Patent Grant
8559149
This disclosure relates to a primary power distribution panel used in high current aircraft power distribution systems.
Traditional aircraft electric power systems have high power AC contactors to switch and protect power on the primary power distribution system. These contactors are individual line replaceable units that mount terminal posts or pads coming from the primary bus structure and are usually housed in a primary distribution panel that contains current-sensing features and sometimes control functions connected by numerous wires and that adds intelligence to open or close the contactors.
As electric power systems become more integrated, it is desirable to house the primary and secondary power distribution functions in a single enclosure. This is desirable since power from the primary distribution flows to the secondary relays and circuit breakers to be distributed to aircraft loads. However, such integration is problematic due to the amount of wiring and number of interconnects required to perform the functions of power control and protection. For example, it is difficult to gain access to buses that are segregated for safety. It is also difficult to keep that segregation through the secondary distribution with a minimum of cross-channel wiring. Moreover, the replacement of contactors has to be accommodated. Contactors typically use bolted joints, and hardware can be dropped or left untorqued when replacing the power joints.
What is needed is a primary power distribution panel having integrated power control and protection with segregated secondary power distribution and minimal wiring.
An aircraft power distribution system is disclosed that includes a power distribution box. A generator supplies power to the power distribution box, and a load receives power from the power distribution box. The power distribution box includes a board supporting plug-in pins receiving the power. A contactor is supported by the board to selectively provide power to a secondary power distribution connector supported on the board. The board includes power traces within the board to connect the plug-in pins to the secondary power distribution connector. Protection and secondary power distribution circuitry are also supported by the board and connected to the contactors and/or power traces by control traces. The power and control traces eliminate loose wiring and harnesses.
These and other features of the disclosure can be best understood from the following specification and drawings, the following of which is a brief description.
An aircraft power distribution system 10 is shown in
The primary power distribution box 12 includes a board 24 arranged within a housing 22. The board 24 supports plug-in pins 26 that are connected to the power leads 28. Mechanical contactors 30 act as switches to selectively electrically connect the power leads to the supply leads 46. In one example, the contactors 30 are permanently secured to the board 24 such that removal of the contactors 30 from the board 24 would result in damage to the contactors 30 and/or board 24. Circuit breakers 48 are supported by the board 24 to selectively disconnect the supply leads 46 from power in response to an overload. In one example, the circuit breakers 48 plug into the board to eliminate wiring.
The board 24 also supports a connector 32 that communicates with a control 34 through a harness 36. The control 34 provides commands to the board 24 and/or a secondary circuit board 38 and receives feedback regarding various functions related to the system 10. In one embodiment, the secondary circuit board 38 plugs into the board 24 to eliminate wiring. Printed traces are also run on or within the board 24 and secondary circuit board 38 to eliminate loose wiring and harnesses, which is described in more detail below. The components mounted to the board 24 connect to various traces on the board 24.
The secondary circuit board 38 is mounted on the board 24. The secondary circuit board 38 is connected to the connector 32 and contactors 30 through connections 39, which may be provided by electrical traces in (or on) the board 24 to eliminate wiring. The secondary circuit board 38 includes protection circuitry 40 and secondary power distribution circuitry 42. The protection circuitry 40 monitors the current provided by the generator 14, for example, to prevent the secondary power distribution box 16 from undesired currents. The secondary power distribution circuitry 42 commands the contactors 30 between open and closed positions.
Referring to
Although exemplary embodiments have been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of the claims. For that reason, the following claims should be studied to determine their true scope and content.
| Number | Name | Date | Kind |
|---|---|---|---|
| 3323086 | Pimentel | May 1967 | A |
| 4104581 | Arkosy | Aug 1978 | A |
| 4389608 | Dahl et al. | Jun 1983 | A |
| 4715822 | Stribel | Dec 1987 | A |
| 4868535 | Janniere et al. | Sep 1989 | A |
| 4908738 | Kobari et al. | Mar 1990 | A |
| 5481194 | Schantz et al. | Jan 1996 | A |
| 5513072 | Imaji et al. | Apr 1996 | A |
| 5552976 | Munro et al. | Sep 1996 | A |
| 5567991 | Schantz et al. | Oct 1996 | A |
| 5581130 | Boucheron | Dec 1996 | A |
| 5594285 | Wisbey et al. | Jan 1997 | A |
| 5648892 | Wieloch et al. | Jul 1997 | A |
| 5760587 | Harvey | Jun 1998 | A |
| 6122155 | Aromin et al. | Sep 2000 | A |
| 6201701 | Linden et al. | Mar 2001 | B1 |
| 6421253 | Ash, Jr. | Jul 2002 | B1 |
| 6441520 | Grant | Aug 2002 | B1 |
| D463362 | Alcantar et al. | Sep 2002 | S |
| 6469907 | Faveluke et al. | Oct 2002 | B1 |
| 6470224 | Drake et al. | Oct 2002 | B1 |
| 6504730 | Cooney et al. | Jan 2003 | B1 |
| 6700795 | Jones et al. | Mar 2004 | B1 |
| 6856045 | Beneditz et al. | Feb 2005 | B1 |
| 7102356 | Wild | Sep 2006 | B2 |
| 7342762 | Harris, IV | Mar 2008 | B2 |
| 7978446 | Lindsey | Jul 2011 | B2 |
| 20040113804 | Cabrera et al. | Jun 2004 | A1 |
| 20050216192 | Bringuel et al. | Sep 2005 | A1 |
| 20050230746 | Eden et al. | Oct 2005 | A1 |
| 20050265008 | Chamberlin et al. | Dec 2005 | A1 |
| 20070223160 | Coffey et al. | Sep 2007 | A1 |
| 20070297109 | Borrego Bel et al. | Dec 2007 | A9 |
| Number | Date | Country |
|---|---|---|
| 0495322 | Nov 1995 | EP |
| 1 263 012 | Dec 2002 | EP |
| 9-121089 | May 1997 | JP |
| Entry |
|---|
| European Search Report for European Patent Application No. 09251257.3 completed Jan. 30, 2013. |
| Number | Date | Country | |
|---|---|---|---|
| 20090273234 A1 | Nov 2009 | US |
