CN109592000A - A kind of unmanned helicopter harness installation region design method - Google Patents
A kind of unmanned helicopter harness installation region design method Download PDFInfo
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- CN109592000A CN109592000A CN201811333277.0A CN201811333277A CN109592000A CN 109592000 A CN109592000 A CN 109592000A CN 201811333277 A CN201811333277 A CN 201811333277A CN 109592000 A CN109592000 A CN 109592000A
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- China
- Prior art keywords
- harness
- installation region
- region
- unmanned helicopter
- design
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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
- B64C1/40—Sound or heat insulation, e.g. using insulation blankets
- B64C1/403—Arrangement of fasteners specially adapted therefor, e.g. of clips
- B64C1/406—Arrangement of fasteners specially adapted therefor, e.g. of clips in combination with supports for lines, e.g. for pipes or cables
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G3/00—Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles
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- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Installation Of Indoor Wiring (AREA)
Abstract
The application belongs to electrical harness interconnection field, in particular to a kind of unmanned helicopter harness installation region design method.Include: step 1: subregion being carried out to the installation region of harness (9), the installation region of the harness (9) is specifically divided into: upper mounting plate harness installation region (10), middle layer harness installation region (11), lower layer's harness installation region (12), endpiece harness installation region (13) and exterior strands installation region (14)；Step 2: the design that interconnects is carried out to each region of the installation region of the harness (9)；Step 3: parting surface design is carried out to each region of the installation region of the harness (9).The unmanned helicopter harness installation region design method of the application has fully considered helicopter structure feature and each system demand for interconnection, on the basis of investigating each system requirements comprehensively, a kind of practical, reasonably optimizing, high efficiency unmanned helicopter harness installation region design method are formd.
Description
Technical field
The application belongs to electrical harness interconnection field, in particular to a kind of unmanned helicopter harness installation region design side
Method.
Background technique
Currently, electrical harness interacted system is widely used in large-scale fixed wing aircraft, effectively full machine harness can be carried out
It makes rational planning for and optimization design, realization improves electromagnetic compatibility and complete machine safety to full machine harness management.
But in helicopter field, the country there is no the application of electrical harness interacted system technology.Fly compared to large-scale fixed-wing
Machine, helicopter has the characteristics that installation space is limited, Electro Magnetic Compatibility complexity is high, vibration environment is severe, mutual to electrical harness
The application of connection systems technology brings new challenge.
Thus, it is desirable to have a kind of technical solution overcomes or at least mitigates at least one drawbacks described above of the prior art.
Summary of the invention
There is provided a kind of unmanned helicopter harness installation region design methods for the purpose of the application, to solve the prior art
At least one existing problem.
The technical solution of the application is:
A kind of unmanned helicopter harness installation region design method, comprising:
Step 1: zoning design is carried out to the installation region of harness；
Step 2: the design that interconnects is carried out to each region of the installation region of the harness；
Step 3: parting surface design is carried out to each region of the installation region of the harness.
Optionally, the installation region of the harness is specifically divided into: upper mounting plate harness installation region, middle layer harness installing zone
Domain, lower layer's harness installation region, endpiece harness installation region and exterior strands installation region.
Optionally, middle layer harness installation region includes front platform installation region and rear platform installation region.
Optionally, lower layer's harness installation region includes left main channel installation region and right main channel installation region.
Optionally, in step 2, the design that interconnects is carried out to each region of the installation region of the harness, comprising:
It is opened between upper mounting plate harness installation region and the front platform installation region of middle layer harness installation region
If cable-through hole, opened up between upper mounting plate harness installation region and the rear platform installation region of middle layer harness installation region
Cable-through hole.
Optionally, in step 2, the design that interconnects is carried out to each region of the installation region of the harness, is also wrapped
It includes:
In the left main channel installation region of lower layer's harness installation region and right main channel installation region respectively along course
Open up cable-through hole.
Optionally, in step 3, parting surface design is carried out to each region of the installation region of the harness, comprising:
The first parting surface is designed between endpiece harness and front wiring harness mounting structure.
Optionally, endpiece harness and front harness are attached at first parting surface using separating socket.
Optionally, in step 3, parting surface design is carried out to each region of the installation region of the harness, further includes:
The second parting surface is being designed in exterior strands and machine between wiring harness mounting structure.
Optionally, exterior strands and harness in machine are attached at second parting surface using separating socket.
At least there are following advantageous effects in the application:
The unmanned helicopter harness installation region design method of the application meets complete in conjunction with helicopter overall structure feature
The primary demand of the interconnection of machine harness, installation, while realizing that efficient installation space utilizes, the channel of optimization is planned, reasonable line
Beam installation is fixed.
Detailed description of the invention
Fig. 1 is typical helicopter composition schematic diagram；
Fig. 2 is the unmanned helicopter harness installation region schematic diagram of one embodiment of the application；
Fig. 3 is the unmanned helicopter harness installation region cable-through hole layout of one embodiment of the application；
Wherein:
1- main rotor；2- main reducing gear；3- engine；4- upper mounting plate；5- front platform；The floor 6-；7- rear platform；8- tail
Section；9- harness；10- upper mounting plate harness installation region；The middle layer 11- harness installation region；12- lower layer harness installation region；13- tail
Section harness installation region；14- exterior strands installation region；The first parting surface of 15-；The second parting surface of 16-；The right main channel peace of 17-
Fill region；The left main channel installation region 18-.
Specific embodiment
To keep the purposes, technical schemes and advantages of the application implementation clearer, below in conjunction in the embodiment of the present application
Attached drawing, technical solutions in the embodiments of the present application is further described in more detail.In the accompanying drawings, identical from beginning to end or class
As label indicate same or similar element or element with the same or similar functions.Described embodiment is the application
A part of the embodiment, instead of all the embodiments.The embodiments described below with reference to the accompanying drawings are exemplary, it is intended to use
In explanation the application, and it should not be understood as the limitation to the application.Based on the embodiment in the application, ordinary skill people
Member's every other embodiment obtained without creative efforts, shall fall in the protection scope of this application.Under
Face is described in detail embodiments herein in conjunction with attached drawing.
In the description of the present application, it is to be understood that term " center ", " longitudinal direction ", " transverse direction ", "front", "rear",
The orientation or positional relationship of the instructions such as "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outside" is based on attached drawing institute
The orientation or positional relationship shown is merely for convenience of description the application and simplifies description, rather than the dress of indication or suggestion meaning
It sets or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as protecting the application
The limitation of range.
1 to Fig. 3 the application is described in further details with reference to the accompanying drawing.
The unmanned helicopter harness installation region design method of the application, comprising:
Step 1: subregion is carried out to the installation region of harness 9, the installation region of harness 9 is specifically divided into: upper mounting plate harness peace
Fill region 10, middle layer harness installation region 11, lower layer's harness installation region 12, endpiece harness installation region 13 and outer lines
Beam installation region 14；
Step 2: the design that interconnects is carried out to each region of the installation region of harness 9；
Step 3: parting surface design is carried out to each region of the installation region of harness 9.
Design the target that needs are realized in unmanned helicopter harness installation region
The interconnection and interflow in integral installation region, with to be distributed in harness connection of the full machine everywhere between equipment；Integral installation
The optimization design in region, to provide a kind of efficient electrical harness interacted system scheme；The optimization design of each part installation region,
Such as local installation passage is planned and is fixed.
To realize above-mentioned target, need comprehensively to analyze unmanned helicopter overall structure.
As shown in Figure 1, unmanned helicopter is generally by housing construction, main rotor 1, tail-rotor, main reducing gear 2, engine 3, machine
Carry the composition such as equipment.Unmanned helicopter housing construction generally can be divided into upper mounting plate 4, front platform 5, cabin, floor 6, rear platform 7,
The parts such as endpiece 8, wherein upper mounting plate 4 is generally used for installation main rotor 1, main reducing gear 2,3 equal power device of engine, cabin
It is mainly used for carrying out the installation of all kinds of airborne equipments, fuel tank etc., also can be used as the installation region of equipment component under floor 6.
For the interconnection needs for meeting full electromechanical equipment, full machine equipment position characteristic is considered, in combination with helicopter
Division can be carried out as follows in structure feature, the angle that unmanned helicopter overall structure is installed from electrical harness interacted system:
In a vertical direction, upper, middle, and lower part can be divided into；
By horizontal direction, before, during and after being divided into, four part of endpiece, or it is divided into left and right two parts；
In conjunction with unmanned helicopter overall structure division mode, in the unmanned helicopter harness installation region design side of the application
In one embodiment of method, adopt the following technical scheme that
Firstly, the installation region to harness 9 carries out subregion, it is specifically divided into: upper mounting plate harness installation region 10, middle layer harness
Installation region 11, lower layer's harness installation region 12, endpiece harness installation region 13 and exterior strands installation region 14.Wherein,
Middle layer harness installation region 11 is divided for front platform installation region and rear platform installation region, lower layer's harness installation region 12 is divided
For left main channel installation region 18 and right main channel installation region 17.
Secondly, carrying out the design that interconnects to each region of the installation region of harness 9.To realize that unmanned helicopter is electrical
The interconnection and interflow of harness interacted system installation region, the present embodiment uses a kind of efficient opening approach, in upper mounting plate harness
Cable-through hole is opened up between installation region 10 and the front platform installation region of middle layer harness installation region 11, is installed in upper mounting plate harness
Cable-through hole is opened up between region 10 and the rear platform installation region of middle layer harness installation region 11, before upper mounting plate and middle layer to be provided
Harness interconnecting channels between rear platform；Further, on the left main channel installation region 18 of lower layer's harness installation region 12 and the right side
Main channel installation region 17 opens up cable-through hole along course respectively, and respectively left and right main channel provides harness interconnecting channels.By upper
Design is stated, interconnecting for unmanned helicopter each region of full machine is adequately achieved, condition is provided for harness interconnection, meets and set
Demand for interconnection between standby.
