BR112017000294A2 - conversor para uma aeronave, e aeronave - Google Patents
conversor para uma aeronave, e aeronaveInfo
- Publication number
- BR112017000294A2 BR112017000294A2 BR112017000294A BR112017000294A BR112017000294A2 BR 112017000294 A2 BR112017000294 A2 BR 112017000294A2 BR 112017000294 A BR112017000294 A BR 112017000294A BR 112017000294 A BR112017000294 A BR 112017000294A BR 112017000294 A2 BR112017000294 A2 BR 112017000294A2
- Authority
- BR
- Brazil
- Prior art keywords
- circuit
- voltage
- series
- converter
- aircraft
- Prior art date
Links
- 238000010276 construction Methods 0.000 abstract 1
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
- H02M5/00—Conversion of ac power input into ac power output, e.g. for change of voltage, for change of frequency, for change of number of phases
- H02M5/40—Conversion of ac power input into ac power output, e.g. for change of voltage, for change of frequency, for change of number of phases with intermediate conversion into dc
- H02M5/42—Conversion of ac power input into ac power output, e.g. for change of voltage, for change of frequency, for change of number of phases with intermediate conversion into dc by static converters
- H02M5/44—Conversion of ac power input into ac power output, e.g. for change of voltage, for change of frequency, for change of number of phases with intermediate conversion into dc by static converters using discharge tubes or semiconductor devices to convert the intermediate dc into ac
- H02M5/453—Conversion of ac power input into ac power output, e.g. for change of voltage, for change of frequency, for change of number of phases with intermediate conversion into dc by static converters using discharge tubes or semiconductor devices to convert the intermediate dc into ac using devices of a triode or transistor type requiring continuous application of a control signal
- H02M5/458—Conversion of ac power input into ac power output, e.g. for change of voltage, for change of frequency, for change of number of phases with intermediate conversion into dc by static converters using discharge tubes or semiconductor devices to convert the intermediate dc into ac using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K19/00—Synchronous motors or generators
- H02K19/16—Synchronous generators
- H02K19/34—Generators with two or more outputs
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
- H02M7/00—Conversion of ac power input into dc power output; Conversion of dc power input into ac power output
- H02M7/02—Conversion of ac power input into dc power output without possibility of reversal
- H02M7/04—Conversion of ac power input into dc power output without possibility of reversal by static converters
- H02M7/12—Conversion of ac power input into dc power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode
- H02M7/21—Conversion of ac power input into dc power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal
- H02M7/217—Conversion of ac power input into dc power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only
- H02M7/25—Conversion of ac power input into dc power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only arranged for operation in series, e.g. for multiplication of voltage
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
- H02M7/00—Conversion of ac power input into dc power output; Conversion of dc power input into ac power output
- H02M7/42—Conversion of dc power input into ac power output without possibility of reversal
- H02M7/44—Conversion of dc power input into ac power output without possibility of reversal by static converters
- H02M7/48—Conversion of dc power input into ac power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode
- H02M7/53—Conversion of dc power input into ac power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal
- H02M7/537—Conversion of dc power input into ac power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only, e.g. single switched pulse inverters
- H02M7/5387—Conversion of dc power input into ac power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only, e.g. single switched pulse inverters in a bridge configuration
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P27/00—Arrangements or methods for the control of AC motors characterised by the kind of supply voltage
- H02P27/04—Arrangements or methods for the control of AC motors characterised by the kind of supply voltage using variable-frequency supply voltage, e.g. inverter or converter supply voltage
- H02P27/06—Arrangements or methods for the control of AC motors characterised by the kind of supply voltage using variable-frequency supply voltage, e.g. inverter or converter supply voltage using dc to ac converters or inverters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D2221/00—Electric power distribution systems onboard aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
- H02M1/00—Details of apparatus for conversion
- H02M1/0067—Converter structures employing plural converter units, other than for parallel operation of the units on a single load
- H02M1/0074—Plural converter units whose inputs are connected in series
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
- H02M1/00—Details of apparatus for conversion
- H02M1/32—Means for protecting converters other than automatic disconnection
- H02M1/325—Means for protecting converters other than automatic disconnection with means for allowing continuous operation despite a fault, i.e. fault tolerant converters
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
- H02M3/00—Conversion of dc power input into dc power output
- H02M3/02—Conversion of dc power input into dc power output without intermediate conversion into ac
- H02M3/04—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters
- H02M3/10—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode
- H02M3/145—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal
- H02M3/155—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only
- H02M3/156—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only with automatic control of output voltage or current, e.g. switching regulators
- H02M3/158—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only with automatic control of output voltage or current, e.g. switching regulators including plural semiconductor devices as final control devices for a single load
- H02M3/1588—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only with automatic control of output voltage or current, e.g. switching regulators including plural semiconductor devices as final control devices for a single load comprising at least one synchronous rectifier element
-
- 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
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B70/00—Technologies for an efficient end-user side electric power management and consumption
- Y02B70/10—Technologies improving the efficiency by using switched-mode power supplies [SMPS], i.e. efficient power electronics conversion e.g. power factor correction or reduction of losses in power supplies or efficient standby modes
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Inverter Devices (AREA)
- Rectifiers (AREA)
Abstract
a presente invenção refere-se a um conversor (1) para um aeroplano, compreendendo um circuito intermediário (3), para proporcionar uma tensão cc (18) entre uma linha positiva (15) e uma linha negativa (16), pelo menos dois retificadores (7) conectados ao circuito intermediário (3), para produzir a tensão cc (18) de tensões ca de entrada, e pelo menos dois inversores (19) conectados ao circuito intermediário (3), para produzir as tensões ca de saída da tensão cc (18). o conversor deve ser configurado de uma maneira compacta para construção da aeronave. para esse fim, os terminais da tensão cc (11) dos retificadores (7) são conectados a um primeiro circuito em série (14), e os terminais da tensão cc (11) dos inversores (19) são conectados a um segundo circuito em série (21). a linha positiva (15) e a linha negativa (16) do circuito intermediário (3) são conectadas, no lado de entrada, pelo primeiro circuito em série (14), e, no lado de saída, pelo segundo circuito em série (21). pelo menos um dos terminais de tensão cc (11) compreende um circuito em curto (s1, 9) para os contatos de terminais em curto-circuito (12), pelos quais o terminal de tensão cc (11) é conectado ao respectivo circuito em série (14, 21).
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102014213307 | 2014-07-09 | ||
DE102015207117.0A DE102015207117A1 (de) | 2014-07-09 | 2015-04-20 | Umrichter mit redundanter Schaltungstopologie |
PCT/EP2015/061932 WO2016005101A1 (de) | 2014-07-09 | 2015-05-29 | Umrichter mit redundanter schaltungstopologie |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112017000294A2 true BR112017000294A2 (pt) | 2017-10-31 |
Family
ID=54867121
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112017000294A BR112017000294A2 (pt) | 2014-07-09 | 2015-05-29 | conversor para uma aeronave, e aeronave |
Country Status (7)
Country | Link |
---|---|
US (1) | US10287030B2 (pt) |
EP (1) | EP3143686A1 (pt) |
CN (1) | CN106471724B (pt) |
BR (1) | BR112017000294A2 (pt) |
CA (1) | CA2954461A1 (pt) |
DE (1) | DE102015207117A1 (pt) |
WO (1) | WO2016005101A1 (pt) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102015206627A1 (de) * | 2014-07-09 | 2016-01-28 | Siemens Aktiengesellschaft | Selbstsichernder Umrichter |
US10093250B2 (en) * | 2014-10-16 | 2018-10-09 | The Boeing Company | Aircraft supplemental electrical power systems and methods |
DE102015207187B4 (de) * | 2015-04-21 | 2016-11-17 | Siemens Aktiengesellschaft | Umrichter mit Kurzschlussunterbrechung in einer Halbbrücke |
US10093428B2 (en) * | 2016-08-22 | 2018-10-09 | General Electric Company | Electric propulsion system |
US10703496B2 (en) * | 2017-04-21 | 2020-07-07 | General Electric Company | Propulsion system for an aircraft |
KR102413474B1 (ko) * | 2017-05-31 | 2022-06-27 | 파나소닉 아이피 매니지먼트 가부시키가이샤 | 진단 장치 |
US10199977B1 (en) * | 2017-10-13 | 2019-02-05 | Garrett Transportation I Inc. | Electrical systems having interleaved DC interconnects |
DE102017220941A1 (de) | 2017-11-23 | 2019-05-23 | Siemens Aktiengesellschaft | Elektrische Maschine mit erhöhter Betriebssicherheit |
DE102018201206A1 (de) | 2018-01-26 | 2019-08-01 | Siemens Aktiengesellschaft | Modulare Anordnung eines Umrichters und Luftfahrzeug mit einer derartigen Anordnung |
DE102018206336A1 (de) | 2018-04-25 | 2019-10-31 | Bayerische Motoren Werke Aktiengesellschaft | Vorrichtung zum Absichern einer elektrischen Maschine |
DE102018216485A1 (de) * | 2018-09-26 | 2020-03-26 | Siemens Aktiengesellschaft | PV-Einrichtung mit verbesserter Gesamteffizienz |
DE102018216607A1 (de) | 2018-09-27 | 2020-04-02 | Siemens Aktiengesellschaft | PV-Einrichtung mit reduzierter Alterung |
DE102019206872A1 (de) * | 2019-05-13 | 2020-11-19 | Rolls-Royce Deutschland Ltd & Co Kg | Minimalistischer Stromrichter und Fahrzeug mit einem Stromrichter |
GB2589633B (en) | 2019-12-06 | 2022-01-05 | Rolls Royce Plc | Electrical systems |
GB2589634B (en) | 2019-12-06 | 2024-05-29 | Rolls Royce Plc | Electrical systems |
US11128251B1 (en) * | 2020-04-29 | 2021-09-21 | The Boeing Company | Fault-tolerant power system architecture for aircraft electric propulsion |
EP3955443A1 (de) * | 2020-08-12 | 2022-02-16 | Siemens Aktiengesellschaft | Fehlertoleranter betrieb eines stromrichters |
US11682535B2 (en) | 2021-03-12 | 2023-06-20 | Essex Industries, Inc. | Rocker switch |
WO2022197730A1 (en) | 2021-03-15 | 2022-09-22 | Essex Industries, Inc. | Five-position switch |
FR3125656A1 (fr) * | 2021-07-26 | 2023-01-27 | Safran Electrical & Power | Système propulsif électrique d’aéronef |
US11670942B2 (en) | 2021-09-23 | 2023-06-06 | General Electric Company | Electrically driven distributed propulsion system |
US20240178741A1 (en) * | 2022-11-30 | 2024-05-30 | Infineon Technologies Austria Ag | Power converter having a solid-state transformer and a half bridge converter stage for each isolated dc output of the solid-state transformer |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5023537A (en) * | 1989-08-23 | 1991-06-11 | Sundstrand Corporation | Low frequency feeder fault protection |
US6894418B2 (en) | 2002-07-30 | 2005-05-17 | Comprehensive Power, Inc. | Nested stator coils for permanent magnet machines |
US20070230226A1 (en) * | 2003-11-25 | 2007-10-04 | Jih-Sheng Lai | Multilevel intelligent universal auto-transformer |
EP1974454A4 (en) | 2006-01-18 | 2017-03-01 | ABB Technology Ltd | A transmission system and a method for control thereof |
DE102006031662A1 (de) * | 2006-07-08 | 2008-01-10 | Semikron Elektronik Gmbh & Co. Kg | Stromrichterschaltungsanordnung für eine Hochvoltgleichspannungsverbindung |
US7851943B2 (en) * | 2006-12-08 | 2010-12-14 | General Electric Company | Direct current power transmission and distribution system |
US8002216B2 (en) * | 2007-06-15 | 2011-08-23 | Darwin Kent Decker | Solar powered wing vehicle using flywheels for energy storage |
US9768704B2 (en) * | 2009-02-06 | 2017-09-19 | Abb Research Ltd. | Hybrid distribution transformer having a power electronic module for controlling input power factor and output voltage |
EP2226923B1 (en) | 2009-03-03 | 2015-06-10 | GE Energy Power Conversion Technology Limited | Coils |
US9362839B2 (en) * | 2011-02-09 | 2016-06-07 | Rockwell Automation Technologies, Inc. | Power converter with common mode voltage reduction |
US8379417B2 (en) * | 2011-07-06 | 2013-02-19 | Rockwell Automation Technologies, Inc. | Power converter and integrated DC choke therefor |
US9143029B2 (en) * | 2011-12-15 | 2015-09-22 | General Electric Company | System and method for power distribution |
EP2608397A1 (de) * | 2011-12-19 | 2013-06-26 | Siemens Aktiengesellschaft | Modularer Hochfrequenz-Umrichter für Antriebe |
EP2608383A1 (de) | 2011-12-19 | 2013-06-26 | Siemens Aktiengesellschaft | Stromrichterschaltung |
DE102012219243A1 (de) | 2012-10-22 | 2014-04-24 | Conti Temic Microelectronic Gmbh | Verfahren und Schaltungseinheit zum Ermitteln von Fehlerzuständen einer Halbbrückenschaltung |
-
2015
- 2015-04-20 DE DE102015207117.0A patent/DE102015207117A1/de not_active Withdrawn
- 2015-05-29 CN CN201580036737.1A patent/CN106471724B/zh active Active
- 2015-05-29 US US15/324,540 patent/US10287030B2/en active Active
- 2015-05-29 WO PCT/EP2015/061932 patent/WO2016005101A1/de active Application Filing
- 2015-05-29 EP EP15726583.6A patent/EP3143686A1/de not_active Ceased
- 2015-05-29 CA CA2954461A patent/CA2954461A1/en not_active Abandoned
- 2015-05-29 BR BR112017000294A patent/BR112017000294A2/pt not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
US20170197730A1 (en) | 2017-07-13 |
US10287030B2 (en) | 2019-05-14 |
CN106471724B (zh) | 2019-04-05 |
CA2954461A1 (en) | 2016-01-14 |
EP3143686A1 (de) | 2017-03-22 |
CN106471724A (zh) | 2017-03-01 |
DE102015207117A1 (de) | 2016-01-14 |
WO2016005101A1 (de) | 2016-01-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 4A ANUIDADE. |
|
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2517 DE 02-04-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |