GB201301223D0 - An electrical system for an aircraft anda method of control - Google Patents
An electrical system for an aircraft anda method of controlInfo
- Publication number
- GB201301223D0 GB201301223D0 GB201301223A GB201301223A GB201301223D0 GB 201301223 D0 GB201301223 D0 GB 201301223D0 GB 201301223 A GB201301223 A GB 201301223A GB 201301223 A GB201301223 A GB 201301223A GB 201301223 D0 GB201301223 D0 GB 201301223D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- control
- electrical system
- anda method
- anda
- 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.)
- Withdrawn
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
- H02J3/00—Circuit arrangements for ac mains or ac distribution networks
- H02J3/04—Circuit arrangements for ac mains or ac distribution networks for connecting networks of the same frequency but supplied from different sources
- H02J3/06—Controlling transfer of power between connected networks; Controlling sharing of load between connected networks
-
- 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
- H02J3/00—Circuit arrangements for ac mains or ac distribution networks
- H02J3/02—Circuit arrangements for ac mains or ac distribution networks using a single network for simultaneous distribution of power at different frequencies; using a single network for simultaneous distribution of ac power and of dc power
-
- 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
- H02J3/00—Circuit arrangements for ac mains or ac distribution networks
- H02J3/28—Arrangements for balancing of the load in a network by storage of energy
- H02J3/30—Arrangements for balancing of the load in a network by storage of energy using dynamo-electric machines coupled to flywheels
-
- 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
- H02J3/00—Circuit arrangements for ac mains or ac distribution networks
- H02J3/28—Arrangements for balancing of the load in a network by storage of energy
- H02J3/32—Arrangements for balancing of the load in a network by storage of energy using batteries with converting means
- H02J3/322—Arrangements for balancing of the load in a network by storage of energy using batteries with converting means the battery being on-board an electric or hybrid vehicle, e.g. vehicle to grid arrangements [V2G], power aggregation, use of the battery for network load balancing, coordinated or cooperative battery charging
-
- 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
- H02J4/00—Circuit arrangements for mains or distribution networks not specified as ac or dc
-
- 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
- H02J5/00—Circuit arrangements for transfer of electric power between ac networks and dc networks
-
- 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
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/02—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from ac mains by converters
-
- 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
- H02J2310/00—The network for supplying or distributing electric power characterised by its spatial reach or by the load
- H02J2310/40—The network being an on-board power network, i.e. within a vehicle
- H02J2310/44—The network being an on-board power network, i.e. within a vehicle for aircrafts
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/16—Mechanical energy storage, e.g. flywheels or pressurised fluids
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Control Of Eletrric Generators (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1301223.2A GB2510121A (en) | 2013-01-24 | 2013-01-24 | An aircraft electrical generator supplemented by an energy store until the generator is ramped up to meet the load requirement. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1301223.2A GB2510121A (en) | 2013-01-24 | 2013-01-24 | An aircraft electrical generator supplemented by an energy store until the generator is ramped up to meet the load requirement. |
Publications (2)
Publication Number | Publication Date |
---|---|
GB201301223D0 true GB201301223D0 (en) | 2013-03-06 |
GB2510121A GB2510121A (en) | 2014-07-30 |
Family
ID=47843778
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1301223.2A Withdrawn GB2510121A (en) | 2013-01-24 | 2013-01-24 | An aircraft electrical generator supplemented by an energy store until the generator is ramped up to meet the load requirement. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2510121A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110114951A (en) * | 2016-12-27 | 2019-08-09 | 川崎重工业株式会社 | Power-supply system |
CN110797957A (en) * | 2018-08-03 | 2020-02-14 | 通用电气航空系统有限责任公司 | Dynamically configurable energy storage unit |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20210351731A1 (en) * | 2020-05-08 | 2021-11-11 | Hamilton Sundstrand Corporation | Auxiliary power unit generator systems |
US11527975B2 (en) * | 2021-03-08 | 2022-12-13 | Hamilton Sundstrand Corporation | Low-power bias supply to facilitate the low-RPM startup of three-phase AC aircraft generators |
US11845388B2 (en) * | 2021-05-20 | 2023-12-19 | General Electric Company | AC electrical power system for a vehicle |
FR3129377B1 (en) * | 2021-11-25 | 2023-11-24 | Safran | POWER SUPPLY IN AN AIRCRAFT USING DRY CONTROL |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6031294A (en) * | 1998-01-05 | 2000-02-29 | Capstone Turbine Corporation | Turbogenerator/motor controller with ancillary energy storage/discharge |
US6624533B1 (en) * | 1999-08-04 | 2003-09-23 | Westerbeke Corporation | Controlling generator power |
US6737762B2 (en) * | 2001-10-26 | 2004-05-18 | Onan Corporation | Generator with DC boost for uninterruptible power supply system or for enhanced load pickup |
WO2008063575A2 (en) * | 2006-11-16 | 2008-05-29 | Cummins Power Generation Ip, Inc. | Electric power generation system and methods |
US7573145B2 (en) * | 2006-11-16 | 2009-08-11 | Cummins Power Generation Ip, Inc. | Electric power generation system controlled to reduce perception of operational changes |
EP2238330A1 (en) * | 2007-12-26 | 2010-10-13 | Carrier Corporation | Apparatus and method for boosting output of a generator set |
-
2013
- 2013-01-24 GB GB1301223.2A patent/GB2510121A/en not_active Withdrawn
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110114951A (en) * | 2016-12-27 | 2019-08-09 | 川崎重工业株式会社 | Power-supply system |
CN110797957A (en) * | 2018-08-03 | 2020-02-14 | 通用电气航空系统有限责任公司 | Dynamically configurable energy storage unit |
Also Published As
Publication number | Publication date |
---|---|
GB2510121A (en) | 2014-07-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB2520024B (en) | Electrical power system for an aircraft | |
GB201308292D0 (en) | Aircraft electrical system | |
EP2987001A4 (en) | Landing system for an aircraft | |
EP2954608A4 (en) | System and method for monitoring and control of appliances | |
GB201404245D0 (en) | System and method for determining aircraft operational parameters and enhancing aircraft operation | |
GB201320938D0 (en) | Aircraft electric breaking system | |
GB201514385D0 (en) | Computer system and control method for computer system | |
GB201306565D0 (en) | Aircraft Electrical System Operating Method | |
PL2893169T3 (en) | Method and system for starting an aircraft turboengine | |
GB201219925D0 (en) | An electrical system for an aircraft | |
EP3015148A4 (en) | Control device, control system, and control method of aircraft | |
EP2984501A4 (en) | System and method for channel feedback for location time of flight | |
GB201320500D0 (en) | Solid state power controller for an aircraft | |
GB2519200B (en) | Method and system for controlling an isolated HV circuit | |
GB201412190D0 (en) | Method of optimization for an application | |
GB2522097B (en) | Aircraft control system and method | |
GB2530887B (en) | Electrical distribution system for an aircraft | |
GB201305461D0 (en) | Lift-reducing apparatus for aircraft wings | |
HK1205295A1 (en) | Aircraft control system | |
HK1203657A1 (en) | System and method for diet control | |
GB201301223D0 (en) | An electrical system for an aircraft anda method of control | |
SG11201507114QA (en) | Method and system for the temperature control of components | |
HK1206449A1 (en) | Method and apparatus for controlling aircraft control systems | |
HK1219179A1 (en) | An electrical control system and method | |
GB2514640B (en) | An aircraft instrumentation system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |