CN109533363A - A kind of unmanned helicopter electrical harness interacted system - Google Patents
A kind of unmanned helicopter electrical harness interacted system Download PDFInfo
- Publication number
- CN109533363A CN109533363A CN201811333393.2A CN201811333393A CN109533363A CN 109533363 A CN109533363 A CN 109533363A CN 201811333393 A CN201811333393 A CN 201811333393A CN 109533363 A CN109533363 A CN 109533363A
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- CN
- China
- Prior art keywords
- harness
- unmanned helicopter
- electrical
- mounting plate
- upper mounting
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
Abstract
The application belongs to electrical harness interconnection field, in particular to a kind of unmanned helicopter electrical harness interacted system.System includes upper mounting plate harness (1), Zuo Tongdao harness (3), right channel harness (2), endpiece harness (4) and exterior strands (5).The upper mounting plate (6) of unmanned helicopter is arranged in the upper mounting plate harness (1)；The left side of the lower layer installation region (7) of unmanned helicopter is arranged in the left channel harness (3)；The right side of the lower layer installation region (7) of unmanned helicopter is arranged in the right channel harness (2)；The endpiece (8) of unmanned helicopter is arranged in the tail end harness (4)；The outside of unmanned helicopter is arranged in the exterior strands (5).The unmanned helicopter electrical harness interacted system of the application fully considers helicopter structure feature, each system demand for interconnection, practical, reasonably optimizing, the installation effectiveness and maintenanceability for improving harness.
Description
Technical field
The application belongs to electrical harness interconnection field, in particular to a kind of unmanned helicopter electrical harness interacted system.
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 electrical harness interacted systems for the purpose of the application, to solve prior art presence
At least one problem.
The technical solution of the application is:
A kind of unmanned helicopter electrical harness interacted system, comprising:
The upper mounting plate of unmanned helicopter is arranged in upper mounting plate harness, the upper mounting plate harness；
The left side of the lower layer installation region of unmanned helicopter is arranged in left channel harness, the left channel harness；
The right side of the lower layer installation region of unmanned helicopter is arranged in right channel harness, the right channel harness；
The endpiece of unmanned helicopter is arranged in endpiece harness, the tail end harness；
The outside of unmanned helicopter is arranged in exterior strands, the exterior strands.
Optionally, harness includes: power supply harness, communication harness, control harness, radio frequency harness.
Optionally, the left channel harness and the right channel harness include three beams harness.
Optionally, the three-beam line is respectively as follows: P harness, M harness, S harness, wherein the P harness be radio frequency harness or
The harness that merges of power supply harness and radio frequency harness, the M harness are communication harness, control harness or communication harness and control harness
Merging harness, the S harness be control harness.
Optionally, radio system and radar system of the P harness from unmanned helicopter.
Optionally, communication system and flight control system of the M harness from unmanned helicopter.
Optionally, fire control system, autoflight system and Flight By Wire system of the S harness from unmanned helicopter
System.
Optionally, it is separated between the exterior strands and internal harness by setting parting surface, wherein internal harness includes
The upper mounting plate harness, the left channel harness, the right channel harness and the endpiece harness.
Optionally, it is separated between the endpiece harness and front harness by the way that parting surface is arranged, wherein the front harness
Including the upper mounting plate harness, the left channel harness, the right channel harness and the exterior strands.
Optionally, it is separated and by the way that parting surface is arranged by separating socket progress between the exterior strands and internal harness
Connection；
It is separated between the endpiece harness and front harness by setting parting surface and is attached by separating socket.
At least there are following advantageous effects in the application:
The unmanned helicopter electrical harness interacted system of the application fully considers helicopter structure feature, the interconnection of each system
Demand, practical, reasonably optimizing, the installation effectiveness and maintenanceability for improving harness.
Detailed description of the invention
Fig. 1 is typical helicopter structure schematic diagram；
Fig. 2 is the unmanned helicopter electrical harness interacted system layout of one embodiment of the application.
Fig. 3 is that the left channel harness of the unmanned helicopter electrical harness interacted system of one embodiment of the application and the right side lead to
Road wire harness schematic.
Wherein:
1- upper mounting plate harness；The right channel harness of 2-；The left channel harness of 3-；4- endpiece harness；5- exterior strands；It is put down on 6-
Platform；7- lower layer installation region；8- endpiece；9-P harness；10-M harness；11-S harness.
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.
