REVERSE-THRUST DEVICE Russian patent published in 2014 - IPC F02K1/76 

Abstract RU 2525884 C2

FIELD: engines and pumps.

SUBSTANCE: proposed device comprises at least one cowl arranged to displace between closed and open positions and driven by at least one motor-controlled actuator. Every motor is connected to two separate power source. Note here that every motor represents a two-winding motor, every winding being connected to power supply other than that of another winding.

EFFECT: higher reliability.

9 cl, 3 dwg

Similar patents RU2525884C2

Title Year Author Number
CONTROL SYSTEM OF ELECTRIC DEVICE OF NACELLE 2011
  • Maalioune Hakim
RU2572730C2
THRUST REVERSER HYDRAULIC CONTROL SYSTEM 2011
  • Le Coq Vincent Pierre Germain
RU2570303C2
TURBOJET NACELLE CONTROL SYSTEM 2008
  • Kubiak Benoît
RU2470174C2
AIRCRAFT CONTROL SYSTEM 2011
  • Maalioune Hakim
RU2556474C2
CONTROL SYSTEM FOR TURBOJET ENGINE NACELLE AND NACELLE EQUIPPED WITH SUCH SYSTEM 2010
  • Maalioune Hakim
  • Le-Coq Vincent
  • Moradell-Casellas Pierre
  • Hadjidj Djemouai
  • Garcia Soto Cuillermo
RU2531204C2
THRUST REVERSER ACTUATOR WITH ADJUSTABLE NOZZLE FOR TURBOJET ENGINE NACELLE AND NACELLE WITH SUCH DEVICE 2011
  • Vauchel Guy Bernard
  • Gonidec Patrick
RU2570791C2
AUTOMATIC ADJUSTMENT METHOD OF ELECTRIC POWER CYLINDERS OF JET TURBINE ENGINE NACELLE 2008
  • Marin-Martinod Thierry
  • Maalioune Hakim
RU2459100C2
POWER SUPPLY CIRCUIT FOR TURBOJET ENGINE NACELLE 2010
  • Pereira David
  • Maalioune Hakim
  • Le Coq Vincent
RU2561613C2
TURBOJET THRUST REVERSER WITH CONTROLLED-CROSS-SECTION ADJUSTABLE NOZZLE SECTION AND TURBOJET NACELLE 2011
  • Vauchel Guy Bernard
  • Joret Jean-Philippe
  • Le Boulicaut Loic
  • Avenel Philippe
RU2568362C2
NACELLE FOR AIRCRAFT ENGINE WITH NOZZLE OF VARIABLE CROSS SECTION 2011
  • Voshel' Gi Bernar
  • Moradel'-Kasella P'Er
  • Le Buliko Loik
RU2553833C2

RU 2 525 884 C2

Authors

Maalioune Hakim

Dates

2014-08-20Published

2010-03-18Filed