CN105905300B - A kind of carbon fiber lever apparatus in Modularized unmanned machine system - Google Patents

A kind of carbon fiber lever apparatus in Modularized unmanned machine system Download PDF

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Publication number
CN105905300B
CN105905300B CN201610224853.2A CN201610224853A CN105905300B CN 105905300 B CN105905300 B CN 105905300B CN 201610224853 A CN201610224853 A CN 201610224853A CN 105905300 B CN105905300 B CN 105905300B
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Prior art keywords
carbon fiber
copper lines
fiber bar
degree
polygon
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CN201610224853.2A
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Chinese (zh)
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CN105905300A (en
Inventor
宋宇航
孔祥龙
王昊臣
王健伊
樵明朗
崔大钧
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Beihang University
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Beihang University
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/19Propulsion using electrically powered motors

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Contacts (AREA)
  • Nonwoven Fabrics (AREA)

Abstract

A kind of carbon fiber lever apparatus in Modularized unmanned machine system, it is made of copper lines and polygon carbon fiber bar;The copper lines are embedded in the copper lines slot on polygon carbon fiber bar;Specifically, there are 4 copper lines slots on the polygon carbon fiber bar, which is embedded in four copper lines slots;After insertion, a surface of the copper lines is flushed with the outer surface of polygon carbon fiber bar, is exposed to that " polygon carbon fiber bar surface, remainder are embedded in this " in copper lines slot.The carbon fiber lever apparatus is simple in structure, and combination is convenient, and versatility is good, and manufacturing cost is low, safeguards and is easy.

Description

A kind of carbon fiber lever apparatus in Modularized unmanned machine system
One, technical field
The present invention provides the carbon fiber lever apparatus in a kind of Modularized unmanned machine system, belongs to " UAV system " technology neck Domain.
Two, technical background
UAV system is not restructural at present, cannot be mutually converted between different type of machines, and parts cannot be general, customization Degree is high, and general degree is low, nonstandardized technique, non-modularization.From the point of view of in all its bearings, all with " secondary design can not change again The property of change ".Moreover, in current UAV system, circuit connects the conducting wire for relying on various models mostly, and circuit is more miscellaneous Disorderly, it is unfavorable for debugging, electric wire exposure is easy to be damaged, increases the unstability of unmanned plane electronic system.
Modularized unmanned machine system, including:Power plant module device, link block device, servo module device, three big modules Device and the carbon fiber lever apparatus for connecting them.The carbon fiber lever apparatus be the Modularized unmanned machine system basic module device it One, which provides for UAV system:1, the connection of basic structure;2, the circuit of signal and power supply.The carbon fiber bar The stability requirement of device is high, and intensity requirement is higher;Should have the function of " structure connection " and " circuit pathways " simultaneously;Ying Ke To be easily connected with other three modular devices.
The carbon fiber lever apparatus is that design difficulty is larger in Modularized unmanned machine system, and technology is more demanding, indispensable Basic module device.
Three, invention content
1, goal of the invention:
The object of the present invention is to provide " carbon fiber lever apparatus (0-4) " in a set of Modularized unmanned machine system.It main Effect be:1, in Modularized unmanned machine system, provide the connection in structure for other three modular devices, that is, other three A modular device can be fixed on carbon fiber bar, and then be connected with each other in structure, be formed whole;2, in Modularized unmanned machine In system, the connection on circuit is provided for other three modular devices, so that being realized between modular device:Be in communication with each other and Share power supply.
2, technical solution
The object of the present invention is to provide it is in a kind of Modularized unmanned machine system, structure company can be carried out with other modular devices Connect and circuit connection modular device, that is, provide " carbon fiber lever apparatus (0-4) ", it is characterised in that:1, it can be three with other The interface of modular device (" power plant module device (0-1) ", " link block device (0-2) " and " servo module device (0-3) ") Coordinated, as shown in Figure 1 and Figure 2;2, the circuit that transmission electric energy and signal are provided for other three modular devices connects.
Carbon fiber bar modular device in a kind of Modularized unmanned machine system of the present invention, i.e., " carbon fiber lever apparatus (0-4) ", it is It is made of following two parts:" copper lines (0-4-1) " and " polygon carbon fiber bar (0-4-2) ", as shown in Figure 3.
Relationship that should be between " carbon fiber lever apparatus (0-4) " each component part is:As shown in figure 4, " copper lines (0-4- 1) it " is embedded in " copper lines slot (0-4-1-1) " on " polygon carbon fiber bar (0-4-2) " Nei.Specifically, i.e.,:Such as Shown in Fig. 5, there are 4 " copper lines slot (0-4-1-1) ", 4 " copper lines on " polygon carbon fiber bar (0-4-2) " (0-4-1) " is embedded in this four " copper lines slot (0-4-1-1) ".After insertion, " copper lines (0-4-1's) " One surface is flushed with the outer surface of " polygon carbon fiber bar (0-4-2) ", is exposed to " polygon carbon fiber bar (0-4-2) " table Face, remainder are embedded in " copper lines slot (0-4-1-1) ", when other three modular devices are " power plant module device (0-1) ", " link block device (0-2) " and " servo module device (0-3) " are fixed on " polygon carbon fiber bar (0-4-2) " After upper, which contacts conducting with this 4 " copper lines (0-4-1) ".
Should the shape design of " copper lines (0-4-1) " be:Cross section is rectangle, length with and its cooperation it is " more Side shape carbon fiber bar (0-4-2) " is identical.
Should the material of " copper lines (0-4-1) " be:It is copper.
It is somebody's turn to do there are two types of " polygon carbon fiber bars (0-4-2) ", they are respectively:" positive eight prisms carbon fiber bar (0-4-2- 1) " and " four-prism carbon fiber bar (0-4-2-2) ", as needed and technological requirement select one of which use.
When " the polygon carbon fiber bar (0-4-2) " is " positive eight prisms carbon fiber bar (0-4-2-1) ", shape design It is as follows:
1, as shown in fig. 6, generally positive eight prism, is tubulose, as positive eight prismatic shell, inside is " positive eight prisms cavity (0-4-2-1-1) ".
2, as shown in fig. 6, being somebody's turn to do " positive eight prisms carbon fiber bar (0-4-2-1) " has eight " positive eight prisms carbon fiber rod outer surfaces (0-4-2-1-2) ", wherein having " copper lines slot on four " positive eight prisms carbon fiber rod outer surfaces (0-4-2-1-2) " (0-4-1-1) ".
3, as shown in fig. 6, the section " copper lines slot (0-4-1-1) " is rectangle, size and " copper lines (0- Section 4-1) " is identical.
Should " positive eight prisms carbon fiber bar (0-4-2-1) " and three modular devices (i.e. " power plant module device (0-1) ", " link block device (0-2) " and " servo module device (0-3) ") between relationship be:As shown in fig. 7, three module dresses Setting can be fixed on some special angles on " the positive eight prisms carbon fiber bar (0-4-2-1) ", these fixed angles are 45 degree Integral multiple, i.e.,:0 degree, 45 degree, 90 degree, 135 degree, 180 degree, 225 degree, 270 degree, 315 degree.
When " the polygon carbon fiber bar (0-4-2) " is " four-prism carbon fiber bar (0-4-2-2) ", shape design It is as follows:
As shown in figure 8, generally four-prism, is tubulose, as four-prism shell, inside are " four-prism cavitys (0-4-2-2-1) ".
4, as shown in figure 8, being somebody's turn to do " four-prism carbon fiber bar (0-4-2-2) ", there are four " four-prism carbon fiber rod outer surfaces (0-4-2-2-2) ", " four-prism carbon fiber rod outer surface (0-4-2-2-2) " are equipped with " copper lines slot (0- 4-1-1) ".
5, as shown in figure 8, the section " copper lines slot (0-4-1-1) " is rectangle, size and " copper lines (0- Section 4-1) " is identical.
Should " four-prism carbon fiber bar (0-4-2-2) " and three modular devices (i.e. " power plant module device (0-1) ", " link block device (0-2) " and " servo module device (0-3) ") between relationship be:As shown in figure 9, three module dresses Setting can be fixed on some special angles on " the four-prism carbon fiber bar (0-4-2-2) ", these fixed angles are 90 degree Integral multiple, i.e.,:0 degree, 90 degree, 180 degree, 270 degree.
3, advantage and effect
Other several modular devices that should be in the design and Modularized unmanned machine system of " carbon fiber lever apparatus (0-4) " shape and Component matches, simple in structure, and combination is convenient, and versatility is good, and manufacturing cost is low, safeguards and is easy.
The cylindrical carbon fiber bar common compared to market, it is positive multi-edge column-shaped to be somebody's turn to do " carbon fiber lever apparatus (0-4) ", this makes it Structural strength is more preferable, when fixing other three modular devices, more difficult skidding.
It is somebody's turn to do " carbon fiber lever apparatus (0-4) " and provides connection for Modularized unmanned machine system, eliminate complicated easy break-down Connection.
Four, description of the drawings
Fig. 1:Three big modular devices are connected to by unified interface on positive eight prisms carbon fiber bar ligand.
Fig. 2:Three big modular devices are connected to by unified interface on four-prism carbon fiber bar ligand.
Fig. 3:The composition figure of carbon fiber lever apparatus.
Fig. 4:Copper lines are embedded in the copper lines slot on polygon carbon fiber bar.
Fig. 5:Show 4 copper lines slots on polygon carbon fiber bar.
Fig. 6:The shape design of positive eight prisms carbon fiber bar and copper lines slot is shown.
Fig. 7:Three big modular devices are fixed on some special angles on positive eight prisms carbon fiber bar.
Fig. 8:The shape design of four-prism carbon fiber bar and copper lines slot is shown.
Fig. 9:Three big modular devices are fixed on some special angles on four-prism carbon fiber bar.
Serial number in figure, symbol, the meaning representated by code name are as follows:
0-1:Power plant module device
0-2:Link block device
0-3:Servo module device
0-4:Carbon fiber lever apparatus
0-4-1:Copper lines
0-4-1-1:Copper lines slot
0-4-2:Polygon carbon fiber bar
0-4-2-1:Positive eight prisms carbon fiber bar
0-4-2-1-1:Positive eight prisms cavity
0-4-2-1-2:Positive eight prisms carbon fiber rod outer surface
0-4-2-2:Four-prism carbon fiber bar
0-4-2-2-1:Four-prism cavity
0-4-2-2-2:Four-prism carbon fiber rod outer surface
Five, specific implementation mode
" carbon fiber lever apparatus (0-4) " is somebody's turn to do to be made of following two parts:" copper lines (0-4-1) ", " polygon carbon fiber Bar (0-4-2) ", as shown in Figure 3.
Relationship that should be between " carbon fiber lever apparatus (0-4) " each component part is:As shown in figure 4, " copper lines (0-4- 1) it " is embedded in " copper lines slot (0-4-1-1) " on " polygon carbon fiber bar (0-4-2) " Nei.Specifically, i.e.,:Such as Shown in Fig. 5, there are 4 " copper lines slot (0-4-1-1) ", 4 " copper lines on " polygon carbon fiber bar (0-4-2) " (0-4-1) " is embedded in this four " copper lines slot (0-4-1-1) ".After insertion, " copper lines (0-4-1's) " One surface is flushed with the outer surface of " polygon carbon fiber bar (0-4-2) ", is exposed to " polygon carbon fiber bar (0-4-2) " table Face, remainder are embedded in " copper lines slot (0-4-1-1) ", when other three modular devices are fixed on " polygon carbon After on fine bar (0-4-2) ", three modular devices contact conducting with this 4 " copper lines (0-4-1) ".
Should the shape design of " copper lines (0-4-1) " be:Cross section is rectangle, length with and its cooperation it is " more Side shape carbon fiber bar (0-4-2) " is identical.
Should the material of " copper lines (0-4-1) " be:It is copper.
" polygon carbon fiber bar (0-4-2) " is somebody's turn to do by two kinds, they are respectively:" positive eight prisms carbon fiber bar (0-4-2- 1) ", " four-prism carbon fiber bar (0-4-2-2) ".
Relationship between two kinds " polygon carbon fiber bar (0-4-2) " is:Respectively there are advantage and disadvantage, according to demand and process choice One of which use.
Should the shape design of " positive eight prisms carbon fiber bar (0-4-2-1) " be:
6, as shown in fig. 6, generally positive eight prism, is tubulose, as positive eight prismatic shell, inside is " positive eight prisms cavity (0-4-2-1-1) ".
7, as shown in fig. 6, being somebody's turn to do " positive eight prisms carbon fiber bar (0-4-2-1) " has eight " positive eight prisms carbon fiber rod outer surfaces (0-4-2-1-2) ", wherein having " copper lines slot on four " positive eight prisms carbon fiber rod outer surfaces (0-4-2-1-2) " (0-4-1-1) ".
8, as shown in fig. 6, the section " copper lines slot (0-4-1-1) " is rectangle, size and " copper lines (0- Section 4-1) " is identical.
Three modular devices of " the positive eight prisms carbon fiber bar (0-4-2-1) " and other (" power plant module device (0-1) ", " link block device (0-2) " and " servo module device (0-3) ") between relationship be:As shown in fig. 7, other modular devices It can be fixed on some special angles on " the positive eight prisms carbon fiber bar (0-4-2-1) ", these fixed angles are 45 degree Integral multiple, i.e.,:0 degree, 45 degree, 90 degree, 135 degree, 180 degree, 225 degree, 270 degree, 315 degree.
Should the shape design of " four-prism carbon fiber bar (0-4-2-2) " be:
9, as shown in figure 8, generally four-prism, is tubulose, as four-prism shell, inside are " four-prism cavitys (0-4-2-2-1) ".
10, as shown in figure 8, being somebody's turn to do " four-prism carbon fiber bar (0-4-2-2) ", there are four " four-prism carbon fiber bar appearances There is " copper lines slot (0- in face (0-4-2-2-2) " on " four-prism carbon fiber rod outer surface (0-4-2-2-2) " 4-1-1) ".
11, as shown in figure 8, the section " copper lines slot (0-4-1-1) " is rectangle, size and " copper lines (0- Section 4-1) " is identical.
Three modular devices of " the four-prism carbon fiber bar (0-4-2-2) " and other (" power plant module device (0-1) ", " link block device (0-2) " and " servo module device (0-3) ") between relationship be:As shown in figure 9, other modular devices It can be fixed on some special angles on " the four-prism carbon fiber bar (0-4-2-2) ", these fixed angles are 90 degree Integral multiple, i.e.,:0 degree, 90 degree, 180 degree, 270 degree.

Claims (1)

1. the carbon fiber bar modular device in a kind of Modularized unmanned machine system, i.e. carbon fiber lever apparatus, it is by following two parts group At:Copper lines and polygon carbon fiber bar;
Relationship between each component part of carbon fiber lever apparatus is:Copper lines are embedded in the copper lines on polygon carbon fiber bar In slot;I.e.:There are 4 copper lines slots, 4 copper lines to be embedded in this four copper lines slots on polygon carbon fiber bar;It is embedding After entering, a surface of copper lines is flushed with the outer surface of polygon carbon fiber bar, is exposed to polygon carbon fiber bar surface, remaining It is partly embedded in copper lines slot, when other three modular devices, that is, power plant module device, link block device and servo moulds After block assembly is fixed on polygon carbon fiber bar, 4 copper lines of three modular devices and this contact conducting;
The shape design of the copper lines is:Cross section is rectangle, length with and its polygon carbon fiber bar for coordinating it is identical;
The material of the copper lines is:It is copper;
There are two types of the polygon carbon fiber bars, is respectively:Positive eight prisms carbon fiber bar and four-prism carbon fiber bar, as needed and technique It is required that selection one of which use;
When the polygon carbon fiber bar is positive eight prisms carbon fiber bar, shape design is as follows:
Generally positive eight prism, is tubulose, and as positive eight prismatic shell, inside is positive eight prisms cavity;
The positive eight prisms carbon fiber bar has eight positive eight prisms carbon fiber rod outer surfaces, wherein on four positive eight prisms carbon fiber rod outer surfaces There is copper lines slot;
Copper lines slot cross-section is rectangle, and size is identical as the section of copper lines;
The positive eight prisms carbon fiber bar and three modular devices can be fixed on some special angles on the positive eight prisms carbon fiber bar, this The integral multiple that a little fixed angles are 45 degree, i.e.,:0 degree, 45 degree, 90 degree, 135 degree, 180 degree, 225 degree, 270 degree, 315 degree;
When the polygon carbon fiber bar is four-prism carbon fiber bar, shape design is as follows:
Generally four-prism is tubulose, as four-prism shell, and inside is four-prism cavity;
There are four four-prism carbon fiber rod outer surface, four-prism carbon fiber rod outer surfaces to be equipped with copper for the four-prism carbon fiber bar Line slot;
Copper lines slot cross-section is rectangle, and size is identical as the section of copper lines;
The four-prism carbon fiber bar and three modular devices can be fixed on some special angles on the four-prism carbon fiber bar, this The integral multiple that a little fixed angles are 90 degree, i.e.,:0 degree, 90 degree, 180 degree, 270 degree.
CN201610224853.2A 2016-04-12 2016-04-12 A kind of carbon fiber lever apparatus in Modularized unmanned machine system Expired - Fee Related CN105905300B (en)

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2197419A (en) * 1986-09-25 1988-05-18 Raychem Gmbh Conduit with heater strip
CN1620573A (en) * 2001-11-20 2005-05-25 北卡罗来纳康姆斯科普公司 Toneable conduit and method of preparing same
CN202046437U (en) * 2011-02-28 2011-11-23 贵阳高新冰点科技有限公司 Small-sized electric tailless type unmanned plane for remote sensing and monitoring of emergency
CN204173154U (en) * 2014-10-09 2015-02-25 中国航天空气动力技术研究院 A kind of modularized combination type unmanned plane

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NO325540B1 (en) * 2005-02-11 2008-06-16 Nexans Umbilical and method of its preparation
US7942717B2 (en) * 2008-12-15 2011-05-17 Ting-Shuo Chou Brick assembly with automatically recognizing connecting relationships

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2197419A (en) * 1986-09-25 1988-05-18 Raychem Gmbh Conduit with heater strip
CN1620573A (en) * 2001-11-20 2005-05-25 北卡罗来纳康姆斯科普公司 Toneable conduit and method of preparing same
CN202046437U (en) * 2011-02-28 2011-11-23 贵阳高新冰点科技有限公司 Small-sized electric tailless type unmanned plane for remote sensing and monitoring of emergency
CN204173154U (en) * 2014-10-09 2015-02-25 中国航天空气动力技术研究院 A kind of modularized combination type unmanned plane

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