surface, holds on aircraft in high airflight
It is loaded with passenger, just in case accident occurs, can be threatened to the security of the lives and property of passenger, so aircraft is selected in production
Material all needs to rest in theoretical calculation by actually detected.
Summary of the invention
The purpose of the present invention is to solve the above problems, devise a kind of airplane skin material wind detection device.
Realize above-mentioned purpose the technical scheme is that, a kind of airplane skin material wind detection device, including pedestal,
The pedestal is fixedly mounted on outdoor ground, and the pedestal is equipped with material rotating mechanism, the material rotating mechanism by
Positioned at base upper surface square groove, be fixedly mounted in square groove and servo motor that round end is upward, one end with watch
Rotation axis that the shaft coupling, one end that motor round end is fixedly connected be fixedly connected with the shaft coupling other end is taken, is fixedly mounted on and turns
The moving axis other end and the spherical placing table of upper end level excision, to be located at the spherical equally distributed multiple circles in placing table upper surface recessed
Slot, is fixedly mounted on consolidating for electric telescopic rod upper end two sides at the multiple electric telescopic rods being respectively and fixedly installed in circular groove
Dead axle, is respectively and fixedly installed to small-sized fixing bearing upper end at the small-sized fixing bearing for being fixedly set in fixing axle two sides respectively
Connection sheet, is fixedly mounted on holding plate, being fixedly mounted for connecting plate upper surface at the connecting plate for being fixedly mounted on connection sheet upper surface
It is collectively formed in the sheathing material for holding plate upper surface, the pedestal is equipped with wind-force testing agency, the wind-force testing agency
By being fixedly mounted on the equally distributed multiple supporting legs in base upper surface two sides, being fixedly mounted on the circle of supporting leg upper surface thoroughly
Bright channel is fixedly mounted on the wind sensor of rear side in circular non-opaque channel, the signal transmitting inside wind sensor
Device one, below the circular non-opaque channel circular open of side, be fixedly mounted on two sides in circular non-opaque channel and be uniformly distributed
Multiple support columns, be fixedly mounted on support column upper surface taper intake stack, be fixedly mounted on taper intake stack outlet air
Different types of spray wind spray head at end is fixedly mounted on taper intake stack air intake and surrounding and circular non-opaque vias inner walls are solid
Surely the wind deflector that connects, on wind deflector equally distributed multiple circular holes, be fixedly mounted on base upper surface side and uniformly divide
Cloth and air intake towards different directions multiple air blowers, one end is fixedly connected with the other end with blower export end and circular hole is fixed
The blast pipe of connection, the small-sized wind power generator structure for being fixedly mounted on circular non-opaque channel outlet air end collectively form, described small-sized
Wind generator set is by being fixedly mounted on fixed frame on the outside of circular non-opaque channel outlet on ground, being fixedly mounted on fixed frame
The fixed link of upper front end, the small generator being fixedly mounted on above fixed link, before being fixedly mounted on small power generation inboard rotor
The small-sized wind wheel at end is fixedly mounted on equally distributed multiple small-sized fan blades on small-sized wind wheel, is fixedly mounted on fixed frame
Inverter, the battery being fixedly mounted on fixed frame, the common structure of natural wind power generation mechanism being fixedly mounted on rear side of fixed frame
At the base upper surface side is equipped with controller.
The spherical shape placing table is entered in circular non-opaque channel by circular open.
Gasket is equipped between the circular open and spherical placing table.
The variety classes spray wind spray head not only can change the type of spray wind, can also change the angle of spray wind.
The air blower is equipped with knob wind-force regulating switch.
Electric quantity detection apparatus is equipped in the battery.
The natural wind power generation mechanism is by being fixedly mounted on tower tube on rear side of fixed frame on ground, being fixedly mounted in tower tube
The fixed station on surface, positioned at fixed station upper surface groove, be fixedly mounted on the stepper motor of lower surface in groove, be fixedly mounted
Stepper motor round end generator, be fixedly mounted on generator inner rotor front end wind wheel, be fixedly mounted on wind wheel
The fan blade of even distribution, the wind transducer for being fixedly mounted on fixed station upper surface side, the signal inside wind transducer
Transmitter two collectively forms.
