CN109891030A - Airplane parking area - Google Patents
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- CN109891030A CN109891030A CN201780066296.9A CN201780066296A CN109891030A CN 109891030 A CN109891030 A CN 109891030A CN 201780066296 A CN201780066296 A CN 201780066296A CN 109891030 A CN109891030 A CN 109891030A
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- 238000012545 processing Methods 0.000 claims abstract description 33
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 16
- 239000011888 foil Substances 0.000 claims description 14
- 238000004891 communication Methods 0.000 claims description 2
- 238000001514 detection method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 238000005259 measurement Methods 0.000 description 3
- 230000006978 adaptation Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012790 confirmation Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
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- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
- E01F3/00—Landing stages for helicopters, e.g. located above buildings
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01G—WEIGHING
- G01G19/00—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups
- G01G19/02—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups for weighing wheeled or rolling bodies, e.g. vehicles
- G01G19/07—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups for weighing wheeled or rolling bodies, e.g. vehicles for weighing aircraft
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
- Measuring Fluid Pressure (AREA)
Abstract
A kind of airplane parking area (100); include: pedestal (1), the shutdown platform (2) being installed on pedestal (1), be set to the measuring wind speed module (3) shut down on platform (2) and the processing module (4) being electrically connected with measuring wind speed module (3); processing module (4) is configured as: obtaining measuring wind speed module (3) real-time airflow value detected, and real-time airflow value is compared with setting airflow value；When real-time airflow value lower than setting airflow value when, determine unmanned vehicle landed in shut down platform (2) or do not reach shut down platform (2) airspace；When real-time airflow value is higher than setting airflow value, determine that unmanned vehicle is in the airspace for shutting down platform (2).The airplane parking area is compared by air measuring module airflow value detected with setting airflow value, can accurately judge that unmanned vehicle has landed in shutdown platform or whether in the airspace for shutting down platform.
Description
The present invention relates to unmanned vehicles to stop technical field, in particular to a kind of airplane parking area.
Place of the airplane parking area for unmanned vehicle landing, is of crucial importance unmanned vehicle.The current effect in existing airplane parking area is relatively simple, can take off or identify landing for unmanned vehicle, usually only includes weight detecting for unmanned vehicle, i.e. when detecting weight, confirmation aircraft landing is in airplane parking area on no shutdown level ground.
However; unmanned vehicle is behind the airspace for entering airplane parking area; the air pressure for acting on airplane parking area is generated since the rotor of unmanned vehicle forms downward air-flow; airplane parking area weight detected can also change at this time; so cause according to airplane parking area result detected; it can not definitely pick out whether unmanned vehicle has landed on airplane parking area, be easy to causeing erroneous judgement accident.
Summary of the invention
The present invention propose it is a kind of can detecte unmanned vehicle whether reach shut down platform airspace or whether land in shut down platform airplane parking area.
According to an embodiment of the invention, providing a kind of airplane parking area characterized by comprising pedestal, the shutdown platform being installed on the pedestal, the measuring wind speed module on the shutdown platform, and the processing module being electrically connected with the measuring wind speed module；
Wherein, the processing module is configured as: obtaining the measuring wind speed module real-time airflow value detected, and the real-time airflow value is compared with setting airflow value；When the real-time airflow value is lower than the setting airflow value, determine that unmanned vehicle has landed in the shutdown platform or do not reached the airspace for shutting down platform；When the real-time airflow value is higher than the setting airflow value, determine that the unmanned vehicle is in the airspace for shutting down platform.
Further, the airplane parking area further includes set on the edge ring for shutting down platform, and the measuring wind speed module is set on the outer rim ring.
Further, the measuring wind speed module is multiple, and multiple measuring wind speed modules are set in the edge ring；Wherein, the real-time airflow value is the processing module according to multiple measuring wind speed module airflow values detected, calculated average airflow value.
Further; the height of the edge ring is higher than the shutdown platform; multiple through-holes are formed in the edge ring; multiple through-holes are arranged along the edge ring circular array; the measuring wind speed module is set in the through-hole, for detecting the air quantity for flowing out the edge ring through the through-hole from the shutdown platform.
Further, the measuring wind speed module includes fan and infrared tube unit；Wherein, when the fan is by air stream drives, the infrared tube unit detects the revolving speed of the fan so that it is determined that real-time airflow value on the airplane parking area.
