CN102097752A - Direct-current distribution panel for helicopter - Google Patents
Direct-current distribution panel for helicopter Download PDFInfo
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- CN102097752A CN102097752A CN 201010612915 CN201010612915A CN102097752A CN 102097752 A CN102097752 A CN 102097752A CN 201010612915 CN201010612915 CN 201010612915 CN 201010612915 A CN201010612915 A CN 201010612915A CN 102097752 A CN102097752 A CN 102097752A
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- contactor
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- power supply
- busbar
- fuse
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Abstract
The invention relates to a direct-current distribution panel for a helicopter. In the direct-current distribution panel, a bottom plate is a composite insulating bottom plate; a generator power circuit comprises a fuse, a mutual inductor and a first direct-current contactor; a generator power supply passes through the mutual inductor and is connected to the end B of the first direct-current contactor, and the end A of the first direct-current contactor is connected with the fuse by a first bus bar; a ground power circuit comprises a fuse and a second direct-current contactor; a ground power supply is connected to the end B of the second direct-current contactor by a second bus bar, and the end A of the second direct-current contactor is connected with the fuse by the first bus bar; a storage battery power circuit comprises a fuse, a countercurrent protector and a third direct-current contactor; the countercurrent protector is connected to the end A of the third direct-current contactor by a third bus bar, and the end B of the third direct-current contactor is connected with the end B of the first direct-current contactor by a fourth bus bar; and the first direct-current contactor, the second direct-current contactor and the third direct-current contactor are connected with a breaker assembly and a relay assembly to switch the generator power circuit, the ground power circuit and the storage battery power circuit.
Description
Technical field
The present invention relates to a kind of DC distribution plate, is a kind of DC distribution plate that is used for helicopter specifically.
Background technology
The DC distribution plate of conventional helicopters, base plate is an aluminium sheet, though in light weight, insulation property are bad, easily by fixed screw the electric leakage on the finished product are delivered on the casing.The broken easily skin of long-term grazing forms electric leakage between lead and the aluminum soleplate in addition, causes potential safety hazard.In addition, separate connection between each parts on traditional DC distribution plate, connector is loose, in disorder, dismounting, maintenance inconvenience, connector is easily lost, and is not suitable for the aircraft small space and uses.
Summary of the invention
DC distribution plate base plate is that aluminium sheet easily leaks electricity in the prior art in order to solve, security performance is low, and DC distribution plate upper-part syndeton complexity, the various easy loss of connector is unfavorable for deficiencies such as dismounting, maintenance, the purpose of this invention is to provide a kind of compact conformation, connector is simplified and is difficult for losing, dismounting, easy to maintenance, base plate leakproof, the DC distribution plate of the helicopter that security performance is high.
The technical solution used in the present invention is: a kind of DC distribution plate of helicopter, base plate are provided with generator power supply circuit, ground power supply circuit and battery feed circuit, and its technical characterstic is that described base plate is the insulating base of composite material; The generator power supply circuit comprises fuse, instrument transformer and first D.C. contactor, and generator power supply passes the B end that instrument transformer connects first D.C. contactor, and the A end of first D.C. contactor connects fuse through first busbar; Described ground power supply circuit comprises the fuse and second D.C. contactor, and ground power supply is held through the B that second busbar connects second D.C. contactor, and the A end of second D.C. contactor connects fuse through first busbar; Described battery feed circuit comprises fuse, Reverse Current Protection device and the 3rd D.C. contactor, the Reverse Current Protection device is held through the A that the 3rd busbar connects the 3rd D.C. contactor 11, and the B end of the 3rd D.C. contactor connects the B end of first D.C. contactor through the 4th busbar; Described first, second and third D.C. contactor all connects the switching that breaker assembly on the insulating base and relay assembly are realized generator power supply circuit, ground power supply circuit and battery feed circuit.
Further, the B of described the 3rd D.C. contactor 11 end connects first busbar.
Again further, described first, second, third and fourth busbar all is fixed on the insulating base.