It is equipped in the controller and uses electrical interface, capacitor display screen, signal receiver, PLC system.
The signal projector one and signal projector two are connect by Bluetooth signal with signal receiver.
The controller and servo motor, electric telescopic rod, wind sensor, air blower, battery, wind transducer electricity
Property connection, controlled by PLC system.
The airplane skin material wind detection device made using technical solution of the present invention can will manufacture selected when aircraft
The sheathing material that takes carries out wind-force test, can be gradually increased wind-force as needed, and can be according to aircraft flight course in the sky
In a variety of situations for encountering simulated, the sheathing material of aircraft can be rotated, and can adjust the angle height as needed, in many ways
It is detected in position, and can convert wind energy into electric energy, saves electric power resource.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of airplane skin material wind detection device of the present invention；
Fig. 2 is the fragmentary sectional view of airplane skin material wind detection device of the present invention；
Fig. 3 is the partial schematic diagram of material rotating mechanism of the present invention；
Fig. 4 is the partial schematic diagram of natural wind power generation mechanism of the present invention；
Fig. 5 is the partial schematic diagram of controller of the present invention；
In figure, 1, pedestal；2, square groove；3, servo motor；4, shaft coupling；5, rotation axis；6, spherical placing table；7, circle
Connected in star；8, electric telescopic rod；9, fixing axle；10, small-sized fixing bearing；11, connection sheet；12, connecting plate；13, plate is held；
14, sheathing material；15, supporting leg；16, circular non-opaque channel；17, wind sensor；18, signal projector one；19, circle is opened
Mouthful；20, support column；21, taper intake stack；22, wind spray head is sprayed；23, wind deflector；24, circular hole；25, air blower；26, it enters the wind
Pipe；27, fixed frame；28, fixed link；29, small generator；30, small-sized wind wheel；31, small-sized fan blade；32, inverter；33, it stores
Battery；34, controller；35, gasket；36, knob wind-force regulating switch；37, electric quantity detection apparatus；38, tower tube；39, solid
Determine platform；40, groove；41, stepper motor；42, generator；43, wind wheel；44, fan blade；45, wind transducer；46, signal emits
Device two；47, electrical interface is used；48, capacitor display screen；49, signal receiver；50, PLC system.
Specific embodiment
The present invention is specifically described with reference to the accompanying drawing, as shown in Figs. 1-5, a kind of airplane skin material wind-force detection
Device, including pedestal 1, the pedestal 1 are fixedly mounted on outdoor ground, and the pedestal 1 is equipped with material rotating mechanism, institute
Material rotating mechanism is stated by being located at the square groove 2 of 1 upper surface of pedestal, being fixedly mounted in square groove 2 and round end is upward
Servo motor 3, one end shaft coupling 4, one end and 4 other end of shaft coupling that are fixedly connected with 3 round end of servo motor are fixed connects
The rotation axis 5 that connects, is located at spherical placing table at the spherical placing table 6 for being fixedly mounted on 5 other end of rotation axis and the excision of upper end level
The equally distributed multiple circular grooves 7 in 6 upper surfaces, are consolidated the multiple electric telescopic rods 8 being respectively and fixedly installed in circular groove 7
Dingan County mounted in 8 upper end two sides of electric telescopic rod fixing axle 9, be fixedly set in the small-sized fixing bearings of 9 two sides of fixing axle respectively
10, the connection sheet 11 for being respectively and fixedly installed to small-sized 10 upper end of fixing bearing, the connection for being fixedly mounted on 11 upper surface of connection sheet
