CN110015398A - A kind of single aircraft based on the analysis of real-time climatic data - Google Patents
A kind of single aircraft based on the analysis of real-time climatic data Download PDFInfo
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- CN110015398A CN110015398A CN201910178490.7A CN201910178490A CN110015398A CN 110015398 A CN110015398 A CN 110015398A CN 201910178490 A CN201910178490 A CN 201910178490A CN 110015398 A CN110015398 A CN 110015398A
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- 238000004458 analytical method Methods 0.000 title claims abstract description 16
- 230000001681 protective effect Effects 0.000 claims abstract description 14
- 238000012545 processing Methods 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 2
- 230000006378 damage Effects 0.000 abstract description 15
- 208000027418 Wounds and injury Diseases 0.000 abstract description 7
- 238000005299 abrasion Methods 0.000 abstract description 6
- 208000014674 injury Diseases 0.000 abstract description 6
- 230000000452 restraining effect Effects 0.000 abstract description 3
- 238000013461 design Methods 0.000 description 7
- 238000001514 detection method Methods 0.000 description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 6
- 238000007405 data analysis Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 241001269238 Data Species 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 230000001568 sexual effect Effects 0.000 description 2
- 239000000443 aerosol Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 238000013500 data storage Methods 0.000 description 1
- 230000005684 electric field Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000010365 information processing Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000003595 mist Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000001869 rapid Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 239000004575 stone Substances 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/06—Helicopters with single rotor
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Geophysics And Detection Of Objects (AREA)
Abstract
The invention discloses a kind of single aircrafts based on the analysis of real-time climatic data; including main body; it further include protective device and guiding device and protective device; the main body includes body shell and bracket and pedal, and the protective device includes fixed block, and the fixed block is located at the top of pedal; the top surface of the fixed block is fixedly connected with rubber pad; the bottom surface of the fixed block is connected with inner tube set, and the bottom of said inner tube set connects restraining position ring block, and the lower section of said inner tube set is connected with fixing seat；By designing the fixed block etc. for being mounted with to be located at the top of pedal, non-skid property can be promoted, convenient for increasing the stability between user of service and pedal, solves existing single aircraft, due to being not provided with the devices such as fixed block, and the non-slip mat abrasion of pedal surface is very fast, after long-time service, user of service is in boarding, the problem of foot may slide in pedal surface, staff is caused to be likely to occur unexpected injury.
Description
Technical field
The invention belongs to aircraft technology fields, and in particular to a kind of single aircraft based on the analysis of real-time climatic data.
Background technique
Weather aircraft can carry out atmosphere data analysis by the processing data information case at top, be for detection meteorological element,
Weather phenomenon, Atmospheric processes and weather modification and the general aviation aircraft for designing equipment, using aircraft as observation platform to atmosphere
Detected, some special meteorological datas can be provided for daily weather forecast and special meteorological planning of experiments, detection it is interior
Hold mainly including the conventional meteorological element of 1. temperature, pressure, humidity, wind etc.；2. various clouds, mist, precipitation physical parameter (nuclei of condensation,
Sexual intercourse drop-size distribution, hail spectrum, ice-nucleus number, water content, cloud internal electric field, carrying capacity etc.)；3. atmospheric turbulance, atmospheric electricity, the gas of atmosphere at
Point and aerosol；4. with the sexual intercourse within the scope of several hundred kilometers around airborne weather radar and meteorological doppler radar, wind, rapids
Stream；5. add up water content with microwave radiometer observation airplane overhead with infrared radiometer detection ground, sea and cloud temperature,
With the weather information around camera shooting course line；6. thrown above and below aircraft sonde survey mission height atmospheric temperature below,
The vertical distribution of pressure, humidity, wind, lower water temperature profiler of throwing measure hundreds of meters of deep ocean temperatures etc., and meteorological aircraft sounding is
It is increasingly automated, most airborne detection systems, no matter from high-speed sampling to data storage and analysis processing, all by computer
Control is completed, and can also provide graphical record or figure punch immediately, some course line detection datas (temperature, humidity, pressure, wind direction,
Longitude and latitude where wind speed and aircraft), it can be sent in real time by aircraft-kusatellite relay system using unit, this is known as
A Sida (ASDAR), this detection system is for making up the rare area of the aerological stations such as ocean, desert, low latitudes and the Southern Hemisphere
Meteorological data plays an important role, and for aircraft flight speed at tens meters per second or more, flight course can cause aircraft ambient atmosphere shape
Therefore state change dramatically to obtain various representational observational datas, is commonly used the methods of wind tunnel simulation experiment, is seen to aircraft
The design and installation for surveying instrument carry out particular study.
Existing single aircraft, due to being not provided with the devices such as fixed block, and the non-slip mat abrasion of pedal surface is very fast, long
After phase use, in boarding, foot may slide user of service in pedal surface, and staff is caused to be likely to occur unexpected injury
The problem of, and existing single aircraft causes the guiding device of aircraft less due to being not provided with the devices such as baffle, so that
The air turbulence in outside has certain influence to aircraft flight speed, in some instances it may even be possible to the problem of influencing oil consumption, while existing list
People's aircraft, due to being not provided with the devices such as raised plate, in aircraft landing, the bottom of bracket there may be rubble, lead to rubble
The problem of bottom surface of damage bracket may be pressed against, thus it is proposed that a kind of single aircraft based on the analysis of real-time climatic data.
Summary of the invention
The purpose of the present invention is to provide a kind of single aircrafts based on the analysis of real-time climatic data, to solve above-mentioned background
Existing single aircraft is proposed in technology, due to being not provided with the devices such as fixed block, and the non-slip mat abrasion of pedal surface is very fast,
After long-time service, in boarding, foot may slide user of service in pedal surface, and staff is caused to be likely to occur accidental wound
Harmful problem, and existing single aircraft causes the guiding device of aircraft less, makes due to being not provided with the devices such as baffle
Outside air turbulence, have certain influence to aircraft flight speed, in some instances it may even be possible to the problem of influencing oil consumption, while existing
Single aircraft, due to being not provided with the devices such as raised plate, in aircraft landing, the bottom of bracket there may be rubble, cause broken
Stone may press against the problem of bottom surface of damage bracket.
To achieve the above object, the invention provides the following technical scheme: it is a kind of based on real-time climatic data analysis one
Aircraft, including main body, further include protective device and guiding device and protective device, and the main body includes body shell and bracket
And pedal, the protective device include fixed block, the fixed block is located at the top of pedal, and the top surface of the fixed block is fixed
It is connected with rubber pad, the bottom surface of the fixed block is connected with inner tube set, and the bottom of said inner tube set connects restraining position ring block, described interior
It is connected with fixing seat below pipe sleeve, is fixedly connected with spring on the inside of the fixing seat.
Preferably, the guiding device includes fixed plate and baffle, and the fixed plate and baffle are respectively positioned on body housing
The side of body is connected with fixed rotating shaft on the inside of the baffle, and offers diversion trench on the inside of the baffle, described to lead
It is connected with deflector on the inside of chute, spring one is fixedly connected between the baffle and fixed plate.
Preferably, the protective device includes bracket, and the raised plate is located at the inside of bracket, the top of the raised plate
It is fixedly connected with limit plate, spring two is connected at the top of the limit plate, guide post, institute are fixedly connected on the inside of the bracket
It states and offers guide hole on the inside of limit plate.
Preferably, the main body further includes propeller and gate and rubber pad, the top movable connection of the rubber pad
There is propeller, one end of the body shell is connected with rubber pad, and the top of the body shell is in the one of propeller
Side is provided with processing data information case.
Preferably, the bottom of the body shell is fixedly connected with bracket, is fixedly connected with pedal on the inside of the bracket.