The beneficial effect that the present invention reaches is:
1, base plate adopts the insulating base of composite material, fundamentally solved the potential safety hazard of transmitting electric leakage, the base plate weight ratio aluminium of this composite material is light, be higher than designing requirement, by cold test, high-temperature test (+60 ° of C), low-temperature test (40 ° of C), temperature shock test, vibration test, shock test, acceleration test, salt mist test, mould test, the humid heat test of national Specification, its intensity of evidence, hardness, toughness, ageing properties all can satisfy the aircraft utilization requirement;
2, adopt many fuse and a plurality of contactors on the busbars connection distribution panelboard, each busbar bifurcated connects remaining component on fuse, a plurality of contactor and the distribution panelboard, solved that the operation of a plurality of contactors of a plurality of connector separate connection of traditional employing, fuse is loaded down with trivial details, the easy problem such as loss of connector, help keeping in repair fast, changing on the helicopter of small space.
The present invention is on the insulating base of composite material, to be fixed on finished products such as D.C. contactor on the base plate, fuse by many busbars organically combines, safety realizes the power supply control of helicopter DC power system and the conversion of various DC power supply, it is simple in structure, compact, loading and unloading, easy to maintenance, there is not electric leakage hidden danger, the usage safety performance height.
Description of drawings
Fig. 1 is a structural representation of the present invention;
Fig. 2 is a generator power supply electrical block diagram of the present invention;
Fig. 3 is a ground power supply electrical block diagram of the present invention;
Fig. 4 is a battery feed electrical block diagram of the present invention.
Among the figure: insulating base 1, fuse 2, instrument transformer 3; first D.C. contactor, 4, the first busbars 5, Reverse Current Protection device 6; second busbar 7; connector assembly 8, the second D.C. contactors 9, breaker assembly 10; the 3rd D.C. contactor 11; relay assembly 12, the three busbars 13, the four busbars 14.
Embodiment
The invention will be further described below in conjunction with drawings and Examples.
Shown in Fig. 1-4, a kind of DC distribution plate of helicopter mainly comprises insulating base 1, fuse 2, instrument transformer 3, first D.C. contactor 4, first busbar 5, Reverse Current Protection device 6, second busbar 7, connector assembly 8, second D.C. contactor 9, breaker assembly 10, the 3rd D.C. contactor 11 relay assemblies 12, the 3rd busbar 13 and the 4th busbar 14.Insulating base 1 upper left side from top to bottom successively level be provided with many fuses 2, insulating base 1 upper side edge middle part by a left side at least the right side successively level be provided with many instrument transformers 3, insulating base 1 upper right side is provided with Reverse Current Protection device 6, insulating base 1 lower-left side is provided with relay assembly 11, insulating base 1 lower side middle part is provided with breaker assembly 10, insulating base 1 bottom right side is provided with connector assembly 8, insulating base 1 middle and upper part level successively is provided with many first D.C. contactors 4, many first D.C. contactor 4 positions and the corresponding setting up and down of many instrument transformers, insulating base 1 right edge middle and lower part is provided with second D.C. contactor 9, and insulating base 1 middle and lower part level successively is provided with many 3rd D.C. contactors 11; The generator power supply of helicopter passes the B end that many instrument transformers 3 connect many first D.C. contactors 4, and the A end of many first D.C. contactors 4 connects many fuses 2 (as shown in Figure 2) through first busbar 5; Ground power supply is held through the B that second busbar 7 connects second D.C. contactor 9, and the A end of second D.C. contactor 9 connects many fuses 2 (as shown in Figure 3) through first busbar 5; Reverse Current Protection device 6 connects the A end of the 3rd D.C. contactor 11 through the 3rd busbar 13, the B end of the 3rd D.C. contactor 11 is held through the B that the 4th busbar 14 connects first D.C. contactor 4, and the B end of the 3rd D.C. contactor 11 connects first busbar 5 (as shown in Figure 4); First, second, third and fourth busbar 5,7,13,14 all is fixed on the insulating base 1, and first, second and third D.C. contactor 4,9,11 all connects the switching that breaker assembly 10 on the insulating base 1 and relay assembly 12 are realized generator power supply circuit, ground power supply circuit and battery feed circuit.
