RU2581754C2 - Отказоустойчивая система управления для распределенных микродвижителей - Google Patents
Отказоустойчивая система управления для распределенных микродвижителей Download PDFInfo
- Publication number
- RU2581754C2 RU2581754C2 RU2013144217/06A RU2013144217A RU2581754C2 RU 2581754 C2 RU2581754 C2 RU 2581754C2 RU 2013144217/06 A RU2013144217/06 A RU 2013144217/06A RU 2013144217 A RU2013144217 A RU 2013144217A RU 2581754 C2 RU2581754 C2 RU 2581754C2
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- Russia
- Prior art keywords
- power lines
- layer
- power
- micromotors
- micromotor
- Prior art date
Links
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Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H1/00—Using plasma to produce a reactive propulsive thrust
- F03H1/0037—Electrostatic ion thrusters
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/46—Feeding propellants using pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/62—Combustion or thrust chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H1/00—Using plasma to produce a reactive propulsive thrust
- F03H1/0006—Details applicable to different types of plasma thrusters
- F03H1/0018—Arrangements or adaptations of power supply systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H99/00—Subject matter not provided for in other groups of this subclass
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/40—Use of a multiplicity of similar components
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/09—Purpose of the control system to cope with emergencies
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/60—Control system actuates means
- F05D2270/62—Electrical actuators
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Resistance Heating (AREA)
- Power Sources (AREA)
- Supply And Distribution Of Alternating Current (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US201161448621P | 2011-03-02 | 2011-03-02 | |
| US61/448,621 | 2011-03-02 | ||
| PCT/US2012/027324 WO2012118994A2 (en) | 2011-03-02 | 2012-03-01 | Fault tolerant control system for distributed micro-thrusters |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2013144217A RU2013144217A (ru) | 2015-04-10 |
| RU2581754C2 true RU2581754C2 (ru) | 2016-04-20 |
Family
ID=46758501
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2013144217/06A RU2581754C2 (ru) | 2011-03-02 | 2012-03-01 | Отказоустойчивая система управления для распределенных микродвижителей |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US9784251B2 (https=) |
| EP (1) | EP2681438B1 (https=) |
| JP (1) | JP6046645B2 (https=) |
| KR (1) | KR101525012B1 (https=) |
| IL (1) | IL228167B (https=) |
| RU (1) | RU2581754C2 (https=) |
| WO (1) | WO2012118994A2 (https=) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2012119039A1 (en) * | 2011-03-02 | 2012-09-07 | Game Changers, Llc | Apparatus and methods using non-fouling bypass filter |
| EP3406900A1 (en) | 2012-06-15 | 2018-11-28 | Game Changers, Llc | Micro thruster uses and improvements |
| JP2024534349A (ja) * | 2021-09-09 | 2024-09-20 | トーラミックス インク | ガスポンプを動作させる装置及び方法 |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2137621C1 (ru) * | 1998-12-24 | 1999-09-20 | Орлов Александр Борисович | Система активной безопасности транспортного средства |
| US6457306B1 (en) * | 1998-06-15 | 2002-10-01 | Lockheed Martin Corporation | Electrical drive system for rocket engine propellant pumps |
| RU2364551C2 (ru) * | 2004-10-06 | 2009-08-20 | Юрий Иванович Безруков | Дисколет |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS58179298U (ja) * | 1982-05-25 | 1983-11-30 | 株式会社東芝 | 冗長系リアクシヨンホイ−ルのモ−タコイル装置 |
| JPH02132501A (ja) | 1988-11-14 | 1990-05-22 | Toshiba Corp | 並列型駆動装置 |
| US5269131A (en) * | 1992-08-25 | 1993-12-14 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Segmented ion thruster |
| US6597073B1 (en) * | 1998-02-18 | 2003-07-22 | Compaq Information Technologies Group, L.P. | Circuit and method for providing power supply redundancy |
| FR2802335B1 (fr) | 1999-12-09 | 2002-04-05 | Cit Alcatel | Systeme et procede de controle de minienvironnement |
| US6683392B2 (en) * | 2001-08-20 | 2004-01-27 | The Boeing Company | Switch matrix |
| US7703273B2 (en) * | 2002-11-01 | 2010-04-27 | Marcy Dulligan, legal representative | Dual-mode chemical-electric thrusters for spacecraft |
| US20060000215A1 (en) | 2004-07-01 | 2006-01-05 | Kremen Stanley H | Encapsulated radiometric engine |
| US20060001569A1 (en) * | 2004-07-01 | 2006-01-05 | Marco Scandurra | Radiometric propulsion system |
| SE530415C2 (sv) * | 2006-09-04 | 2008-05-27 | Nanospace Ab | Gastrustor |
| US7690187B2 (en) | 2006-09-26 | 2010-04-06 | The Aerospace Corporation | Modular micropropulsion device and system |
| JP2010213443A (ja) | 2009-03-10 | 2010-09-24 | Omron Corp | 電力調整器 |
| EP2473785B1 (en) * | 2009-09-03 | 2018-06-13 | Game Changers, Llc | Nanomolecular solid state electrodynamic thruster |
| US9086060B1 (en) * | 2012-10-31 | 2015-07-21 | The Boeing Company | Telemetry for testing switch configuration in ion propulsion system |
-
2012
- 2012-03-01 RU RU2013144217/06A patent/RU2581754C2/ru not_active IP Right Cessation
- 2012-03-01 EP EP12751939.5A patent/EP2681438B1/en not_active Not-in-force
- 2012-03-01 US US14/001,890 patent/US9784251B2/en not_active Expired - Fee Related
- 2012-03-01 JP JP2013556870A patent/JP6046645B2/ja not_active Expired - Fee Related
- 2012-03-01 WO PCT/US2012/027324 patent/WO2012118994A2/en not_active Ceased
- 2012-03-01 KR KR1020137026006A patent/KR101525012B1/ko not_active Expired - Fee Related
-
2013
- 2013-08-28 IL IL228167A patent/IL228167B/en active IP Right Grant
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6457306B1 (en) * | 1998-06-15 | 2002-10-01 | Lockheed Martin Corporation | Electrical drive system for rocket engine propellant pumps |
| RU2137621C1 (ru) * | 1998-12-24 | 1999-09-20 | Орлов Александр Борисович | Система активной безопасности транспортного средства |
| RU2364551C2 (ru) * | 2004-10-06 | 2009-08-20 | Юрий Иванович Безруков | Дисколет |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2014514482A (ja) | 2014-06-19 |
| RU2013144217A (ru) | 2015-04-10 |
| KR101525012B1 (ko) | 2015-06-03 |
| US20140075917A1 (en) | 2014-03-20 |
| WO2012118994A3 (en) | 2012-10-26 |
| EP2681438A2 (en) | 2014-01-08 |
| EP2681438A4 (en) | 2015-04-29 |
| WO2012118994A2 (en) | 2012-09-07 |
| IL228167B (en) | 2018-02-28 |
| EP2681438B1 (en) | 2019-01-23 |
| US9784251B2 (en) | 2017-10-10 |
| JP6046645B2 (ja) | 2016-12-21 |
| KR20130133276A (ko) | 2013-12-06 |
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