Further, the pedestal is equipped with positioning annular distance, and the bottom for shutting down platform is equipped with the connecting column with the positioning annular distance cooperation；Wherein, the processing module is set in the connecting column or is set between the connecting column and the positioning annular distance.
Further, the airplane parking area further includes carrying the manometric module for shutting down platform, and the manometric module and the processing module are electrically connected；
Wherein, the processing module is according to the manometric module real-time weight value detected compared with setting weight value; in the state that the real-time airflow value is lower than the setting airflow value; when the real-time weight value is greater than the setting weight value, determine that unmanned vehicle has landed in the shutdown platform；When the real-time weight value is less than the setting magnitude, determine that the unmanned vehicle does not reach the airspace for shutting down platform.
Further, when the real-time weight value is less than the setting magnitude, the processing module is also used to the airflow value obtained according to the air measuring module, calculates the distance between the unmanned vehicle and the shutdown platform.
Further, the manometric module is one, and the manometric module is set to the center for shutting down platform.
Further, the manometric module is multiple, and multiple manometric modules are set on the shutdown platform；Wherein, the real-time weight value is the processing module according to multiple manometric module weight values detected, calculated averaged weight value.
Further, the manometric module includes strain pressure transducer.
Further, the manometric module includes collet, the strain pressure block on the collet, the foil gauge being oppositely arranged with the strain pressure block and the upper mounted plate on the foil gauge, and fixed plate is to affixed with shutdown platform；Wherein, when unmanned vehicle landing is when the shutdown platform, pass through the relatively described strain pressure block of the foil gauge is displaced the real-time weight value determined on the shutdown platform.
Further, the airplane parking area further includes the remote control terminal with processing module communication connection, to obtain the relatively described state for shutting down platform of the unmanned vehicle.
Further, the platform of shutting down is equipped with the identification identified for the unmanned vehicle
Mark, the identification mark are set to the center for shutting down platform.
The technical solution that the embodiment of the present invention provides can include the following benefits: airplane parking area of the invention is equipped with air measuring module on shutting down platform; pass through air measuring module airflow value detected; it can accurately judge that unmanned vehicle is in the state for having landed in the shutdown platform or whether being in the airspace for shutting down platform; the above-mentioned state of unmanned vehicle is determined in advance; it realizes and state of the unmanned vehicle with respect to airplane parking area is identified and determined from different dimensions, prevent the state whether landed to unmanned plane from causing to judge by accident.
It should be understood that above general description and following detailed description be only it is exemplary and explanatory, the present invention can not be limited.
To describe the technical solutions in the embodiments of the present invention more clearly, the accompanying drawings required for describing the embodiments of the present invention are briefly described below, apparently, drawings in the following description are only some embodiments of the invention, for those of ordinary skill in the art, without any creative labor, it is also possible to obtain other drawings based on these drawings.
Fig. 1 is a kind of axial cross-sectional views of airplane parking area shown in an exemplary embodiment of the invention；
Fig. 2 is a kind of top view of airplane parking area shown in an exemplary embodiment of the invention；
Fig. 3 is the structural schematic diagram of the edge ring on a kind of airplane parking area shown in an exemplary embodiment of the invention；
Fig. 4 is a kind of structural schematic diagram of measuring wind speed module shown in an exemplary embodiment of the invention；
Fig. 5 is a kind of schematic cross-section of measuring wind speed module shown in an exemplary embodiment of the invention；
Fig. 6 is a kind of structural schematic diagram of manometric module shown in an exemplary embodiment of the invention.
Following will be combined with the drawings in the embodiments of the present invention, and technical scheme in the embodiment of the invention is clearly and completely described, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, every other embodiment obtained by those of ordinary skill in the art without making creative efforts, shall fall within the protection scope of the present invention.
With reference to the accompanying drawing, the cradle head structure to holder armshaft structure of the present invention and with the holder armshaft structure elaborates, and in the absence of conflict, the feature in following embodiment and embodiment can be combined with each other.
As shown in Figures 1 to 5, the airplane parking area 100 of the embodiment of the present invention includes: pedestal 1, the shutdown platform 2 being installed on pedestal 1, set on the measuring wind speed module 3 shut down on platform 2, and the processing module 4 being electrically connected with measuring wind speed module 3.Wherein, the measuring wind speed module 3 can obtain unmanned vehicle in real time and be formed by airflow function in the airflow value for shutting down platform 2; the processing module 4 is handled acquired airflow value to basis, to determine the unmanned vehicle in the state for shutting down 2 airspace of platform.