Finally, carrying out parting surface design to each region of the installation region of harness 9.For realize harness efficient installation,
The application designs the first parting surface 15 between endpiece harness and front wiring harness mounting structure, and is connected using separation socket
It connects；The second parting surface 16 is being designed in exterior strands and machine between wiring harness mounting structure simultaneously, is being attached using separation socket,
Guarantee the independence of exterior strands.
By the unmanned helicopter harness installation region design method of above-mentioned the application, unmanned helicopter harness peace is realized
Fill the optimization design in region.It is upper flat this application provides the aperture design between upper mounting plate and front platform, upper mounting plate and rear platform
Platform harness cabling can select most reasonable routing path according to shortest path principle；This application provides front platform lower part harness peaces
Pick-up the optimization design of thread path, can not only meet between front platform or so harness the needs of across wiring, and avoid
The space of front platform is occupied, remains sufficient installation space for the installation of each system equipment.
The unmanned helicopter harness installation region design method of the application has fully considered helicopter structure feature and each
System demand for interconnection forms a kind of practical, reasonably optimizing, high efficiency on the basis of investigating each system requirements comprehensively
Unmanned helicopter harness installation region design method.
The above, the only specific embodiment of the application, but the protection scope of the application is not limited thereto, it is any
Within the technical scope of the present application, any changes or substitutions that can be easily thought of by those familiar with the art, all answers
Cover within the scope of protection of this application.Therefore, the protection scope of the application should be with the scope of protection of the claims
It is quasi-.
Claims (10)
1. a kind of unmanned helicopter harness installation region design method characterized by comprising
Step 1: zoning design is carried out to the installation region of harness (9)；
Step 2: the design that interconnects is carried out to each region of the installation region of the harness (9)；
Step 3: parting surface design is carried out to each region of the installation region of the harness (9).
2. unmanned helicopter harness according to claim 1 installation region design method, which is characterized in that the harness
(9) installation region is specifically divided into: upper mounting plate harness installation region (10), middle layer harness installation region (11), lower layer's harness peace
Fill region (12), endpiece harness installation region (13) and exterior strands installation region (14).
3. unmanned helicopter harness according to claim 2 installation region design method, which is characterized in that the zero line
Beam installation region (11) includes front platform installation region and rear platform installation region.
4. unmanned helicopter harness according to claim 3 installation region design method, which is characterized in that the lower layer line
Beam installation region (12) includes left main channel installation region (18) and right main channel installation region (17).
5. unmanned helicopter harness according to claim 4 installation region design method, which is characterized in that in step 2,
The design that interconnects is carried out to each region of the installation region of the harness (9), comprising:
The front platform installation region of upper mounting plate harness installation region (10) and middle layer harness installation region (11) it
Between open up cable-through hole, the rear platform installation region of upper mounting plate harness installation region and middle layer harness installation region (11)
Between open up cable-through hole.
6. unmanned helicopter harness according to claim 5 installation region design method, which is characterized in that in step 2,
The design that interconnects is carried out to each region of the installation region of the harness (9), further includes:
In the left main channel installation region (18) of lower layer's harness installation region (12) and right main channel installation region (17) point
Cable-through hole is not opened up along course.
7. unmanned helicopter harness according to claim 6 installation region design method, which is characterized in that in step 3,
Parting surface design is carried out to each region of the installation region of the harness (9), comprising:
The first parting surface (15) are designed between endpiece harness and front wiring harness mounting structure.
8. unmanned helicopter harness according to claim 7 installation region design method, which is characterized in that endpiece harness with
Front harness is attached at first parting surface (15) using separation socket.
9. unmanned helicopter harness according to claim 8 installation region design method, which is characterized in that in step 3,
Parting surface design is carried out to each region of the installation region of the harness (9), further includes:
The second parting surface (16) are being designed in exterior strands and machine between wiring harness mounting structure.
10. unmanned helicopter harness according to claim 9 installation region design method, which is characterized in that exterior strands
It is attached at second parting surface (16) using separating socket with harness in machine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811333277.0A CN109592000A (en) | 2018-11-09 | 2018-11-09 | A kind of unmanned helicopter harness installation region design method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811333277.0A CN109592000A (en) | 2018-11-09 | 2018-11-09 | A kind of unmanned helicopter harness installation region design method |
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| Publication Number | Publication Date |
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| CN109592000A true CN109592000A (en) | 2019-04-09 |
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ID=65957113
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811333277.0A Pending CN109592000A (en) | 2018-11-09 | 2018-11-09 | A kind of unmanned helicopter harness installation region design method |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115033986A (en) * | 2022-05-27 | 2022-09-09 | 中国航空工业集团公司沈阳飞机设计研究所 | Comprehensive design method for aircraft wire harness |
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| CN102470924A (en) * | 2009-07-07 | 2012-05-23 | 空中客车营运有限公司 | Method for reducing the installation time of a supply line |
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| CN204391601U (en) * | 2014-08-01 | 2015-06-10 | 南方电网科学研究院有限责任公司 | Photoelectric pod universal system for helicopter inspection |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN115033986A (en) * | 2022-05-27 | 2022-09-09 | 中国航空工业集团公司沈阳飞机设计研究所 | Comprehensive design method for aircraft wire harness |
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Application publication date: 20190409 |