AR047151A1 - Unidades de expresion p gro y uso de las mismas en la regulacion de la transcripcion y la expresion de genes - Google Patents
Unidades de expresion p gro y uso de las mismas en la regulacion de la transcripcion y la expresion de genesInfo
- Publication number
- AR047151A1 AR047151A1 ARP040104736A ARP040104736A AR047151A1 AR 047151 A1 AR047151 A1 AR 047151A1 AR P040104736 A ARP040104736 A AR P040104736A AR P040104736 A ARP040104736 A AR P040104736A AR 047151 A1 AR047151 A1 AR 047151A1
- Authority
- AR
- Argentina
- Prior art keywords
- expression
- nucleic acid
- transcription
- degree
- sequence
- Prior art date
Links
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/10—Adaptations for driving, or combinations with, electric generators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/107—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
- F02C3/113—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission with variable power transmission between rotors
-
- 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
- F05D2220/00—Application
- F05D2220/50—Application for auxiliary power units (APU's)
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Micro-Organisms Or Cultivation Processes Thereof (AREA)
Abstract
Se refiere al uso de secuencias de ácidos nucleicos para la regulacion de la transcripcion y la expresion de genes, a los nuevos promotores y unidades de expresion propiamente dichos, a procedimientos para la modificacion o activacion del grado de transcripcion y/o grado de expresion de genes, a casetes de expresion que contienen las unidades de expresion, a microorganismos modificados genéticamente con grado de transcripcion y/o grado de expresion modificado o activado, así como también a procedimientos para la preparacion de productos biosintéticos por medio del cultivo de los microorganismos genéticamente modificados. Reivindicacion 1: Uso de un ácido nucleico con actividad promotora, que contiene: A) la secuencia de ácidos nucleicos SEQ. ID. NO. 1 o B) una secuencia derivada de esta secuencia por sustitucion, insercion o delecion de nucleotidos, la que presenta una identidad de por lo menos 90 % a nivel de ácidos nucleicos con la secuencia SEQ. ID. NO. 1, o C) una secuencia de ácidos nucleicos, que hibrida con la secuencia de ácidos nucleicos SEQ. ID. NO. 1 bajo condiciones severas o D) fragmentos funcionalmente equivalentes de las secuencias de A), B) o C), para la transcripcion de genes.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10359559A DE10359559A1 (de) | 2003-12-18 | 2003-12-18 | Gasturbine, insbesondere Flugtriebwerk |
Publications (1)
Publication Number | Publication Date |
---|---|
AR047151A1 true AR047151A1 (es) | 2006-01-11 |
Family
ID=34683536
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ARP040104736A AR047151A1 (es) | 2003-12-18 | 2004-12-17 | Unidades de expresion p gro y uso de las mismas en la regulacion de la transcripcion y la expresion de genes |
Country Status (5)
Country | Link |
---|---|
US (1) | US7495354B2 (es) |
EP (1) | EP1694944B1 (es) |
AR (1) | AR047151A1 (es) |
DE (2) | DE10359559A1 (es) |
WO (1) | WO2005059316A1 (es) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2878286B1 (fr) * | 2004-11-25 | 2009-05-22 | Snecma Moteurs Sa | Turbomachine comportant un generateur de courant electrique integre |
FR2896537B1 (fr) | 2006-01-24 | 2011-07-29 | Snecma | Turbomachine a generateur-demarreur integre |
US7603864B2 (en) | 2006-11-29 | 2009-10-20 | General Electric Company | Blade tip electric machine |
US8198744B2 (en) * | 2006-12-21 | 2012-06-12 | General Electric Company | Integrated boost cavity ring generator for turbofan and turboshaft engines |
US7854582B2 (en) | 2007-05-08 | 2010-12-21 | Pratt & Whitney Canada Corp. | Operation of an aircraft engine after emergency shutdown |
US7926287B2 (en) | 2007-05-08 | 2011-04-19 | Pratt & Whitney Canada Corp. | Method of operating a gas turbine engine |
GB201112319D0 (en) * | 2011-07-18 | 2011-08-31 | Rolls Royce Plc | A electromagnetic component for a stator segment of an electrical machine |
WO2014137424A1 (en) | 2013-03-03 | 2014-09-12 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine |
EP2964891B1 (en) | 2013-03-05 | 2019-06-12 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine component arrangement |
WO2014163698A1 (en) | 2013-03-07 | 2014-10-09 | Vandervaart Peter L | Cooled gas turbine engine component |
DE102013209388B4 (de) * | 2013-05-22 | 2021-07-22 | Robert Bosch Gmbh | Hybridantrieb für kraftgetriebenes Luftfahrzeug, kraftgetriebenes Luftfahrzeug mit Hybridantrieb und zugehöriges Betriebsverfahren |
US10000293B2 (en) | 2015-01-23 | 2018-06-19 | General Electric Company | Gas-electric propulsion system for an aircraft |
US9938853B2 (en) | 2015-10-23 | 2018-04-10 | General Electric Company | Torsional damping for gas turbine engines |
US9764848B1 (en) | 2016-03-07 | 2017-09-19 | General Electric Company | Propulsion system for an aircraft |
US10308366B2 (en) | 2016-08-22 | 2019-06-04 | General Electric Company | Embedded electric machine |
US10487839B2 (en) | 2016-08-22 | 2019-11-26 | General Electric Company | Embedded electric machine |
US10071811B2 (en) | 2016-08-22 | 2018-09-11 | General Electric Company | Embedded electric machine |
US10093428B2 (en) | 2016-08-22 | 2018-10-09 | General Electric Company | Electric propulsion system |
US10793281B2 (en) | 2017-02-10 | 2020-10-06 | General Electric Company | Propulsion system for an aircraft |
US10822103B2 (en) | 2017-02-10 | 2020-11-03 | General Electric Company | Propulsor assembly for an aircraft |
US11149578B2 (en) | 2017-02-10 | 2021-10-19 | General Electric Company | Propulsion system for an aircraft |
US10762726B2 (en) | 2017-06-13 | 2020-09-01 | General Electric Company | Hybrid-electric propulsion system for an aircraft |
US11156128B2 (en) | 2018-08-22 | 2021-10-26 | General Electric Company | Embedded electric machine |
US11097849B2 (en) | 2018-09-10 | 2021-08-24 | General Electric Company | Aircraft having an aft engine |
FR3087819B1 (fr) * | 2018-10-26 | 2020-11-13 | Safran Aircraft Engines | Turbomachine d'aeronef equipee d'une machine electrique |
US11539316B2 (en) | 2019-07-30 | 2022-12-27 | General Electric Company | Active stability control of compression systems utilizing electric machines |
US11661856B2 (en) | 2021-03-19 | 2023-05-30 | Rolls-Royce North American Technologies Inc. | Gas turbine engine with embedded generator |
US11859552B2 (en) * | 2021-04-30 | 2024-01-02 | Rtx Corporation | Flow recirculative power system |
US11629640B2 (en) | 2021-09-08 | 2023-04-18 | Rolls-Royce North American Technologies Inc. | Oil pumping control for electrical oil pumping system |
US11702990B2 (en) | 2021-09-08 | 2023-07-18 | Rolls-Royce North American Technologies Inc. | Redundant electrically driven fuel and oil pumping system for gas turbine with bidirectional pump motor |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1041587A (en) * | 1962-08-27 | 1966-09-07 | Bristol Siddeley Engines Ltd | Improvements in gas turbine engines |
US4514991A (en) * | 1983-10-17 | 1985-05-07 | Carrier Corporation | Variable speed drive motor system with inverter control |
DE4131713A1 (de) | 1991-09-24 | 1993-04-08 | Mtu Muenchen Gmbh | Zusatzverdichter fuer fantriebwerke mit hohem bypass-verhaeltnis |
US5309029A (en) * | 1993-06-18 | 1994-05-03 | The United States Of America As Represented By The Secretary Of The Air Force | Aircraft power unit with elective mechanical coupling |
US5497615A (en) * | 1994-03-21 | 1996-03-12 | Noe; James C. | Gas turbine generator set |
GB9606546D0 (en) | 1996-03-28 | 1996-06-05 | Rolls Royce Plc | Gas turbine engine system |
US6294842B1 (en) * | 1997-12-19 | 2001-09-25 | Alliedsignal Inc. | Fog cycle for microturbine power generating system |
US6158210A (en) * | 1998-12-03 | 2000-12-12 | General Electric Company | Gear driven booster |
JP2000350414A (ja) * | 1999-06-03 | 2000-12-15 | Hitachi Ltd | タービン発電機の運転方法 |
US6355987B1 (en) * | 2000-06-27 | 2002-03-12 | General Electric Company | Power converter and control for microturbine |
FR2842565B1 (fr) * | 2002-07-17 | 2005-01-28 | Snecma Moteurs | Demarreur-generateur integre pour turbomachine |
US6895741B2 (en) * | 2003-06-23 | 2005-05-24 | Pratt & Whitney Canada Corp. | Differential geared turbine engine with torque modulation capability |
US7285871B2 (en) * | 2004-08-25 | 2007-10-23 | Honeywell International, Inc. | Engine power extraction control system |
-
2003
- 2003-12-18 DE DE10359559A patent/DE10359559A1/de not_active Withdrawn
-
2004
- 2004-11-20 US US10/582,917 patent/US7495354B2/en not_active Expired - Fee Related
- 2004-11-20 EP EP04802783A patent/EP1694944B1/de not_active Not-in-force
- 2004-11-20 WO PCT/DE2004/002572 patent/WO2005059316A1/de active IP Right Grant
- 2004-11-20 DE DE502004006868T patent/DE502004006868D1/de active Active
- 2004-12-17 AR ARP040104736A patent/AR047151A1/es not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
EP1694944B1 (de) | 2008-04-16 |
EP1694944A1 (de) | 2006-08-30 |
DE10359559A1 (de) | 2005-07-28 |
DE502004006868D1 (de) | 2008-05-29 |
US7495354B2 (en) | 2009-02-24 |
WO2005059316A1 (de) | 2005-06-30 |
US20070152534A1 (en) | 2007-07-05 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FA | Abandonment or withdrawal |