In an alternative embodiment, pedestal 1 be equipped with positioning annular distance 11, shut down platform 2 bottom be equipped with positioning annular distance 11 cooperate connecting column 22, by positioning annular distance 11 with connect
Column 22 cooperates, so that shutdown platform 2 be made to be fixed on pedestal 1.Wherein, processing module 4 is set in connecting column or is set between connecting column and positioning annular distance.In a further alternative embodiment, it can also be equipped with connecting column on pedestal 1, shut down the bottom of platform 2 equipped with positioning annular distance, cooperated by positioning annular distance and connecting column, so that shutdown platform 2 be made to be fixed on pedestal 1.Certainly, in other embodiments, pedestal 1 is not limited to this with the assembly for shutting down platform 2, which can also be fixed on pedestal 1 by modes such as welding, bolts.
The shutdown platform 2 is equipped with the identification mark 23 identified for unmanned vehicle, and identification mark 23 is set to the center for shutting down platform 2, and identification mark 23, which can be embedded in, shuts down on platform 2, can also be set to and shut down 2 surface of platform.Wherein, when unmanned vehicle needs to land, identification mark 23 is locked by the filming apparatus of unmanned vehicle, may thereby determine that landing place, and then can accurately land on airplane parking area 100.
Further, airplane parking area 100 further includes the remote control terminal (not shown) communicated to connect with processing module 4, which passes through the data information for obtaining processing module 4, so as to obtain the opposite state for shutting down platform 2 of unmanned vehicle.It can determine whether unmanned vehicle land in the region or unmanned vehicle for shutting down 2 overhead of platform in shutdown platform 2 or the simultaneously dead stick that whether lands.
Wherein, which can be configured as: obtaining the real-time airflow value detected of measuring wind speed module 3, and real-time airflow value is compared with setting airflow value；When real-time airflow value lower than setting airflow value when, determine unmanned vehicle landed in shut down platform 2 or do not reach shut down platform 2 airspace；When real-time airflow value is higher than setting airflow value, determine that unmanned vehicle is in the airspace for shutting down platform 2.In the embodiment, setting airflow value is unmanned vehicle landing when shutting down platform 2, airflow value acquired in measuring wind speed module 3.
In an optional embodiment, which further includes set on the edge ring 21 for shutting down 2 outer rim of platform, and measuring wind speed module 3 is set on outer rim ring 21.The measuring wind speed module 3 is to detect the airflow value for flowing to edge ring 21, wherein the airflow value is blowed to by unmanned vehicle shuts down the airflow value that the air-flow of platform 2 is then spread along the table top for shutting down platform 2 towards edge.In a further alternative embodiment, which can also be set in the plane for shutting down platform 2, and the air-flow of shutdown platform 2 is blowed to directly to detect unmanned vehicle.
Measuring wind speed module 3 be set to edge ring 21 embodiment in, the measuring wind speed module 3 be it is multiple, multiple measuring wind speed modules 3 be set to edge ring 21 on.Wherein, real-time airflow value is processing module 4 according to multiple measuring wind speed modules 3 airflow value detected, calculated average airflow value.In this embodiment, several measuring wind speed modules 3 can be evenly distributed in edge ring 21, it, can be from the measuring wind speed module 3 chosen in several measuring wind speed modules 3 in multiple directions, so as to so that airflow value is more accurate in real time when detecting real-time airflow value.In addition, being equipped with multiple measuring wind speed modules 3 in edge ring 21, it can also be ensured that the stability of real-time airflow value detection, such as: wherein a certain measuring wind speed module 3 after a failure, can replace detecting by controlling adjacent redundancy measuring wind speed module 3.
In the present embodiment; the height of edge ring 21, which is higher than, shuts down platform 2; multiple through-holes 211 are formed in edge ring 21; multiple through-holes 211 are arranged along 21 circular array of edge ring; measuring wind speed module 3 is set in through-hole 211, for detecting from the air quantity for shutting down 2 via through holes 211 of platform outflow edge ring 21.Optionally, measuring wind speed module 3 includes fan and infrared tube unit.Wherein, when fan is by air stream drives, infrared tube unit detects the revolving speed of fan so that it is determined that real-time airflow value on airplane parking area 100.Certainly, in other embodiments, the equipment such as measuring wind speed module 3 or wind speed measuring sensor.
As shown in Fig. 1 to Fig. 3 and Fig. 6; further; the airplane parking area 100 further includes the manometric module 5 that platform 2 is shut down in carrying; manometric module 5 and processing module 4 are electrically connected; to which pressure data detected is sent to processing module 4, so as to determine whether unmanned vehicle lands on shutdown platform 2 after 4 analysis of processing module processing.In an alternative embodiment, shutting down platform 2 may include Support tray and the table top on Support tray, wherein manometric module 5 can be set between Support tray and table top.
Wherein, processing module 4 in the state that real-time airflow value is lower than setting airflow value, when real-time weight value is greater than setting weight value, determines that unmanned vehicle has landed in shutdown platform 2 according to the real-time weight value detected of manometric module 5 compared with setting weight value；When real-time weight value is less than setting magnitude, determine that unmanned vehicle does not reach the airspace for shutting down platform 2.Setting weight value is that unmanned vehicle lands in shutting down platform 2, the weight value of unmanned vehicle acquired in manometric module 5.In the embodiment; by being equipped with the basis of measuring wind speed module 3 on shutting down platform 2 upper; again equipped with manometric module 5; again by measurement weight in the state of being determined as real-time air quantity lower than setting airflow value; the opposite state for shutting down platform 2 of unmanned vehicle is identified and determined to realize from different dimensions; interference caused by when not only eliminating excessive air quantity measurement weight, achievees the purpose that precisely to detect.
In addition; when real-time weight value is less than setting magnitude; when unmanned vehicle is in the airspace for shutting down platform 2; processing module 4 is also used to the airflow value obtained according to air measuring module; the distance between calculate unmanned vehicle and shut down platform 2; it can so provide more unmanned vehicle the opposite specific data for shutting down 2 state of platform, user is allow to accomplish real-time tracking state of flight to unmanned vehicle.
In an alternative embodiment, which is one, and manometric module 5, which is set to, shuts down
The center of platform 2.In a further alternative embodiment, manometric module 5 is multiple, and multiple manometric modules 5, which are set to, shuts down on platform 2；Wherein, real-time weight value is processing module 4 according to multiple manometric modules 5 weight value detected, calculated averaged weight value.Optionally; multiple manometric modules 5 can be distributed evenly in the edge for shutting down platform 2; in the detection process; it can choose wherein several opposite manometric modules 5 to be detected; and remaining manometric module 5 can be used as the spare manometric module 5 of redundancy; with replacement failure ground manometric module 5, the accuracy of detection data thereby may be ensured that.
Wherein, which includes strain pressure transducer, which shuts down the pressure change that platform 2 is born by detection to detect whether unmanned vehicle lands on shutdown platform 2.Certainly, in other embodiments of the invention, which is not limited to strain pressure transducer, can also be can detecte by any other type and shut down the pressure measuring unit that platform 2 bears pressure change.
As shown in Figure 6; in an alternative embodiment; the manometric module 5 includes collet 51, the strain pressure block (not shown) on collet, the foil gauge 53 being oppositely arranged with strain pressure block and the upper mounted plate 54 on foil gauge, and upper mounted plate 54 is to affixed with shutdown platform 2.Wherein, when unmanned vehicle landing is when shutting down platform 2, by the determining real-time weight value shut down on platform 2 of the displacement of 53 relative strain pressure block of foil gauge, i.e. the manometric module 5 is strain beam type pressure sensor.
In a further alternative embodiment, which can also strain pressure sensor for strain tubular type, and the elastic sensing element which strains pressure sensor is thin-walled cylinder closed at one end, and the other end is connect with flange with system under test (SUT).2 or 4 foil gauges are posted on barrel, wherein half is attached to solid section as temperature-compensating plate, the other half is answered as measurement
Become piece.The full bridge circuit of 4 foil gauge Compositional balances when not having pressure；When pressure acts on inner cavity, cylinder is deformed into " dolioform ", makes electric bridge disequilibrium, output and pressure at the voltage of certain relationship.Tested pressure conversion can also be transmitted on strain tube using piston for power or be transmitted by the diaphragm of vertical chain shape by measuring pressure by this sensor.
In a further alternative embodiment, the manometric module 5 can also strain pressure sensor for diaphragm type, the elastic sensing element that the diaphragm type strains pressure sensor is the fixed circular metal flat diaphragm in periphery, when diaphragm stress deformation, radial strain and tangential strain reach positive maximum value at center, and edge radial strain reaches negative maximum value, tangential strain zero.Therefore often two foil gauges are attached to respectively at positive and negative maximum strain, and are connected into the half-bridge circuit of adjacent bridge arm to obtain larger sensitivity and temperature compensation function.Wherein, can then maximally utilise the strain effects of diaphragm using round foil strain gauge, this sensor it is non-linear more significant.
In a further alternative embodiment, which can also strain pressure sensor for combined type, and the elastic sensing element in combined type strain pressure sensor can be divided into primary element and elastic strain element.Pressure conversion is transmitted to elastic strain element for power and strains most sensitive position by primary element, and foil gauge is then attached at the maximum strain of elastic strain element.Wherein, primary element includes diaphragm, bellows, bellows, Bourdon tube etc., elastic strain element include cantilever beam, fixed beam,Ellbeam, annular girder, thin wall cylinder etc..A variety of patterns can be needed to be combined into according to different between them.
Certainly, strain pressure transducer is not limited to the type of above-described embodiment, and other structures or combination also should belong to strain pressure transducer of the invention by the survey pressure mode of strain-type.
Airplane parking area of the invention is equipped with air measuring module on shutting down platform, passes through air measuring
Module airflow value detected can accurately judge that unmanned vehicle has landed in the shutdown platform or whether in the airspace for shutting down platform.Further, it is additionally provided with manometric module on airplane parking area of the invention, by manometric module pressure value detected, can accurately judges whether unmanned vehicle lands in shutdown platform.The present invention passes through the common detection of air measuring module and manometric module, may be implemented that state of the unmanned vehicle with respect to airplane parking area is identified and determined from different dimensions.
Those skilled in the art after considering the specification and implementing the invention disclosed here, will readily occur to other embodiments of the present invention.This application is intended to cover any variations, uses, or adaptations of the invention, these variations, uses, or adaptations follow general principle of the invention and including the undocumented common knowledges or conventional techniques in the art of the present invention.The description and examples are only to be considered as illustrative, and true scope and spirit of the invention are pointed out by claims hereof.
It should be understood that the present invention is not limited to the precise structure already described above and shown in the accompanying drawings, and various modifications and changes may be made without departing from the scope thereof.The scope of the present invention is limited only by the attached claims.
Claims (14)
- A kind of airplane parking area characterized by comprising pedestal, the shutdown platform being installed on the pedestal, the measuring wind speed module on the shutdown platform, and the processing module being electrically connected with the measuring wind speed module；Wherein, the processing module is configured as: obtaining the measuring wind speed module real-time airflow value detected, and the real-time airflow value is compared with setting airflow value；When the real-time airflow value is lower than the setting airflow value, determine that unmanned vehicle has landed in the shutdown platform or do not reached the airspace for shutting down platform；When the real-time airflow value is higher than the setting airflow value, determine that the unmanned vehicle is in the airspace for shutting down platform.
- Airplane parking area according to claim 1, which is characterized in that the airplane parking area further includes set on the edge ring for shutting down platform, and the measuring wind speed module is set on the outer rim ring.
- Airplane parking area according to claim 2, which is characterized in that the measuring wind speed module be it is multiple, multiple measuring wind speed modules be set to the edge ring on；Wherein, the real-time airflow value is the processing module according to multiple measuring wind speed module airflow values detected, calculated average airflow value.
- Airplane parking area according to claim 3; it is characterized in that; the height of the edge ring is higher than the shutdown platform; multiple through-holes are formed in the edge ring; multiple through-holes are arranged along the edge ring circular array; the measuring wind speed module is set in the through-hole, for detecting the air quantity for flowing out the edge ring through the through-hole from the shutdown platform.
- Airplane parking area according to claim 1, which is characterized in that the measuring wind speed module includes fan and infrared tube unit；Wherein, when the fan is by air stream drives, institute It states infrared tube unit and detects the revolving speed of the fan so that it is determined that real-time airflow value on the airplane parking area.
- Airplane parking area according to claim 1, which is characterized in that the pedestal is equipped with positioning annular distance, and the bottom for shutting down platform is equipped with the connecting column with the positioning annular distance cooperation；Wherein, the processing module is set in the connecting column or is set between the connecting column and the positioning annular distance.
- Airplane parking area according to claim 1, which is characterized in that the airplane parking area further includes carrying the manometric module for shutting down platform, and the manometric module and the processing module are electrically connected；Wherein, the processing module is according to the manometric module real-time weight value detected compared with setting weight value; in the state that the real-time airflow value is lower than the setting airflow value; when the real-time weight value is greater than the setting weight value, determine that unmanned vehicle has landed in the shutdown platform；When the real-time weight value is less than the setting magnitude, determine that the unmanned vehicle does not reach the airspace for shutting down platform.
