CN108910033A - The long-range manned aerodone of individual and its manufacturing method based on electronic unmanned air vehicle technique - Google Patents
The long-range manned aerodone of individual and its manufacturing method based on electronic unmanned air vehicle technique Download PDFInfo
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- CN108910033A CN108910033A CN201810640663.8A CN201810640663A CN108910033A CN 108910033 A CN108910033 A CN 108910033A CN 201810640663 A CN201810640663 A CN 201810640663A CN 108910033 A CN108910033 A CN 108910033A
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- aerodone
- range
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- manned
- electronic
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
- B64C31/02—Gliders, e.g. sailplanes
- B64C31/024—Gliders, e.g. sailplanes with auxiliary power plant
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
Abstract
The long-range manned aerodone of the individual that the present invention relates to a kind of based on electronic unmanned air vehicle technique includes aircraft assembly, electronic equipment and software systems.Wherein aircraft assembly includes the aircraft cockpit module being arranged on fuselage, cockpit hatchcover and undercarriage, further includes for controlling the wing module of airplane motion, shrouded propeller module, empennage module, vertical fin module, control wing module and shrouded propeller cover board.The present invention also proposes a kind of manufacturing method of long-range manned aerodone of the individual based on electronic unmanned air vehicle technique, including：The design drawing of unmanned plane and CAD model data are converted into CAM data and imported into 3D printer, and the fabric swatch data of electronic circuitry are imported into circuit laminator；The shell of electronic manned long-range solar energy aerodone is printed, and makes associated electronic circuits, and relevant part is installed；Nobody is carried out to personal long-range manned solar energy aerodone to take a flight test；Carry to personal long-range manned solar energy aerodone that dummy takes a flight test and true man take a flight test.
Description
Technical field
The present invention relates to aerodone fields, carry particularly with regard to a kind of individual based on electronic unmanned air vehicle technique is long-range
People's aerodone and its manufacturing method.
Background technique
With the technology of related flight equipment it is improved day by day and it is related manufacture production cost decline, unmanned air vehicle technique is
It is widely spread in multiple industries, such as fields such as aerial mapping, disaster area search, agricultural production and logistics express deliveries.
In above-mentioned many application fields, the portable weight of object of unmanned plane is continuously increased, or even close to the weight of normal adult.
Meanwhile the single voyage of unmanned plane also constantly extends.For example, formally being thrown along the rich long endurance shipping unmanned plane of large size at present
Enter into logistics service, the goods and materials that can carry suitable weight carry out fixed point delivery.
However, on the one hand controlling in view of the application scenarios and production cost of unmanned plane itself, its own can not have any
For the safety measure of carrying personnel.This to apply the portion of techniques in unmanned plane, especially to extension flight equipment
Technology in terms of the manufacturing cost of cruise duration and flight equipment, can not all be grafted directly on manned aerodone.On the other hand,
For to carrying personnel safety guarantee etc. the considerations of, the cost of manned aerodone itself is high；And manned aerodone
Many restrictions requirement is proposed to itself cruise duration and scope of application etc..Above-mentioned various limitations are so that manned gliding
Machine distance, which is widely applied, still quite remote distance.
Summary of the invention
The present invention provides a kind of personal long-range manned aerodone and its manufacturing method based on electronic unmanned air vehicle technique, passes through
The intermediate manufacture link of aerodone is improved, is obtained under the premise of keeping aerodone performance, reduce aerodone manufacture at
This technical effect.
Technical solution of the present invention first aspect is a kind of long-range manned aerodone of the individual based on electronic unmanned air vehicle technique,
It includes aircraft assembly, electronic equipment and software systems.Wherein aircraft assembly include the aircraft cockpit module being arranged on fuselage,
Cockpit hatchcover and undercarriage further include for controlling the wing module of airplane motion, shrouded propeller module, empennage module, hanging down
Tail module, control wing module and shrouded propeller cover board.
Further, the electronic equipment includes：Brushless motor, battery, solar panels, GPS device, gyroscope, steering engine,
Radio receiver, satellite phone；Respectively with the brushless motor, battery, solar panels, GPS device, gyroscope, steering engine, nothing
The airborne computer that line electricity receiver is connected with satellite phone；And the seat console being connect with the airborne computer, for driving
The person's of sailing operation.
Further, the software systems include：Navigation software, automatic Flight Control Software, radio reception end software
With satellite phone software.