Preferably, said inner tube set be an integral structure with stop collar, and the top surface of the rubber pad offer limit it is recessed
Slot.
Preferably, the fixed block is an integral structure with inner tube set, and said inner tube set and fixing seat and spring phase
Mutually close connection.
Preferably, the baffle is flexibly connected with body shell by fixed rotating shaft, and the deflector and baffle
For integral type connection.
Preferably, the guide post fixation corresponding with the guide hole of the inside of limit plate on the inside of the bracket, and the raised plate
Bottom is connected with non-slip mat.
Preferably, the raised plate is an integral structure with limit plate, and the limit plate and spring two and raised plate
Mutually close connection.
Compared with prior art, the beneficial effects of the present invention are:
(1) fixed block etc. being located at the top of pedal is mounted with by design, non-skid property can be promoted, convenient for increasing user
Stability between member and pedal, when preventing user of service's boarding, foot is slided in pedal surface, leads to user of service's injury
Situation solves existing single aircraft, due to being not provided with the devices such as fixed block, and the non-slip mat abrasion of pedal surface compared with
Fastly, after long-time service, in boarding, foot may slide user of service in pedal surface, and staff is caused to be likely to occur meaning
The problem of outer injury.
(2) baffle etc. being located on the outside of body shell is mounted with by design, convenient for being led for air-flow in flight
Stream, prevents air turbulence, solves existing single aircraft, due to being not provided with the devices such as baffle, cause the water conservancy diversion of aircraft
Device is less, so that the air turbulence in outside, has certain influence to aircraft flight speed, in some instances it may even be possible to influence asking for oil consumption
Topic.
(3) raised plate etc. positioned at frame bottom, the bottom of bracket when convenient for preventing aircraft landing are mounted with by design
There are rubble, rubble may press against the bottom surface of damage bracket, solve existing single aircraft, due to being not provided with the dress such as raised plate
Set, in aircraft landing, the bottom of bracket there may be rubble, cause rubble may press against damage bracket bottom surface the problem of.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is the cross-sectional view of fixed block of the present invention；
Fig. 3 is the cross-sectional view of baffle of the present invention；
Fig. 4 is the cross-sectional view of bracket of the present invention；
Fig. 5 is the structural schematic diagram of raised plate of the present invention；
In figure: 1, propeller；2, fixed plate；3, body shell；4, bracket；5, gate；6, fixed block；7, raised plate；8,
Baffle；9, rubber pad；10, inner tube set；11, fixing seat；12, spring；13, stop collar；14, spring one；15, deflector；16,
Fixed rotating shaft；17, diversion trench；18, guide post；19, spring two；20, limit plate；21, guide hole；22, pedal；23, at data information
Manage case.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Please refer to Fig. 1-Fig. 5, the present invention provides a kind of technical solution: it is a kind of based on real-time climatic data analysis one fly
Machine, including main body, further include protective device and guiding device and protective device, main body include body shell 3 and bracket 4 and
Pedal 22, protective device include fixed block 6, and fixed block 6 is located at the top of pedal 22, and the top surface of fixed block 6 is fixedly connected with rubber
Rubber mat 9, the bottom surface of fixed block 6 are connected with inner tube set 10, and the bottom of inner tube set 10 connects restraining position ring block 13, the lower section of inner tube set 10
It is connected with fixing seat 11, the inside of fixing seat 11 is fixedly connected with spring 12, is mounted with to be located at 22 top of pedal by designing
Fixed block 6 etc. can promote non-skid property, convenient for increasing the stability between user of service and pedal 22, prevent user of service from stepping on
When machine, foot is slided on 22 surface of pedal, solves existing single aircraft, due to being not provided with the devices such as fixed block 6, and steps on
The non-slip mat abrasion on 22 surface of plate is very fast, and after long-time service, for user of service in boarding, foot may be sliding on 22 surface of pedal
The problem of moving, staff caused to be likely to occur unexpected injury.