- Airplane parking area according to claim 7; it is characterized in that; when the real-time weight value is less than the setting magnitude, the processing module is also used to the airflow value obtained according to the air measuring module, calculates the distance between the unmanned vehicle and the shutdown platform.
- Airplane parking area according to claim 7, which is characterized in that the manometric module is one, and the manometric module is set to the center for shutting down platform.
- Airplane parking area according to claim 7, which is characterized in that the manometric module be it is multiple, multiple manometric modules be set to the shutdown platform on；Wherein, the real-time weight value is the processing module according to multiple manometric module weight values detected, is calculated Averaged weight value.
- Airplane parking area according to claim 7, which is characterized in that the manometric module includes strain pressure transducer.
- Airplane parking area according to claim 11; it is characterized in that; the manometric module includes collet, the strain pressure block on the collet, the foil gauge being oppositely arranged with the strain pressure block and the upper mounted plate on the foil gauge, and fixed plate is to affixed with shutdown platform；Wherein, when unmanned vehicle landing is when the shutdown platform, pass through the relatively described strain pressure block of the foil gauge is displaced the real-time weight value determined on the shutdown platform.
- Airplane parking area according to claim 1, which is characterized in that the airplane parking area further includes the remote control terminal with processing module communication connection, to obtain the relatively described state for shutting down platform of the unmanned vehicle.
- Airplane parking area according to claim 1, which is characterized in that the platform of shutting down is equipped with the identification mark identified for the unmanned vehicle, and the identification mark is set to the center for shutting down platform.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720506825.XU CN207775740U (en) | 2017-05-08 | 2017-05-08 | Airplane parking area |
| CN201720506825X | 2017-05-08 | ||
| PCT/CN2017/090973 WO2018205379A1 (en) | 2017-05-08 | 2017-06-30 | Tarmac |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109891030A true CN109891030A (en) | 2019-06-14 |
| CN109891030B CN109891030B (en) | 2021-06-25 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720506825.XU Expired - Fee Related CN207775740U (en) | 2017-05-08 | 2017-05-08 | Airplane parking area |
| CN201780066296.9A Active CN109891030B (en) | 2017-05-08 | 2017-06-30 | Parking apron |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720506825.XU Expired - Fee Related CN207775740U (en) | 2017-05-08 | 2017-05-08 | Airplane parking area |
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| CN (2) | CN207775740U (en) |
| WO (1) | WO2018205379A1 (en) |
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|---|---|---|---|---|
| CN207775740U (en) * | 2017-05-08 | 2018-08-28 | 深圳市大疆创新科技有限公司 | Airplane parking area |
| CN109178338A (en) * | 2018-09-03 | 2019-01-11 | 送飞实业集团有限公司 | A kind of helicopter auto cleaning system |
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2017
- 2017-05-08 CN CN201720506825.XU patent/CN207775740U/en not_active Expired - Fee Related
- 2017-06-30 WO PCT/CN2017/090973 patent/WO2018205379A1/en active Application Filing
- 2017-06-30 CN CN201780066296.9A patent/CN109891030B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2012154075A (en) * | 2011-01-25 | 2012-08-16 | Aero Facility Kk | Heliport with lightning protection |
| CN204228737U (en) * | 2014-10-23 | 2015-03-25 | 黄守瑜 | The wind speed measuring device of agricultural depopulated helicopter |
| CN204676442U (en) * | 2015-04-09 | 2015-09-30 | 浙江圣翔机械有限公司 | A kind of lightweight energy-absorbing damping apron |
| CN205840453U (en) * | 2016-07-22 | 2016-12-28 | 国网电力科学研究院武汉南瑞有限责任公司 | UAV Intelligent storehouse |
| CN106527455A (en) * | 2017-01-03 | 2017-03-22 | 北京博瑞空间科技发展有限公司 | UAV landing control method and device |
| CN207775740U (en) * | 2017-05-08 | 2018-08-28 | 深圳市大疆创新科技有限公司 | Airplane parking area |
Also Published As
| Publication number | Publication date |
|---|---|
| CN207775740U (en) | 2018-08-28 |
| CN109891030B (en) | 2021-06-25 |
| WO2018205379A1 (en) | 2018-11-15 |
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