The foregoing description is a kind of brief layout connected mode of helicopter DC distribution plate, and protection scope of the present invention is not limited to said structure, every employing syndeton theory of the present invention all in protection range.
Claims (3)
1. the DC distribution plate of a helicopter, base plate is provided with generator power supply circuit, ground power supply circuit and battery feed circuit, it is characterized in that: described base plate is the insulating base (1) of composite material; The generator power supply circuit comprises fuse (2), instrument transformer (3) and first D.C. contactor (4), and generator power supply passes the B end that instrument transformer connects first D.C. contactor, and the A end of first D.C. contactor connects fuse through first busbar (5); Described ground power supply circuit comprises fuse and second D.C. contactor (9), and ground power supply is held through the B that second busbar (7) connects second D.C. contactor, and the A end of second D.C. contactor connects fuse through first busbar; Described battery feed circuit comprises fuse, Reverse Current Protection device (6) and the 3rd D.C. contactor (11), the Reverse Current Protection device is held through the A that the 3rd busbar (13) connects the 3rd D.C. contactor, and the B end of the 3rd D.C. contactor connects the B end of first D.C. contactor through the 4th busbar (14); Described first, second and third D.C. contactor all connects the switching that breaker assembly (10) on the insulating base and relay assembly (12) are realized generator power supply circuit, ground power supply circuit and battery feed circuit.
2. the DC distribution plate of a kind of helicopter according to claim 1 is characterized in that: described the 3rd D.C. contactor (11) B end connection first busbar (5).
3. the DC distribution plate of a kind of helicopter according to claim 1, it is characterized in that: described first, second, third and fourth busbar (5,7,13,14) all is fixed on the insulating base.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010612915 CN102097752B (en) | 2010-12-30 | 2010-12-30 | Direct-current distribution panel for helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010612915 CN102097752B (en) | 2010-12-30 | 2010-12-30 | Direct-current distribution panel for helicopter |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102097752A true CN102097752A (en) | 2011-06-15 |
| CN102097752B CN102097752B (en) | 2013-02-13 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201010612915 Active CN102097752B (en) | 2010-12-30 | 2010-12-30 | Direct-current distribution panel for helicopter |
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| CN (1) | CN102097752B (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103036158A (en) * | 2012-12-19 | 2013-04-10 | 贵州振华华联电子有限公司 | Automobile instrument distribution board |
| CN104659900A (en) * | 2013-11-25 | 2015-05-27 | 中国直升机设计研究所 | Power supply system of unmanned helicopter |
| CN105027364A (en) * | 2013-01-10 | 2015-11-04 | 泰科电子公司 | Manual service disconnects for battery systems |
| CN105471079A (en) * | 2016-01-12 | 2016-04-06 | 济南轨道交通装备有限责任公司 | Emergency control system and emergency control method for railway track car |
| CN107979084A (en) * | 2017-11-28 | 2018-05-01 | 浙江中航通飞研究院有限公司 | A kind of low-voltage direct distribution system in general-purpose aircraft distribution region |
| CN108199425A (en) * | 2017-12-20 | 2018-06-22 | 中国航空工业集团公司西安飞行自动控制研究所 | A kind of flight control system stand-by power supply ground uses guard method |
| CN109524883A (en) * | 2018-03-16 | 2019-03-26 | 陕西飞机工业（集团）有限公司 | A kind of aircraft four-way AC distribution device |
| CN110697057A (en) * | 2019-10-11 | 2020-01-17 | 中国直升机设计研究所 | Unmanned helicopter electrical power generating system |
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| US5013929A (en) * | 1989-11-22 | 1991-05-07 | Sundstrand Corporation | Power conversion system having prime mover start capability |
