ES2400152B1 - AN ELECTRICAL SYSTEM OF AN AIRCRAFT. - Google Patents
AN ELECTRICAL SYSTEM OF AN AIRCRAFT. Download PDFInfo
- Publication number
- ES2400152B1 ES2400152B1 ES201131498A ES201131498A ES2400152B1 ES 2400152 B1 ES2400152 B1 ES 2400152B1 ES 201131498 A ES201131498 A ES 201131498A ES 201131498 A ES201131498 A ES 201131498A ES 2400152 B1 ES2400152 B1 ES 2400152B1
- Authority
- ES
- Spain
- Prior art keywords
- loads
- status
- aircraft
- distribution
- electrical system
- 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
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J9/00—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting
Abstract
Un sistema eléctrico de una aeronave. Comprende: a) unas fuentes de generación de energía eléctrica (11, 13); b) un dispositivo integrado de distribución de energía eléctrica (29) que comprende unas barras de distribución (21, 23), una pluralidad de cargas conectadas a ellas a través de SSPCs y una unidad de gestión (31) conectada a dichos SSPCs para monitorizar su estado y asignarles el estado de conmutación (ON/OFF) a ser implementado por ellos; c) un subsistema de control para monitorizar el estado de dichas barras de distribución (21, 23) y dichas cargas y para proporcionar a dicha unidad de gestión (31) la información de control necesaria para la distribución de energía eléctrica a las cargas que comprende circuitos de comunicaciones de señales digitales (35) desde un bus de control (36) y circuitos de comunicación de señales discretas (40) de las unidades de control (38) de dichas cargas.An electrical system of an aircraft. It includes: a) sources of electricity generation (11, 13); b) an integrated electric power distribution device (29) comprising distribution bars (21, 23), a plurality of loads connected to them through SSPCs and a management unit (31) connected to said SSPCs for monitoring their status and assign them the switching status (ON / OFF) to be implemented by them; c) a control subsystem to monitor the status of said distribution bars (21, 23) and said loads and to provide said management unit (31) with the control information necessary for the distribution of electrical energy to the loads comprising digital signal communication circuits (35) from a control bus (36) and discrete signal communication circuits (40) of the control units (38) of said loads.
Description
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201131498A ES2400152B1 (en) | 2011-09-15 | 2011-09-15 | AN ELECTRICAL SYSTEM OF AN AIRCRAFT. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201131498A ES2400152B1 (en) | 2011-09-15 | 2011-09-15 | AN ELECTRICAL SYSTEM OF AN AIRCRAFT. |
Publications (3)
Publication Number | Publication Date |
---|---|
ES2400152A2 ES2400152A2 (en) | 2013-04-05 |
ES2400152R1 ES2400152R1 (en) | 2013-10-24 |
ES2400152B1 true ES2400152B1 (en) | 2014-08-18 |
Family
ID=47890758
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES201131498A Expired - Fee Related ES2400152B1 (en) | 2011-09-15 | 2011-09-15 | AN ELECTRICAL SYSTEM OF AN AIRCRAFT. |
Country Status (1)
Country | Link |
---|---|
ES (1) | ES2400152B1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10101749B1 (en) | 2017-03-21 | 2018-10-16 | Bell Helicopter Textron Inc. | Combined airspeed and inertial data for rotorcraft longitudinal control |
US10942527B2 (en) | 2017-05-30 | 2021-03-09 | Textron Innovations Inc. | System and method for controlling rotorcraft load priority |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7020790B2 (en) * | 2001-02-08 | 2006-03-28 | Honeywell International Inc. | Electric load management center including gateway module and multiple load management modules for distributing power to multiple loads |
US7205681B2 (en) * | 2004-02-06 | 2007-04-17 | Honeywell International Inc. | Generation and distribution of a dual-redundant logic supply voltage for an electrical system |
US7634329B2 (en) * | 2007-03-05 | 2009-12-15 | Honeywell International Inc. | Intelligent aircraft secondary power distribution system that facilitates condition based maintenance |
US7805204B2 (en) * | 2007-03-21 | 2010-09-28 | Honeywell International Inc. | Integrated electrical power distribution system using common building blocks |
US7598625B2 (en) * | 2007-06-08 | 2009-10-06 | Honeywell International Inc. | Network-based aircraft secondary electric power distribution system |
-
2011
- 2011-09-15 ES ES201131498A patent/ES2400152B1/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
ES2400152R1 (en) | 2013-10-24 |
ES2400152A2 (en) | 2013-04-05 |
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Legal Events
Date | Code | Title | Description |
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FG2A | Definitive protection |
Ref document number: 2400152 Country of ref document: ES Kind code of ref document: B1 Effective date: 20140818 |
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FD2A | Announcement of lapse in spain |
Effective date: 20181015 |