Technical solution of the present invention second aspect is a kind of long-range manned aerodone of the individual based on electronic unmanned air vehicle technique
Manufacturing method.It the described method comprises the following steps：A, the design drawing of unmanned plane and CAD model data are converted into CAM number
According to importeding into 3D printer, and the fabric swatch data of electronic circuitry are imported into circuit laminator；B, it is beaten in 3D printer
The shell of electronic manned long-range solar energy aerodone is printed, and makes associated electronic circuits, and the relevant part of installation；C, to base
Nobody is carried out in the long-range manned solar energy aerodone of the individual of electronic unmanned air vehicle technique to take a flight test to complete verifying work；D, to being based on
The long-range manned solar energy aerodone of individual of electronic unmanned air vehicle technique successively carries out carrying after dummy takes a flight test and take a flight test with true man, and investment makes
With.
Further, the step A includes：Before data imported into 3D printer and circuit laminator, verify data
Integrality.The integrality of above-mentioned data may include the edge detection of model (for example whether being section, crack and/or slickness
Defect).
Further, the step B includes：It integrally prints in 3D printer based on the remote of electronic unmanned air vehicle technique
The shell and skeleton of the manned solar energy aerodone of journey, and print relevant electronic circuit mainboard.
Further, the step C includes：By the long-range solar energy aerodone of individual based on electronic unmanned air vehicle technique on ground
It is travelled on face, is driven to the airport in countryside, after obtaining relevant license, start aircraft, and open the long-range sun on ground
The remote controler of energy aerodone, takes a flight test, the overall performance of solar energy aerodone is verified by taking a flight test, which includes
Flight stability, safety, voyage time, all-weather flight ability and remote control distance.
Further, the step D includes：To the long-range manned solar energy aerodone of individual based on electronic unmanned air vehicle technique
It carries people to fly, includes but is not limited to voyage data, operating characteristics data, the flexible performance of aircraft by airborne computer record
Data, aircraft takeoffs and landings performance data and all-weather flight performance data.
Beneficial effects of the present invention are：By improveing the existing structure and manufacturing method of personal long-range manned aerodone,
Under the premise of the existing performance and safety coefficient that keep personal long-range aerodone, the production system of personal long-range manned aerodone is reduced
Cause this.
Detailed description of the invention
Fig. 1 show the top view of aerodone one embodiment according to the present invention；
Fig. 2 show the front view of aerodone one embodiment according to the present invention；
Fig. 3 show the side view of aerodone one embodiment according to the present invention；
Fig. 4 show the electronic device block diagram of aerodone according to the present invention；
Fig. 5 show the block diagram of the software systems of aerodone according to the present invention；
Fig. 6 show the overview flow chart of the manufacturing method of aerodone according to the present invention.
Specific embodiment
It is carried out below with reference to technical effect of the embodiment and attached drawing to design of the invention, specific structure and generation clear
Chu, complete description, to be completely understood by the purpose of the present invention, scheme and effect.Different embodiments as disclosed hereinafter
It is for realizing the different characteristic of provided theme.Component and the specific example of configuration are as described below to simplify the application.
It should be noted that in the absence of conflict, the features in the embodiments and the embodiments of the present application can be combined with each other.It is attached
The identical appended drawing reference used everywhere in figure indicates the same or similar part.Shown component, object and module in attached drawing
Quantity, shape and size only as illustrative reference, not as the limitation to the application.
It should be noted that unless otherwise specified, when a certain feature referred to as " fixation ", " connection " are in another feature,
It can directly fix, be connected to another feature, and can also fix, be connected to another feature indirectly.In addition, this
The descriptions such as the upper and lower, left and right used in open are only the mutual alignment pass relative to each component part of the disclosure in attached drawing
For system.The "an" of used singular, " described " and "the" are also intended to including most forms in the disclosure, are removed
Non- context clearly expresses other meaning.In addition, unless otherwise defined, all technical and scientific terms used herein
It is identical as the normally understood meaning of those skilled in the art.Term used in the description is intended merely to describe herein
Specific embodiment is not intended to be limiting of the invention.Term as used herein "and/or" includes one or more relevant
The arbitrary combination of listed item.
It will be appreciated that though various elements, but this may be described using term first, second, third, etc. in the disclosure
A little elements should not necessarily be limited by these terms.These terms are only used to for same type of element being distinguished from each other out.For example, not departing from
In the case where disclosure range, first element can also be referred to as second element, and similarly, second element can also be referred to as
One element.The use of provided in this article any and all example or exemplary language (" such as ", " such as ") is intended merely to more
Illustrate the embodiment of the present invention well, and unless the context requires otherwise, otherwise the scope of the present invention will not be applied and be limited.
With reference to shown in Fig. 1, Fig. 2 and Fig. 3, disclosed one or more embodiments according to the present invention, based on it is electronic nobody
The long-range manned aerodone of the individual of machine technology includes aircraft assembly 10, electronic equipment 20 and software systems 30.
Wherein aircraft assembly 10 includes aircraft cockpit module 11, cockpit hatchcover 18 and the undercarriage 17 being arranged on fuselage,
It further include for controlling the wing module 12 of airplane motion, shrouded propeller module 13, empennage module 14, vertical fin module 15, control
Wing module 16 processed and shrouded propeller cover board 19.
As shown in figure 4, the electronic equipment 20 includes：Brushless motor 21, battery 22, solar panels 23, GPS device 24,
Gyroscope 25, steering engine 26, radio receiver 27, satellite phone 28；Respectively with the brushless motor 21, battery 22, solar energy
The airborne computer 29 that plate 23, GPS device 24, gyroscope 25, steering engine 26, radio receiver 27 and satellite phone 28 connect；With
And the seat console 291 being connect with the airborne computer 29, it operates and positions for driver.
As shown in figure 5, the software systems 30 include：Navigation software 31, automatic Flight Control Software 32, radio reception
Hold software 33 and satellite phone software 34.
As shown in fig. 6, the method for manufacturing aerodone according to the present invention includes the following steps：
A, the design drawing of unmanned plane and CAD model data are converted into CAM data and imported into 3D printer, and will be electric
The fabric swatch data of sub-circuit figure imported into circuit laminator；
B, the shell of electronic manned long-range solar energy aerodone is printed in 3D printer, and makes associated electronic circuits,
And relevant part is installed；
C, nobody is carried out to the long-range manned solar energy aerodone of individual based on electronic unmanned air vehicle technique to take a flight test, complete verifying
Work；
D, it carries out load dummy to the long-range manned solar energy aerodone of individual based on electronic unmanned air vehicle technique to take a flight test, then again
It carries out true man to take a flight test, then come into operation.
In step, in the actual operation process implementation process is as follows.Of the production based on electronic unmanned air vehicle technique
The conceptual schematic drawing of the long-range manned solar energy aerodone of people, and carry out relevant verifying and discuss, after completing verifying work, use
CAD software makes the three-dimensional CAD model of long-range manned solar energy aerodone, and designs electronic circuitry, and according to design scheme
Purchase relevant auxiliary component, such as navigation module, instrumentation module, remote control module, servomechanism module, hinge module, brushless electricity
Machine 21, battery 22,22 plate of solar battery, display screen, wireless transmitter and receiver etc..
In stepb, in the actual operation process implementation process is as follows.Printing is based on electronic nothing in 3D printer
The shell and skeleton of the long-range manned solar energy aerodone of man-machine technology, and relevant electronic circuit mainboard is printed, it is carried to be long-range
People's solar energy aerodone installs each relevant module, completes assembly working.
In step C, implementation process in the actual operation process is as follows.By the individual based on electronic unmanned air vehicle technique
Long-range solar energy aerodone travels on the ground, is driven to the airport in countryside, after obtaining relevant license, starts aircraft,
And the remote controler of the long-range solar energy aerodone on ground is opened, it takes a flight test, the phase of solar energy aerodone is verified by taking a flight test
Pass performance, stability, safety, voyage, all-weather capability, night flying capability, remote control distance etc. carry out comprehensive test
Card, each classification examination in 100 hours, by completing verifying work after all classifications.
In step D, in the actual operation process implementation process is as follows.To the individual based on electronic unmanned air vehicle technique
Long-range manned solar energy aerodone carries people to fly, and Aviatrix and aircraft enter airport, and Aviatrix wears the helmet and parachute,
Into aircraft, and start aircraft, take a flight test, complete the verifying work of manned part, such as voyage, operating characteristics, aircraft is flexible
Performance, aircraft takeoffs and landings performance, round-the-clock performance wait related classification, and each classification 100 hours enters formally used after the completion
Journey.
The above, only presently preferred embodiments of the present invention, the invention is not limited to above embodiment, as long as
It reaches technical effect of the invention with identical means, all within the spirits and principles of the present invention, any modification for being made,
Equivalent replacement, improvement etc., should be included within the scope of the present invention.Its technical solution within the scope of the present invention
And/or embodiment can have a variety of different modifications and variations.
Claims (9)
1. a kind of long-range manned aerodone of individual based on electronic unmanned air vehicle technique, which is characterized in that including aircraft assembly (10),
Electronic equipment (20) and software systems (30), wherein aircraft assembly (10) includes the aircraft cockpit module being arranged on fuselage
(11), cockpit hatchcover (18) and undercarriage (17) further include for controlling the wing module (12) of airplane motion, shrouded propeller
Module (13), empennage module (14), vertical fin module (15), control wing module (16) and shrouded propeller cover board (19).
2. the long-range manned aerodone of the individual according to claim 1 based on electronic unmanned air vehicle technique, which is characterized in that institute
Stating electronic equipment (20) includes：
Brushless motor (21), battery (22), solar panels (23), GPS device (24), gyroscope (25), steering engine (26), radio
Receiver (27), satellite phone (28)；
Respectively with the brushless motor (21), battery (22), solar panels (23), GPS device (24), gyroscope (25), steering engine
(26), the airborne computer (29) of radio receiver (27) and satellite phone (28) connection；And
The seat console (291) connecting with the airborne computer (29) is operated for driver.
3. the long-range manned aerodone of the individual according to claim 1 based on electronic unmanned air vehicle technique, which is characterized in that institute
Stating software systems (30) includes：It navigation software (31), automatic Flight Control Software (32), radio reception end software (33) and defends
Star phone software (34).
4. a kind of manufacturing method of the long-range manned aerodone of individual based on electronic unmanned air vehicle technique, which is characterized in that the side
Method includes the following steps：
A, the design drawing of unmanned plane and CAD model data are converted into CAM data and imported into 3D printer, and electronics is electric
The fabric swatch data of road figure imported into circuit laminator；
B, the shell of electronic manned long-range solar energy aerodone is printed in 3D printer, and makes associated electronic circuits, and
Relevant part is installed；
C, nobody is carried out to the long-range manned solar energy aerodone of individual based on electronic unmanned air vehicle technique to take a flight test to complete verifying work
Make；
D, it successively carries out carrying dummy to the long-range manned solar energy aerodone of individual based on electronic unmanned air vehicle technique to take a flight test and true man
After taking a flight test, come into operation.
5. according to the method described in claim 4, it is characterized in that, the step A includes：
Before data imported into 3D printer and circuit laminator, the integrality of verify data.
6. according to the method described in claim 4, it is characterized in that, the step B includes：
Integrally printed in 3D printer the long-range manned solar energy aerodone based on electronic unmanned air vehicle technique shell and
Skeleton, and print relevant electronic circuit mainboard.
7. according to the method described in claim 4, it is characterized in that, the step C includes：
The long-range solar energy aerodone of individual based on electronic unmanned air vehicle technique is travelled on the ground, is driven to the machine in countryside
, after obtaining relevant license, start aircraft, and open the remote controler of the long-range solar energy aerodone on ground, take a flight test, leads to
Cross and take a flight test to verify the overall performance of solar energy aerodone, the overall performance include flight stability, safety, the voyage time,
All-weather flight ability and remote control distance.
8. according to the method described in claim 4, it is characterized in that, the step D includes：
It carries people to fly to the long-range manned solar energy aerodone of individual based on electronic unmanned air vehicle technique, passes through airborne computer
(29) voyage data, operating characteristics data, the flexible performance data of aircraft, aircraft takeoffs and landings performance data and all-weather flight are recorded
It can data.
9. a kind of individual based on electronic unmanned air vehicle technique that the method by as described in any one of claim 4 to 8 manufactures
Long-range manned aerodone.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810640663.8A CN108910033A (en) | 2018-06-21 | 2018-06-21 | The long-range manned aerodone of individual and its manufacturing method based on electronic unmanned air vehicle technique |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201810640663.8A CN108910033A (en) | 2018-06-21 | 2018-06-21 | The long-range manned aerodone of individual and its manufacturing method based on electronic unmanned air vehicle technique |
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| CN108910033A true CN108910033A (en) | 2018-11-30 |
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