| WO2001027468A2 (en) * | 1999-10-01 | 2001-04-19 | Bell Helicopter Textron Inc. | Redundant electrical dc power system for aircraft |
| CN101529686A (en) * | 2006-10-27 | 2009-09-09 | 法国空中客车公司 | System for generating, converting, distributing and electrically starting on board an aircraft |
| CN101710732A (en) * | 2009-11-11 | 2010-05-19 | 北京航空航天大学 | Unmanned helicopter continuous voltage-stabilizing power supply system with engine air restarting function |
| CN201927893U (en) * | 2010-12-30 | 2011-08-10 | 江苏兆胜空调有限公司 | DC distribution panel of helicopter |
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2010
- 2010-12-30 CN CN 201010612915 patent/CN102097752B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
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| US5013929A (en) * | 1989-11-22 | 1991-05-07 | Sundstrand Corporation | Power conversion system having prime mover start capability |
| WO2001027468A2 (en) * | 1999-10-01 | 2001-04-19 | Bell Helicopter Textron Inc. | Redundant electrical dc power system for aircraft |
| CN101529686A (en) * | 2006-10-27 | 2009-09-09 | 法国空中客车公司 | System for generating, converting, distributing and electrically starting on board an aircraft |
| CN101710732A (en) * | 2009-11-11 | 2010-05-19 | 北京航空航天大学 | Unmanned helicopter continuous voltage-stabilizing power supply system with engine air restarting function |
| CN201927893U (en) * | 2010-12-30 | 2011-08-10 | 江苏兆胜空调有限公司 | DC distribution panel of helicopter |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103036158A (en) * | 2012-12-19 | 2013-04-10 | 贵州振华华联电子有限公司 | Automobile instrument distribution board |
| CN105027364A (en) * | 2013-01-10 | 2015-11-04 | 泰科电子公司 | Manual service disconnects for battery systems |
| CN105027364B (en) * | 2013-01-10 | 2017-05-24 | 泰科电子公司 | Manual service disconnects for battery systems |
| CN104659900A (en) * | 2013-11-25 | 2015-05-27 | 中国直升机设计研究所 | Power supply system of unmanned helicopter |
| CN104659900B (en) * | 2013-11-25 | 2017-03-15 | 中国直升机设计研究所 | Depopulated helicopter power-supply system |
| CN105471079A (en) * | 2016-01-12 | 2016-04-06 | 济南轨道交通装备有限责任公司 | Emergency control system and emergency control method for railway track car |
| CN107979084A (en) * | 2017-11-28 | 2018-05-01 | 浙江中航通飞研究院有限公司 | A kind of low-voltage direct distribution system in general-purpose aircraft distribution region |
| CN108199425A (en) * | 2017-12-20 | 2018-06-22 | 中国航空工业集团公司西安飞行自动控制研究所 | A kind of flight control system stand-by power supply ground uses guard method |
| CN108199425B (en) * | 2017-12-20 | 2021-07-16 | 中国航空工业集团公司西安飞行自动控制研究所 | Ground use protection method for emergency power supply of flight control system |
| CN109524883A (en) * | 2018-03-16 | 2019-03-26 | 陕西飞机工业（集团）有限公司 | A kind of aircraft four-way AC distribution device |
| CN110697057A (en) * | 2019-10-11 | 2020-01-17 | 中国直升机设计研究所 | Unmanned helicopter electrical power generating system |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102097752B (en) | 2013-02-13 |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| CB03 | Change of inventor or designer information |
Inventor after: Qin Tianqing Inventor after: Zhang Aiyong Inventor after: Huang Lihua Inventor before: Qin Tianqing Inventor before: Zhang Aiyong Inventor before: Huang Lihua |
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| COR | Change of bibliographic data | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20151109 Address after: 225441 Taizhou, Jiangsu, Taixing City, Jiangxi Road, No. 1, No. 3 Patentee after: JIANGSU ACER RING ELECTRIC COMPANY LIMITED Address before: 225441 Tongjiang Road, Taixing, Jiangsu, No. 18, No. Patentee before: Jiangsu Josun Air Conditioner Co., Ltd. |
|
| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 225441 Taizhou, Jiangsu, Taixing City, Jiangxi Road, No. 1, No. 3 Patentee after: Jiangsu Acer electric ring Limited by Share Ltd Address before: 225441 Taizhou, Jiangsu, Taixing City, Jiangxi Road, No. 1, No. 3 Patentee before: JIANGSU ACER RING ELECTRIC COMPANY LIMITED |