Plate 12 is fixedly mounted on holding plate 13, being fixedly mounted on the sheathing material 14 for holding 13 upper surface of plate for 12 upper surface of connecting plate
It collectively forms, the pedestal 1 is equipped with wind-force testing agency, and the wind-force testing agency is by being fixedly mounted on 1 upper surface of pedestal
The equally distributed multiple supporting legs 15 in two sides, are fixedly mounted the circular non-opaque channel 16 for being fixedly mounted on 15 upper surface of supporting leg
The wind sensor 17 of rear side, the signal projector 1 inside wind sensor 17, position in circular non-opaque channel 16
In 16 lower section side of circular non-opaque channel circular open 19, to be fixedly mounted on two sides in circular non-opaque channel 16 equally distributed
Multiple support columns 20, are fixedly mounted on taper intake stack at the taper intake stack 21 for being fixedly mounted on 20 upper surface of support column
Different types of spray wind spray head 22 at 21 outlet air ends is fixedly mounted on 21 air intake of taper intake stack and surrounding and circular non-opaque
Wind deflector 23 that 16 inner wall of channel is fixedly connected, on wind deflector 23 equally distributed multiple circular holes 24, be fixedly mounted on bottom
1 upper surface side of seat is uniformly distributed and air intake is towards 25 outlet end of multiple air blowers 25 of different directions, one end and air blower
It is fixedly connected with blast pipe 26 that the other end is fixedly connected with circular hole 24, is fixedly mounted on the small-sized of 16 outlet air end of circular non-opaque channel
Wind generator set collectively forms, and the small-sized wind power generator structure is by being fixedly mounted on the outside of 16 outlet end of circular non-opaque channel
Fixed frame 27 on ground, is fixedly mounted on 28 top of fixed link at the fixed link 28 for being fixedly mounted on front end on fixed frame 27
Small generator 29, is fixedly mounted on small-sized wind wheel at the small-sized wind wheel 30 for being fixedly mounted on 29 internal rotor front end of small generator
Equally distributed multiple small-sized fan blades 31 on 30, are fixedly mounted on fixed frame at the inverter 32 being fixedly mounted on fixed frame 27
Battery 33 on 27, the natural wind power generation mechanism for being fixedly mounted on 27 rear side of fixed frame collectively form, 1 upper surface of pedestal
Side is equipped with controller 34；The spherical shape placing table 6 is entered in circular non-opaque channel 16 by circular open 19；The circle is opened
Gasket 35 is equipped between mouth 19 and spherical placing table 6；The variety classes spray wind spray head 22 not only can change the kind of spray wind
Class can also change the angle of spray wind；The air blower 25 is equipped with knob wind-force regulating switch 36；In the battery 33
Equipped with electric quantity detection apparatus 37；The natural wind power generation mechanism by be fixedly mounted on 27 rear side ground of fixed frame tower tube 38,
Be fixedly mounted on 38 upper surface of tower tube fixed station 39, positioned at 39 upper surface of fixed station groove 40, be fixedly mounted on groove 40
The stepper motor 41 of interior lower surface, is fixedly mounted on generator 42 at the generator 42 for being fixedly mounted on 41 round end of stepper motor
The wind wheel 43 of internal rotor front end is fixedly mounted on equally distributed fan blade 44 on wind wheel 43, is fixedly mounted on table on fixed station 39
The wind transducer 45 of face side, the signal projector 2 46 inside wind transducer 45 collectively form；The controller
It is equipped in 34 and uses electrical interface 47, capacitor display screen 48, signal receiver 49, PLC system 50；The signal projector 1 and letter
Number transmitter 2 46 is connect by Bluetooth signal with signal receiver 49；The controller 34 and servo motor 3, electric telescopic rod
8, wind sensor 17, air blower 25, battery 33, wind transducer 45 are electrically connected, and are controlled by PLC system 50.
The characteristics of the present embodiment is that pedestal is fixedly mounted on outdoor ground, and pedestal is equipped with material rotating mechanism,
Material rotating mechanism is by being located at the square groove of base upper surface, being fixedly mounted in square groove and servo that round end is upward
Rotation axis that shaft coupling that motor, one end are fixedly connected with servo motor round end, one end are fixedly connected with the shaft coupling other end,
It is fixedly mounted on the spherical placing table of the rotation axis other end and the excision of upper end level, is uniformly distributed positioned at spherical placing table upper surface
Multiple circular grooves, be respectively and fixedly installed in circular groove multiple electric telescopic rods, be fixedly mounted on electric telescopic rod
The fixing axle of upper end two sides, the small-sized fixing bearing for being fixedly set in fixing axle two sides respectively, be respectively and fixedly installed to it is small-sized solid
Dead axle holds the connection sheet of upper end, the connecting plate for being fixedly mounted on connection sheet upper surface, the Sheng for being fixedly mounted on connecting plate upper surface
Plate is put, is fixedly mounted on and is held the sheathing material of plate upper surface and collectively form, pedestal is equipped with wind-force testing agency, wind-force detection
Mechanism is by the circle that is fixedly mounted on the equally distributed multiple supporting legs in base upper surface two sides, is fixedly mounted on supporting leg upper surface
Shape transparent channel is fixedly mounted on the wind sensor of rear side, the signal inside wind sensor in circular non-opaque channel
Transmitter one, below the circular non-opaque channel circular open of side, to be fixedly mounted on two sides in circular non-opaque channel uniform
Multiple support columns of distribution, are fixedly mounted on taper intake stack at the taper intake stack for being fixedly mounted on support column upper surface
Different types of spray wind spray head at outlet air end is fixedly mounted on taper intake stack air intake and in surrounding and circular non-opaque channel
Wind deflector that wall is fixedly connected, on wind deflector equally distributed multiple circular holes, to be fixedly mounted on base upper surface side equal
Even distribution and air intake are fixedly connected with the other end and circular hole with blower export end towards multiple air blowers of different directions, one end
The blast pipe that is fixedly connected, the small-sized wind power generator structure for being fixedly mounted on circular non-opaque channel outlet air end collectively form, small-sized
Wind generator set is by being fixedly mounted on fixed frame on the outside of circular non-opaque channel outlet on ground, being fixedly mounted on fixed frame
The fixed link of upper front end, the small generator being fixedly mounted on above fixed link, before being fixedly mounted on small power generation inboard rotor
The small-sized wind wheel at end is fixedly mounted on equally distributed multiple small-sized fan blades on small-sized wind wheel, is fixedly mounted on fixed frame
Inverter, the battery being fixedly mounted on fixed frame, the common structure of natural wind power generation mechanism being fixedly mounted on rear side of fixed frame
Controller is equipped at, base upper surface side, it is a kind of to gradually increase that wind-force, sheathing material are rotatable, collect wind-power electricity generation
Airplane skin material wind detection device carries out wind-force detection to sheathing material at many levels, has ensured the in-flight peace of aircraft
Entirely, electric power resource is saved.
In the present embodiment, sheathing material is fixedly installed to and is held on plate, start air blower, by blast pipe by wind
It pours into taper intake stack, and is sprayed by the spray wind spray head in front of taper intake stack, can be replaced according to actual needs not
Congener spray head, the different situations in simulated altitude, in the detection process, starting servo motor change sheathing material to wind
Different location changes sheathing material to the angle of wind by elongating or shortening the electric telescopic rod of different location, multi-faceted to it
It is detected, the size of wind-force is experienced by wind sensor, and sent signal in controller, gradually adjusted as needed
The size of wind-force is blown small-sized fan blade by the wind that circular non-opaque pipeline outlet air end is gone out and is rotated, sent out by small generator
Electricity experiences wind direction by wind transducer, and send signal to after inverter is integrated by power storage into battery
In controller, by controller control stepper motor rotation, generator rotation is driven by stepper motor, wind wheel is made to face the side of wind
To, electricity in electric quantity detection apparatus in battery detection battery, after electricity is full, by stepper motor by the direction of wind wheel
Rotation is lateral, stopping power generation, completion whole work process.
Above-mentioned technical proposal only embodies the optimal technical scheme of technical solution of the present invention, those skilled in the art
The principle of the present invention is embodied to some variations that some of them part may be made, belongs to the scope of protection of the present invention it
It is interior.
Claims (10)
1. a kind of airplane skin material wind detection device, including pedestal (1), which is characterized in that the pedestal (1) is fixedly mounted
On outdoor ground, the pedestal (1) is equipped with material rotating mechanism, and the material rotating mechanism is by being located on pedestal (1)
The square groove (2) on surface is fixedly mounted on square groove (2) is interior and round end is upward servo motor (3), one end and servo
It is rotation axis (5) that shaft coupling (4) that motor (3) round end is fixedly connected, one end are fixedly connected with shaft coupling (4) other end, solid
Dingan County is mounted in the spherical placing table (6) of rotation axis (5) other end and the excision of upper end level, is located at spherical placing table (6) upper surface
Equally distributed multiple circular grooves (7), are fixed at the multiple electric telescopic rods (8) being respectively and fixedly installed in circular groove (7)
The fixing axle (9) for being mounted on electric telescopic rod (8) upper end two sides, the small-sized fixation for being fixedly set in fixing axle (9) two sides respectively
Bearing (10), is fixedly mounted on connection sheet (11) at the connection sheet (11) for being respectively and fixedly installed to small-sized fixing bearing (10) upper end
The connecting plate (12) of upper surface is fixedly mounted on holding plate (13), being fixedly mounted on and hold plate for connecting plate (12) upper surface
(13) sheathing material (14) of upper surface collectively forms, and the pedestal (1) is equipped with wind-force testing agency, the wind-force detection machine
Structure is by being fixedly mounted on the equally distributed multiple supporting legs (15) in pedestal (1) upper surface two sides, being fixedly mounted on supporting leg (15)
The circular non-opaque channel (16) of upper surface is fixedly mounted on the wind sensor (17) of rear side, position in circular non-opaque channel (16)
In the internal signal projector one (18) of wind sensor (17), the circular open positioned at side below circular non-opaque channel (16)
(19), the equally distributed multiple support columns (20) in circular non-opaque channel (16) interior two sides are fixedly mounted on, are fixedly mounted on support
The taper intake stack (21) of column (20) upper surface is fixedly mounted on different types of spray at taper intake stack (21) outlet air end
Wind spray head (22) is fixedly mounted on taper intake stack (21) air intake and surrounding and circular non-opaque channel (16) inner wall are fixed connects
The wind deflector (23) that connects is located at equally distributed multiple circular holes (24) on wind deflector (23), is fixedly mounted on pedestal (1) upper surface
Side is uniformly distributed and air intake connects towards multiple air blowers (25) of different directions, one end and air blower (25) outlet end are fixed
It connects blast pipe (26) that the other end is fixedly connected with circular hole (24), be fixedly mounted on the small-sized of circular non-opaque channel (16) outlet air end
Wind generator set collectively forms, and the small-sized wind power generator structure is by being fixedly mounted on outside circular non-opaque channel (16) outlet end
Fixed frame (27) on the ground of side, is fixedly mounted on fixed link at the fixed link (28) for being fixedly mounted on front end on fixed frame (27)
(28) small generator (29) above, the small-sized wind wheel (30) for being fixedly mounted on small generator (29) internal rotor front end, solid
Dingan County is mounted in equally distributed multiple small-sized fan blades (31), the inversion being fixedly mounted on fixed frame (27) on small-sized wind wheel (30)
Device (32), the battery (33) being fixedly mounted on fixed frame (27), the natural wind being fixedly mounted on rear side of fixed frame (27) hair
Motor structure collectively forms, and pedestal (1) the upper surface side is equipped with controller (34).
2. a kind of airplane skin material wind detection device according to claim 1, which is characterized in that the spherical shape is held
Platform (6) is entered in circular non-opaque channel (16) by circular open (19).
3. a kind of airplane skin material wind detection device according to claim 1, which is characterized in that the circular open
(19) gasket (35) are equipped between spherical placing table (6).
4. a kind of airplane skin material wind detection device according to claim 1, which is characterized in that the variety classes
Spray wind spray head (22) not only can change the type of spray wind, can also change the angle of spray wind.
5. a kind of airplane skin material wind detection device according to claim 1, which is characterized in that the air blower
(25) it is equipped with knob wind-force regulating switch (36).
6. a kind of airplane skin material wind detection device according to claim 1, which is characterized in that the battery
(33) electric quantity detection apparatus (37) are equipped in.
7. a kind of airplane skin material wind detection device according to claim 1, which is characterized in that the natural wind hair
Motor structure is by being fixedly mounted on tower tube (38) on rear side of fixed frame (27) on ground, being fixedly mounted on consolidating for tower tube (38) upper surface
Determine platform (39), the groove (40) for being located at fixed station (39) upper surface, be fixedly mounted on the stepper motor of groove (40) interior lower surface
(41), it is fixedly mounted on the generator (42) of stepper motor (41) round end, is fixedly mounted on generator (42) internal rotor front end
Wind wheel (43), be fixedly mounted on equally distributed fan blade (44) on wind wheel (43), be fixedly mounted on fixed station (39) upper surface
The wind transducer (45) of side, the signal projector two (46) for being located at wind transducer (45) inside collectively form.
8. a kind of airplane skin material wind detection device according to claim 7, which is characterized in that the controller
(34) it is equipped in and uses electrical interface (47), capacitor display screen (48), signal receiver (49), PLC system (50).
9. a kind of airplane skin material wind detection device according to claim 8, which is characterized in that the signal transmitting
Device one (18) and signal projector two (46) are connect by Bluetooth signal with signal receiver (49).
10. a kind of airplane skin material wind detection device according to claim 1, which is characterized in that the controller
(34) it is sensed with servo motor (3), electric telescopic rod (8), wind sensor (17), air blower (25), battery (33), wind direction
Device (45) is electrically connected, and is controlled by PLC system (50).
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811211211.4A CN109470444A (en) | 2018-01-04 | 2018-01-04 | A kind of airplane skin material wind detection device |
| CN201810007871.4A CN108106813B (en) | 2018-01-04 | 2018-01-04 | A kind of airplane skin material wind detection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810007871.4A CN108106813B (en) | 2018-01-04 | 2018-01-04 | A kind of airplane skin material wind detection device |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811211211.4A Division CN109470444A (en) | 2018-01-04 | 2018-01-04 | A kind of airplane skin material wind detection device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108106813A CN108106813A (en) | 2018-06-01 |
| CN108106813B true CN108106813B (en) | 2019-01-01 |
Family
ID=62219774
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811211211.4A Withdrawn CN109470444A (en) | 2018-01-04 | 2018-01-04 | A kind of airplane skin material wind detection device |
| CN201810007871.4A Active CN108106813B (en) | 2018-01-04 | 2018-01-04 | A kind of airplane skin material wind detection device |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811211211.4A Withdrawn CN109470444A (en) | 2018-01-04 | 2018-01-04 | A kind of airplane skin material wind detection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (2) | CN109470444A (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108844706A (en) * | 2018-08-21 | 2018-11-20 | 北京化工大学 | A kind of array multi-function windtunnel drive system |
| CN114427931B (en) * | 2022-01-26 | 2023-05-12 | 内蒙古工业大学 | Wind power automatic testing device of wind power generator |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3472835B2 (en) * | 2001-11-26 | 2003-12-02 | 防衛庁技術研究本部長 | Dynamic wind tunnel test equipment |
| CN101545953A (en) * | 2009-04-24 | 2009-09-30 | 重庆大学 | Minitype aerogenerator performance testing method and special testing platform thereof |
| CN105004503A (en) * | 2015-06-29 | 2015-10-28 | 中国海洋大学 | Self-elevating type offshore platform wind load coefficient test experimental system |
| CN106768809A (en) * | 2017-01-17 | 2017-05-31 | 湖南城市学院 | A kind of wind energy conversion system wind and rain structure Coupling model test apparatus |
| CN206271285U (en) * | 2016-10-21 | 2017-06-20 | 李华玺 | A kind of wind power generation apparatus for demonstrating with wind speed measurement |
| CN206470036U (en) * | 2017-02-20 | 2017-09-05 | 湖北海力士电气股份有限公司 | A kind of wind-force analogue experiment installation |
-
2018
- 2018-01-04 CN CN201811211211.4A patent/CN109470444A/en not_active Withdrawn
- 2018-01-04 CN CN201810007871.4A patent/CN108106813B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3472835B2 (en) * | 2001-11-26 | 2003-12-02 | 防衛庁技術研究本部長 | Dynamic wind tunnel test equipment |
| CN101545953A (en) * | 2009-04-24 | 2009-09-30 | 重庆大学 | Minitype aerogenerator performance testing method and special testing platform thereof |
| CN105004503A (en) * | 2015-06-29 | 2015-10-28 | 中国海洋大学 | Self-elevating type offshore platform wind load coefficient test experimental system |
| CN206271285U (en) * | 2016-10-21 | 2017-06-20 | 李华玺 | A kind of wind power generation apparatus for demonstrating with wind speed measurement |
| CN106768809A (en) * | 2017-01-17 | 2017-05-31 | 湖南城市学院 | A kind of wind energy conversion system wind and rain structure Coupling model test apparatus |
| CN206470036U (en) * | 2017-02-20 | 2017-09-05 | 湖北海力士电气股份有限公司 | A kind of wind-force analogue experiment installation |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108106813A (en) | 2018-06-01 |
| CN109470444A (en) | 2019-03-15 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106525375B (en) | Self-adaptive system for detecting wind resistance of unmanned aerial vehicle | |
| CN107065915B (en) | A kind of six degree of freedom rotor craft on-line debugging platform | |
| CN108106813B (en) | A kind of airplane skin material wind detection device | |
| CN207108388U (en) | A kind of fall arrest aerial work platform | |
| CN108225809B (en) | Ground test system for flight performance of unmanned aerial vehicle | |
| CN213168607U (en) | Special test platform of unmanned aerial vehicle | |
| CN108502188A (en) | A kind of plant protection drone spraying operation wind field test system and method | |
| CN110082060A (en) | A kind of plant protection unmanned aerial vehicle wind resistance test equipment and method | |
| CN109367818A (en) | A kind of rotor wing unmanned aerial vehicle gesture stability test macro and method, unmanned plane | |
| CN216207931U (en) | Unmanned aerial vehicle for sampling haze pollution vertical gradient atmospheric particulates | |
| CN104590582B (en) | A kind of aircraft blade power imitates test device | |
| CN107656092A (en) | A kind of Wind turbines wind speed and direction measuring device and method | |
| CN104843191B (en) | Contactless smart rain insensitive device for unmanned plane | |
| CN104406531A (en) | Wind-induced displacement testing device for cooling tower aeroelastic model | |
| CN204613238U (en) | A kind of wind speed measuring apparatus | |
| CN204613239U (en) | A kind of base construction of wind speed measuring apparatus | |
| CN213139182U (en) | Testing device for unmanned aerial vehicle | |
| EP4009516A1 (en) | Hybrid power generation system | |
| CN106968884A (en) | Gate-type impeller for wind-power electricity generation | |
| CN208278330U (en) | A kind of plant protection drone spraying operation wind field test macro | |
| CN111056004A (en) | Unmanned aerial vehicle inspection system for power grid supervision | |
| CN206517342U (en) | A kind of high-altitude solar power generation unit and electricity generation system | |
| CN104787341B (en) | A kind of high-rise building multi-parameters sampling device based on aeromodelling airplane | |
| CN204548506U (en) | Based on the high-rise building multi-parameters sampling device of aeromodelling airplane | |
| CN109143409A (en) | Monitoring device for upper atmosphere flowing property |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB02 | Change of applicant information |
Address after: 350000 168 JINDA Road, Jianxin Town, Cangshan District, Fuzhou, Fujian. Applicant after: Gao Qinxian Address before: No. 2216, Xingang Road, Binhai New Area, Tianjin City, Tianjin Applicant before: Gao Qinxian |
|
| CB02 | Change of applicant information | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20181010 Address after: 230031 B-1014, 10 floor, business office building, Wo Ye garden, Shushan District, Hefei, Anhui. Applicant after: HEFEI WISDOM LONGTUTENG INTELLECTUAL PROPERTY CO., LTD. Address before: 350000 168 JINDA Road, Jianxin Town, Cangshan District, Fuzhou, Fujian. Applicant before: Gao Qinxian |
|
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20181115 Address after: 242199 No. 21-5 Zhonggang West Road, Jianping Town, Langxi County, Xuancheng City, Anhui Province Applicant after: Xuancheng Conscience Intellectual Property Service Co., Ltd. Address before: 230031 B-1014, 10 floor, business office building, Wo Ye garden, Shushan District, Hefei, Anhui. Applicant before: HEFEI WISDOM LONGTUTENG INTELLECTUAL PROPERTY CO., LTD. |
|
| TA01 | Transfer of patent application right | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |