MX360357B - Dispositivo productor de energía con mecanismo de control. - Google Patents
Dispositivo productor de energía con mecanismo de control.Info
- Publication number
- MX360357B MX360357B MX2015008722A MX2015008722A MX360357B MX 360357 B MX360357 B MX 360357B MX 2015008722 A MX2015008722 A MX 2015008722A MX 2015008722 A MX2015008722 A MX 2015008722A MX 360357 B MX360357 B MX 360357B
- Authority
- MX
- Mexico
- Prior art keywords
- power
- producing device
- controller
- control mechanism
- turbine
- Prior art date
Links
Classifications
-
- 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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/02—Arrangement of sensing elements
-
- 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
- B64D41/00—Power installations for auxiliary purposes
- B64D41/007—Ram air turbines
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
Un dispositivo de producción de energía, tal como una turbina de aire admitido en sentido de la marcha o dinámico, incluye un controlador que se utiliza para controlar la operación de una turbina del dispositivo de producción de energía. El controlador utiliza una entrada basada en una velocidad de aire de la aeronave como parte de un mecanismo de control en el controlador para controlar la turbina. Por ejemplo, el controlador puede ser utilizado para controlar la contrapresión de la turbina, por ejemplo, al controlar el ángulo de las puertas que se utilizan para ajustar la contrapresión de la turbina. El mecanismo de control puede incluir un controlador PID, con la ganancia de uno o más de los valores del controlador PID siendo una función de la velocidad de aire de la aeronave. Además, el mecanismo de control puede incluir manipular un punto de fijación como una función de carga en el dispositivo de producción de energía. El dispositivo de producción de energía puede ser parte de un compartimento desprendible que está instalado en la aeronave.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/734,236 US9371739B2 (en) | 2013-01-04 | 2013-01-04 | Power producing device with control mechanism |
PCT/US2013/075666 WO2014143273A2 (en) | 2013-01-04 | 2013-12-17 | Power-producing device with control mechanism |
Publications (2)
Publication Number | Publication Date |
---|---|
MX2015008722A MX2015008722A (es) | 2016-03-09 |
MX360357B true MX360357B (es) | 2018-10-30 |
Family
ID=51061073
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2015008722A MX360357B (es) | 2013-01-04 | 2013-12-17 | Dispositivo productor de energía con mecanismo de control. |
Country Status (4)
Country | Link |
---|---|
US (1) | US9371739B2 (es) |
EP (1) | EP2941384B1 (es) |
MX (1) | MX360357B (es) |
WO (1) | WO2014143273A2 (es) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3003845B1 (fr) * | 2013-04-02 | 2016-04-15 | Labinal | Systeme de recuperation et de conversion d'energie cinetique et d'energie potentielle en energie electrique pour aeronef |
ES2542557A1 (es) * | 2014-02-06 | 2015-08-06 | Alberto ADARVE LOZANO | Dispositivo de aplicación externa en vehículos móviles para conseguir energía eléctrica |
EP3341677A4 (en) | 2015-08-24 | 2019-04-24 | Leigh Aerosystems Corporation | SYSTEM FOR GUIDING GROUND PROJECTILE |
WO2017062563A1 (en) * | 2015-10-08 | 2017-04-13 | Leigh Aerosystems Corporation | Ground-projectile system |
EP3492386A1 (de) * | 2017-12-01 | 2019-06-05 | Dietmar Posch | Flugzeug mit stromversorgung |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4193005A (en) | 1978-08-17 | 1980-03-11 | United Technologies Corporation | Multi-mode control system for wind turbines |
US4587803A (en) * | 1983-08-15 | 1986-05-13 | Rolls-Royce Inc. | Valve for diverting fluid flows in turbomachines |
US4770368A (en) * | 1985-03-12 | 1988-09-13 | Southwest Aerospace Corporation | Turbine/air vent reeling machine |
US5184461A (en) * | 1990-05-11 | 1993-02-09 | General Electric Company | Method and apparatus for automatic bypass operation |
US5113649A (en) * | 1990-05-11 | 1992-05-19 | General Electric Company | Passive bypass valve assembly |
US5182905A (en) * | 1990-05-11 | 1993-02-02 | General Electric Company | Method for automatic bypass operation |
US5505587A (en) * | 1995-01-05 | 1996-04-09 | Northrop Grumman Corporation | RAM air turbine generating apparatus |
US5820074A (en) * | 1996-12-20 | 1998-10-13 | Sundstrand Corporation | Deployment mechanism for RAM air turbine |
US6270309B1 (en) * | 1998-12-14 | 2001-08-07 | Ghetzler Aero-Power Corporation | Low drag ducted Ram air turbine generator and cooling system |
US6865935B2 (en) | 2002-12-30 | 2005-03-15 | General Electric Company | System and method for steam turbine backpressure control using dynamic pressure sensors |
US6904353B1 (en) * | 2003-12-18 | 2005-06-07 | Honeywell International, Inc. | Method and system for sliding mode control of a turbocharger |
US20060137355A1 (en) * | 2004-12-27 | 2006-06-29 | Pratt & Whitney Canada Corp. | Fan driven emergency generator |
DE102005013099A1 (de) | 2005-02-16 | 2006-09-07 | Rainer Franke | System |
EP3141730A1 (en) * | 2006-10-12 | 2017-03-15 | United Technologies Corporation | Turbofan engine operation control |
US7841163B2 (en) * | 2006-11-13 | 2010-11-30 | Hamilton Sundstrand Corporation | Turbofan emergency generator |
DE102009010243A1 (de) | 2009-02-24 | 2010-09-02 | Airbus Deutschland Gmbh | Leistungserzeugungs-Vorrichtung sowie Rumpf-Bauteil mit einer solchen Leistungserzeugungs-Vorrichtung |
US8424800B2 (en) | 2010-06-23 | 2013-04-23 | Hamilton Sundstrand Corporation | Multi-source emergency power optimization |
US8653688B2 (en) | 2011-05-24 | 2014-02-18 | Advanced Technologies Group, Inc. | Submerged ram air turbine generating system |
US20130204544A1 (en) * | 2012-02-03 | 2013-08-08 | Gulfstream Aerospace Corporation | Methods and systems for determining airspeed of an aircraft |
SG194257A1 (en) * | 2012-04-26 | 2013-11-29 | Yik Hei Sia | Power generating windbags and water-bags |
GB201411975D0 (en) * | 2014-07-04 | 2014-08-20 | Rolls Royce Plc | Aircraft control method |
-
2013
- 2013-01-04 US US13/734,236 patent/US9371739B2/en active Active
- 2013-12-17 EP EP13870383.0A patent/EP2941384B1/en active Active
- 2013-12-17 WO PCT/US2013/075666 patent/WO2014143273A2/en active Application Filing
- 2013-12-17 MX MX2015008722A patent/MX360357B/es active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
WO2014143273A3 (en) | 2014-12-31 |
WO2014143273A2 (en) | 2014-09-18 |
MX2015008722A (es) | 2016-03-09 |
EP2941384B1 (en) | 2017-05-17 |
US9371739B2 (en) | 2016-06-21 |
EP2941384A2 (en) | 2015-11-11 |
US20140193236A1 (en) | 2014-07-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG | Grant or registration |