As shown in Figure 1, unmanned helicopter generally by housing construction, main rotor, tail-rotor, engine, main reducing gear, airborne set
It is standby to wait composition.The housing construction of unmanned helicopter generally can be divided into the portions such as upper mounting plate 6, cabin, lower layer installation region 7, endpiece 8
Point, wherein upper mounting plate 6 is generally used for installation rotor, engine, main reducing gear equal power device, and cabin is mainly used for carrying out all kinds of
The installation of airborne equipment, fuel tank etc., lower layer installation region 7 also can provide the installation region of equipment component.
To meet the needs of full machine equipment interconnection, this application provides a kind of unmanned helicopter electrical harness interacted systems.
It, can will be complete specifically, consider full machine equipment installation site and its demand for interconnection according to unmanned helicopter design feature
Machine harness divides quinquepartite by structural orientation: upper mounting plate harness 1, Zuo Tongdao harness 3, right channel harness 2, endpiece harness 4 and
Exterior strands 5.Wherein, the upper mounting plate 6 of unmanned helicopter is arranged in upper mounting plate harness 1, and Zuo Tongdao harness setting 3 is gone straight up at nobody
The right side of the lower layer installation region 7 of unmanned helicopter, tail end is arranged in the left side of the lower layer installation region 7 of machine, right channel harness 2
The endpiece 8 of unmanned helicopter is arranged in harness 4, and the outside of unmanned helicopter is arranged in exterior strands 5.Unmanned helicopter electric wire
Beam includes: power supply harness, communication harness, control harness, radio frequency harness etc..
In the present embodiment, according to all kinds of conducting wire features, Zuo Tongdao harness 3 and right channel harness 2 include three beams harness, and three
Bunch beam is respectively P harness 9, M harness 10, S harness 11.
P harness 9 includes the independent bunchy of high-power RF harness, such as radio system, radar system, to effectively reduce to it
The influence of his system；And large power supply harness merges harness with radio frequency harness, reduces the interference to systems such as control systems.
M harness 10 is the harness that merges for communicating harness, control harness or communicating harness with control harness, and communication harness is screen
It covers effect and preferably communicates harness, control harness is the lower control harness of security requirement, and M harness 10 comes from unmanned helicopter
Communication system and the systems such as flight control system, influence less, and interfered by other systems less between each other.
S harness 11 is control harness, including sensitive harness and the higher independent bunchy of control harness of security requirement, S
Fire control system, autoflight system, fly-by-wire etc. of the harness 11 from unmanned helicopter.
For the further optimization for realizing unmanned helicopter electrical harness interacted system, the embodiment of the application
In, it is separated between exterior strands 5 and internal harness by the way that parting surface is arranged, and be attached by separating socket, wherein internal
Harness includes that upper mounting plate harness 1, Zuo Tongdao harness 3, right channel harness 2 and endpiece harness 4, independent bunchy are conducive to install
It is made with harness.
In the embodiment of the application, separated between endpiece harness 4 and front harness by the way that parting surface is arranged, and
By separate socket be attached, wherein front harness include upper mounting plate harness 1, Zuo Tongdao harness 3, right channel harness 2 and
Exterior strands 5 are conducive to the independence of harness.
Advantageously, in the unmanned helicopter electrical harness interacted system of the application, the non-coupling partial line of internal system
The independent bunchy of beam, had both reduced relationship complicated between harness, while improving the installation effectiveness and maintenanceability of harness.
The unmanned helicopter electrical harness interacted system of the application fully considers helicopter structure feature, the interconnection of each system
Demand, practical, reasonably optimizing, the installation effectiveness and maintenanceability for improving harness.
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 electrical harness interacted system characterized by comprising
The upper mounting plate (6) of unmanned helicopter is arranged in upper mounting plate harness (1), the upper mounting plate harness (1)；
The left side of the lower layer installation region (7) of unmanned helicopter is arranged in left channel harness (3), the left channel harness (3)；
The right side of the lower layer installation region (7) of unmanned helicopter is arranged in right channel harness (2), the right channel harness (2)；
The endpiece (8) of unmanned helicopter is arranged in endpiece harness (4), the tail end harness (4)；
The outside of unmanned helicopter is arranged in exterior strands (5), the exterior strands (5).
2. unmanned helicopter electrical harness interacted system according to claim 1, which is characterized in that harness includes: power supply
Harness, communication harness, control harness, radio frequency harness.
3. unmanned helicopter electrical harness interacted system according to claim 2, which is characterized in that the left channel harness
(3) and the right channel harness (2) includes three beams harness.
4. unmanned helicopter electrical harness interacted system according to claim 3, which is characterized in that the three beams harness point
Not are as follows: P harness (9), M harness (10), S harness (11), wherein the P harness (9) is radio frequency harness or power supply harness and radio frequency
The merging harness of harness, the M harness (10) are to communicate harness, control harness or communicate harness to merge line with control harness
Beam, the S harness (11) are control harness.
