FR2949175B1 - Architecture de distribution de courant pour un avion - Google Patents
Architecture de distribution de courant pour un avion Download PDFInfo
- Publication number
- FR2949175B1 FR2949175B1 FR1056322A FR1056322A FR2949175B1 FR 2949175 B1 FR2949175 B1 FR 2949175B1 FR 1056322 A FR1056322 A FR 1056322A FR 1056322 A FR1056322 A FR 1056322A FR 2949175 B1 FR2949175 B1 FR 2949175B1
- Authority
- FR
- France
- Prior art keywords
- current distribution
- airplane
- distribution architecture
- current
- length
- 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.)
- Expired - Fee Related
Links
Classifications
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Control Of Eletrric Generators (AREA)
- Supply And Distribution Of Alternating Current (AREA)
- Coupling Device And Connection With Printed Circuit (AREA)
- Rectifiers (AREA)
Abstract
L'architecture de distribution de courant pour avion comprend un rail conducteur (90/88) s'étendant généralement tout le long de la longueur d'un avion pour recevoir du courant d'un générateur (82, 84) et pour distribuer le courant dans des modules enfichables (92) situés le long de la longueur du rail conducteur (90/88).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102009037465.5 | 2009-08-13 | ||
DE102009037465.5A DE102009037465B4 (de) | 2009-08-13 | 2009-08-13 | Stromverteilungsarchitektur für ein Luftfahrzeug |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2949175A1 FR2949175A1 (fr) | 2011-02-18 |
FR2949175B1 true FR2949175B1 (fr) | 2020-04-10 |
Family
ID=43448315
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1056322A Expired - Fee Related FR2949175B1 (fr) | 2009-08-13 | 2010-07-30 | Architecture de distribution de courant pour un avion |
Country Status (3)
Country | Link |
---|---|
US (1) | US8890355B2 (fr) |
DE (1) | DE102009037465B4 (fr) |
FR (1) | FR2949175B1 (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9561867B2 (en) * | 2013-10-11 | 2017-02-07 | The Boeing Company | Modular equipment center lightning threat reduction architecture |
US9511728B2 (en) | 2013-10-11 | 2016-12-06 | The Boeing Company | Modular equipment center distributed primary power architecture |
CA2859807C (fr) | 2013-10-11 | 2018-08-14 | The Boeing Company | Reseau de commutation de puissance primaire a semi-conducteurs pour centres d'equipement modulaires |
US10243331B2 (en) * | 2017-07-31 | 2019-03-26 | Bell Helicopter Textron Inc. | Open relay device and system |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3950058A (en) * | 1973-11-05 | 1976-04-13 | Lockheed Aircraft Corporation | Programmable wiring system and junction box for use therein |
FR2498385A1 (fr) | 1981-01-20 | 1982-07-23 | Modeles Fs | Dispositif de distribution de courant electrique a securite sur engin volant leger equipe pour le vol aux instruments |
DE19617915C2 (de) * | 1996-05-03 | 2001-11-08 | Eads Airbus Gmbh | Anordnung zur Energieverteilung, in einem Flugzeug |
GB9926354D0 (en) * | 1999-11-08 | 2000-01-12 | Rolls Royce Plc | Power supply system for an aircraft |
US6664656B2 (en) | 2000-09-14 | 2003-12-16 | The Boeing Company | Aircraft electrical power distribution network |
US6704625B2 (en) | 2001-02-16 | 2004-03-09 | Hamilton Sunstrand Corporation | Aircraft architecture with a reduced bleed aircraft secondary power system |
US6845630B2 (en) | 2001-02-16 | 2005-01-25 | Hamilton Sundstrand Corporation | Electric power and cooling system for an aircraft |
US6782346B2 (en) | 2001-05-07 | 2004-08-24 | The Boeing Company | Aircraft synthesis and systems evaluation method for determining and evaluating electrical power generation and distribution system components |
US6504730B1 (en) * | 2001-07-23 | 2003-01-07 | Hamilton Sundstrand Corporation | Serviceable power modules for a power distribution assembly |
DE50308156D1 (de) | 2002-08-02 | 2007-10-25 | Airbus Gmbh | Energieversorgungsanordnung für eine Bordküche eines Verkehrsmittels, insbesondere eines Flugzeuges |
US6871919B2 (en) * | 2002-08-20 | 2005-03-29 | Visteon Global Technologies, Inc. | Method and apparatus for power management of a braking system |
US7210653B2 (en) * | 2002-10-22 | 2007-05-01 | The Boeing Company | Electric-based secondary power system architectures for aircraft |
US6778414B2 (en) | 2002-12-20 | 2004-08-17 | The Boeing Company | Distributed system and methodology of electrical power regulation, conditioning and distribution on an aircraft |
US7035115B2 (en) * | 2003-04-11 | 2006-04-25 | Rockwell Automation Technologies, Inc. | Multi-axis motor control with high voltage backplane |
US7116003B2 (en) | 2004-07-14 | 2006-10-03 | Hamilton Sundstrand Corporation | Aircraft starter/generator electrical system with mixed power architecture |
US7429190B2 (en) | 2004-08-12 | 2008-09-30 | Airbus Deutschland Gmbh | Power distribution system for supplying a rail-mounted monument in an aircraft with electric power |
US20060174629A1 (en) * | 2004-08-24 | 2006-08-10 | Honeywell International, Inc | Method and system for coordinating engine operation with electrical power extraction in a more electric vehicle |
US7922117B2 (en) * | 2004-08-30 | 2011-04-12 | Hamilton Sundstrand Corporation | Primary panel and motor controller integration for aircraft power distribution system |
US7339809B2 (en) | 2004-11-30 | 2008-03-04 | The Boeing Company | Systems and methods for electrical power regulation and distribution in aircraft |
JP2007015423A (ja) * | 2005-07-05 | 2007-01-25 | Shin Meiwa Ind Co Ltd | 航空機の電源システム |
US8148842B2 (en) | 2006-02-20 | 2012-04-03 | Hamilton Sundstrand Corporation | Electrical power generation system having multiple secondary power distribution assemblies with integral power conversion |
US7495353B2 (en) | 2006-08-01 | 2009-02-24 | Hamilton Sundstrand Corporation | Power interconnect block for an aircraft electrical component |
US7393248B2 (en) * | 2006-11-03 | 2008-07-01 | The Boeing Company | Modular power control system with multipin connectors and airflow conrol module |
US7800245B2 (en) * | 2007-07-09 | 2010-09-21 | Honeywell International Inc. | Method and architecture for reduction in vehicle wiring |
US8559149B2 (en) * | 2008-05-05 | 2013-10-15 | Hamilton Sundstrand Corporation | Modular primary distribution contact board |
-
2009
- 2009-08-13 DE DE102009037465.5A patent/DE102009037465B4/de not_active Expired - Fee Related
-
2010
- 2010-04-01 US US12/752,447 patent/US8890355B2/en not_active Expired - Fee Related
- 2010-07-30 FR FR1056322A patent/FR2949175B1/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE102009037465B4 (de) | 2019-07-04 |
DE102009037465A1 (de) | 2011-02-17 |
US8890355B2 (en) | 2014-11-18 |
US20110037315A1 (en) | 2011-02-17 |
FR2949175A1 (fr) | 2011-02-18 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLSC | Publication of the preliminary search report |
Effective date: 20151204 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
|
ST | Notification of lapse |
Effective date: 20220305 |