For the ease of guaranteeing the normal use of guiding device, in the present embodiment, it is preferred that guiding device includes fixed plate 2
With baffle 8, fixed plate 2 and baffle 8 are respectively positioned on the side of body shell 3, and the inside of baffle 8 is connected with fixed rotating shaft
16, and the inside of baffle 8 offers diversion trench 17, the inside of diversion trench 17 is connected with deflector 15, baffle 8 and fixed plate
Spring 1 is fixedly connected between 2, by designing the baffle 8 etc. for being mounted with to be located on the outside of body shell 3, convenient for flying
When, water conservancy diversion is carried out for air-flow, air turbulence is prevented, solves existing single aircraft, due to being not provided with the dresses such as baffle 8
It sets, causes the guiding device of aircraft less, so that the air turbulence in outside, has certain influence to aircraft flight speed, even
The problem of may influencing oil consumption.
For the ease of guaranteeing the normal use of protective device, in the present embodiment, it is preferred that protective device includes bracket 4, convex
Starting board 7 is located at the inside of bracket 4, and the top of raised plate 7 is fixedly connected with limit plate 20, and the top of limit plate 20 is connected with spring
2 19, the inside of bracket 4 is fixedly connected with guide post 18, and the inside of limit plate 20 offers guide hole 21, is mounted with position by design
Raised plate 7 etc. in 4 bottom of bracket, there are rubble, rubble may press against damage branch for the bottom of bracket 4 when convenient for preventing aircraft landing
The bottom surface of frame 4 solves existing single aircraft, due to being not provided with the devices such as raised plate 7, the bracket 4 in aircraft landing
The problem of bottom there may be rubble, cause rubble that may press against the bottom surface of damage bracket 4.
For the ease of guaranteeing the normal use of main body, in the present embodiment, it is preferred that main body further includes propeller 1 and machine
Door 5, the top movable of rubber pad 9 is connected with propeller 1, and the side that the top of body shell 3 is in propeller 1 is provided with data
Information processing case 22.
For the ease of protecting body shell 3, in the present embodiment, it is preferred that the bottom of body shell 3 is fixedly connected with bracket
4, the inside of bracket 4 is fixedly connected with pedal 22.
For the ease of preferably increasing non-skid property, in the present embodiment, it is preferred that inner tube set 10 is integrated with stop collar 13
Formula structure, and the top surface of rubber pad 9 offers limiting groove.
For the ease of increasing the compactness of device, in the present embodiment, it is preferred that fixed block 6 and inner tube set 10 are integral type
Structure, and inner tube set 10 is mutually closely connect with fixing seat 11 and spring 12.
For the ease of guaranteeing the rotation of baffle 8, in the present embodiment, it is preferred that baffle 8 and body shell 3 pass through solid
Determine the flexible connection of shaft 16, and deflector 15 is that integral type is connect with baffle 8.
For the ease of preventing raised plate 7 from misplacing, in the present embodiment, it is preferred that the guide post 18 and limit plate 20 of 4 inside of bracket
Inside guide hole 21 it is corresponding fix, and the bottom of raised plate 7 is connected with non-slip mat.
For the ease of preferably increasing compactness, in the present embodiment, it is preferred that raised plate 7 and limit plate 20 are integral type
Structure, and limit plate 20 is mutually closely connect with spring 2 19 and raised plate 7.
The working principle of the invention and process for using: should be in flight in use, the data information for passing through 3 top of body shell
Treatment box 22 can carry out weather data analysis to air, and then in boarding, user of service can be stepped on foot pedal 22
Machine, foot directly contact with part fixed block 6, so that fixed block 6 drives inner tube set 10 to 11 medial movement of fixing seat, another portion
Then deformation occurs for the fixed block 6 point not contacted with foot, then can limit to foot, prevent foot from sliding, pass through
Design is mounted with to be located at the fixed block 6 etc. at the top of pedal 22, can promote non-skid property, convenient for increase user of service and pedal 22 it
Between stability, when preventing user of service's boarding, foot 22 surface of pedal slide, solve existing single aircraft, due to
The devices such as fixed block 6 are not provided with, and the non-slip mat abrasion on 22 surface of pedal is very fast, after long-time service, user of service is in boarding
When, the problem of foot may slide on 22 surface of pedal, staff is caused to be likely to occur unexpected injury, while in aircraft flight
When, baffle 8 can carry out upward angular adjustment according to the state and wind direction of aircraft, while wind can enter the interior of diversion trench 17
Side, and be discharged by the other end of baffle 8, by designing the baffle 8 etc. for being mounted with to be located on the outside of body shell 3,
Convenient for carrying out water conservancy diversion for air-flow, preventing air turbulence, solve existing single aircraft, led due to being not provided in flight
The devices such as block 8 are flowed, cause the guiding device of aircraft less, so that the air turbulence in outside, there is centainly aircraft flight speed
It influences, in some instances it may even be possible to the problem of influencing oil consumption,, can be by 4 bottom of bracket due to the Section Design of raised plate 7 in aircraft landing
Rubble stirred to two sides, prevent from pressing against the surface of damage bracket 4, when aircraft lands completely, raised plate 7 can be contracted in bracket 4
Inside, by designing the raised plate 7 etc. being mounted with positioned at 4 bottom of bracket, the bottom of bracket 4 is deposited when convenient for preventing aircraft landing
There is rubble, rubble may press against the bottom surface of damage bracket 4, solve existing single aircraft, due to being not provided with the dresses such as raised plate 7
Set, in aircraft landing, the bottom of bracket 4 there may be rubble, cause rubble may press against damage bracket 4 bottom surface the problem of.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (10)
1. a kind of single aircraft based on the analysis of real-time climatic data, including main body, it is characterised in that: further include protective device and
Guiding device and protective device, the main body include body shell (3) and bracket (4) and pedal (22), the protection dress
It sets including fixed block (6), the fixed block (6) is located at the top of pedal (22), and the top surface of the fixed block (6) is fixedly connected with
The bottom surface of rubber pad (9), the fixed block (6) is connected with inner tube set (10), and the bottom of said inner tube set (10) is connected with limit
Ring (13) is connected with fixing seat (11) below said inner tube set (10), is fixedly connected with bullet on the inside of the fixing seat (11)
Spring (12).
2. a kind of single aircraft based on the analysis of real-time climatic data according to claim 1, it is characterised in that: described to lead
Flowing device includes fixed plate (2) and baffle (8), and the fixed plate (2) and baffle (8) are respectively positioned on the one of body shell (3)
Side is connected with fixed rotating shaft (16) on the inside of the baffle (8), and offers diversion trench on the inside of the baffle (8)
(17), it is connected with deflector (15) on the inside of the diversion trench (17), it is fixed between the baffle (8) and fixed plate (2) to connect
It is connected to spring one (14).
3. a kind of single aircraft based on the analysis of real-time climatic data according to claim 1, it is characterised in that: the guarantor
Protection unit includes bracket (4), and the raised plate (7) is located at the inside of bracket (4), is fixedly connected at the top of the raised plate (7)
Have limit plate (20), spring two (19) is connected at the top of the limit plate (20), is fixedly connected on the inside of the bracket (4)
Guide post (18) offers guide hole (21) on the inside of the limit plate (20).
4. a kind of single aircraft based on the analysis of real-time climatic data according to claim 1, it is characterised in that: the master
Body further includes propeller (1) and gate (5) and rubber pad (9), and the top movable of the rubber pad (9) is connected with propeller
(1), one end of the body shell (3) is connected with rubber pad (9), and the top of the body shell (3) is in propeller
(1) side is provided with processing data information case (22).
5. a kind of single aircraft based on the analysis of real-time climatic data according to claim 4, it is characterised in that: the machine
The bottom of body shell (3) is fixedly connected with bracket (4), is fixedly connected with pedal (22) on the inside of the bracket (4).
6. a kind of single aircraft based on the analysis of real-time climatic data according to claim 1, it is characterised in that: in described
Pipe sleeve (10) is an integral structure with stop collar (13), and the top surface of the rubber pad (9) offers limiting groove.
7. a kind of single aircraft based on the analysis of real-time climatic data according to claim 1, it is characterised in that: described solid
Determine block (6) to be an integral structure with inner tube set (10), and said inner tube set (10) and fixing seat (11) and spring (12) are mutual
Close connection.
8. a kind of single aircraft based on the analysis of real-time climatic data according to claim 2, it is characterised in that: described to lead
Stream block (8) is flexibly connected with body shell (3) by fixed rotating shaft (16), and the deflector (15) and baffle (8) are one
The connection of body formula.
9. a kind of single aircraft based on the analysis of real-time climatic data according to claim 3, it is characterised in that: the branch
Guide post (18) fixation corresponding with guide hole (21) of inside of limit plate (20) on the inside of frame (4), and the bottom of the raised plate (7)
It is connected with non-slip mat.
10. a kind of single aircraft based on the analysis of real-time climatic data according to claim 3, it is characterised in that: described
Raised plate (7) is an integral structure with limit plate (20), and the limit plate (20) and spring two (19) and raised plate (7) phase
Mutually close connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910178490.7A CN110015398A (en) | 2019-03-11 | 2019-03-11 | A kind of single aircraft based on the analysis of real-time climatic data |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910178490.7A CN110015398A (en) | 2019-03-11 | 2019-03-11 | A kind of single aircraft based on the analysis of real-time climatic data |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110015398A true CN110015398A (en) | 2019-07-16 |
Family
ID=67189423
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910178490.7A Pending CN110015398A (en) | 2019-03-11 | 2019-03-11 | A kind of single aircraft based on the analysis of real-time climatic data |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110015398A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110171037A1 (en) * | 2008-09-22 | 2011-07-14 | Walter Enthammer | Blade for a turbomachine |
| CN103708029A (en) * | 2014-01-06 | 2014-04-09 | 姚昊 | Light aircraft |
| CN205854475U (en) * | 2016-08-03 | 2017-01-04 | 泛洲科技（北京）有限公司 | Suav |
| CN206623989U (en) * | 2017-03-16 | 2017-11-10 | 肖旺旺 | A kind of field exploration aircraft |
| CN108045570A (en) * | 2018-02-24 | 2018-05-18 | 冯林娟 | A kind of unmanned plane undercarriage of more rotors |
| CN207580157U (en) * | 2017-11-22 | 2018-07-06 | 江西天一航空装备有限公司 | A kind of holder connection device that rises and falls of helicopter |
-
2019
- 2019-03-11 CN CN201910178490.7A patent/CN110015398A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110171037A1 (en) * | 2008-09-22 | 2011-07-14 | Walter Enthammer | Blade for a turbomachine |
| CN103708029A (en) * | 2014-01-06 | 2014-04-09 | 姚昊 | Light aircraft |
| CN205854475U (en) * | 2016-08-03 | 2017-01-04 | 泛洲科技（北京）有限公司 | Suav |
| CN206623989U (en) * | 2017-03-16 | 2017-11-10 | 肖旺旺 | A kind of field exploration aircraft |
| CN207580157U (en) * | 2017-11-22 | 2018-07-06 | 江西天一航空装备有限公司 | A kind of holder connection device that rises and falls of helicopter |
| CN108045570A (en) * | 2018-02-24 | 2018-05-18 | 冯林娟 | A kind of unmanned plane undercarriage of more rotors |
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