5. unmanned helicopter electrical harness interacted system according to claim 4, which is characterized in that the P harness (9) is come
From the radio system and radar system of unmanned helicopter.
6. unmanned helicopter electrical harness interacted system according to claim 4, which is characterized in that the M harness (10)
Communication system and flight control system from unmanned helicopter.
7. unmanned helicopter electrical harness interacted system according to claim 4, which is characterized in that the S harness (11)
Fire control system, autoflight system and fly-by-wire from unmanned helicopter.
8. unmanned helicopter electrical harness interacted system according to claim 1, which is characterized in that the exterior strands
(5) it is separated between internal harness by the way that parting surface is arranged, wherein internal harness includes the upper mounting plate harness (1), the left side
Channel harness (3), the right channel harness (2) and the endpiece harness (4).
9. unmanned helicopter electrical harness interacted system according to claim 1, which is characterized in that the endpiece harness
(4) it is separated between the harness of front by the way that parting surface is arranged, wherein the front harness includes the upper mounting plate harness (1), institute
State left channel harness (3), the right channel harness (2) and the exterior strands (5).
10. unmanned helicopter electrical harness interacted system according to claim 8 or claim 9, which is characterized in that
It is separated between the exterior strands (5) and internal harness by setting parting surface and is attached by separating socket；
It is separated between the endpiece harness (4) and front harness by setting parting surface and is attached by separating socket.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811333393.2A CN109533363A (en) | 2018-11-09 | 2018-11-09 | A kind of unmanned helicopter electrical harness interacted system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811333393.2A CN109533363A (en) | 2018-11-09 | 2018-11-09 | A kind of unmanned helicopter electrical harness interacted system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109533363A true CN109533363A (en) | 2019-03-29 |
Family
ID=65846806
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811333393.2A Pending CN109533363A (en) | 2018-11-09 | 2018-11-09 | A kind of unmanned helicopter electrical harness interacted system |
Country Status (1)
| Country | Link |
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| CN (1) | CN109533363A (en) |
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| CN101010844A (en) * | 2004-09-22 | 2007-08-01 | 空中客车德国有限公司 | Cable outlet element, cable outlet device, cable outlet arrangement, method for producing a cable element and the use of a cable outlet element in an aircraft |
| CN105262021A (en) * | 2015-11-04 | 2016-01-20 | 中国直升机设计研究所 | Fireproof sealing layer structure for cable passing place of power cabin |
| CN105814308A (en) * | 2013-12-30 | 2016-07-27 | 谷歌公司 | Wiring harness for an aerial vehicle |
| CN205583569U (en) * | 2016-03-29 | 2016-09-14 | 江苏恒铭达航空设备有限公司 | Special cable fixing frame of helicopter |
| CN207200161U (en) * | 2017-08-18 | 2018-04-06 | 中国航空工业集团公司沈阳飞机设计研究所 | Fuel tanker inner cable boundling laying structure |
| CN208028513U (en) * | 2018-02-28 | 2018-10-30 | 江苏恒铭达航空设备有限公司 | The convenient cable fixed mount of helicopter |
-
2018
- 2018-11-09 CN CN201811333393.2A patent/CN109533363A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101010844A (en) * | 2004-09-22 | 2007-08-01 | 空中客车德国有限公司 | Cable outlet element, cable outlet device, cable outlet arrangement, method for producing a cable element and the use of a cable outlet element in an aircraft |
| CN105814308A (en) * | 2013-12-30 | 2016-07-27 | 谷歌公司 | Wiring harness for an aerial vehicle |
| CN105262021A (en) * | 2015-11-04 | 2016-01-20 | 中国直升机设计研究所 | Fireproof sealing layer structure for cable passing place of power cabin |
| CN205583569U (en) * | 2016-03-29 | 2016-09-14 | 江苏恒铭达航空设备有限公司 | Special cable fixing frame of helicopter |
| CN207200161U (en) * | 2017-08-18 | 2018-04-06 | 中国航空工业集团公司沈阳飞机设计研究所 | Fuel tanker inner cable boundling laying structure |
| CN208028513U (en) * | 2018-02-28 | 2018-10-30 | 江苏恒铭达航空设备有限公司 | The convenient cable fixed mount of helicopter |
Non-Patent Citations (4)
| Title |
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| 刘晓羽: "民用飞机线束主通道规划设计", 《航空科学技术》 * |
| 查奇峰: "浅谈EWIS分离面设计", 《技术与市场》 * |
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Application publication date: 20190329 |