RETRACTABLE TURBULENCE PROMOTER TO REDUCE STALL SPEED Russian patent published in 2016 - IPC B64C23/06 B64C9/12 

Abstract RU 2600014 C2

FIELD: aviation.

SUBSTANCE: method of bearing surface flight at low speeds includes deviation of bearing surface front edge high-lift system component, extending turbulence promoter movably connected to high-lift system component of front edge from slot the bearing surface and removal of turbulence promoter under bearing surface in response to movement of bearing surface front edge high-lift system component in nominal position. Extensible turbulence promoter comprises front edge high-lift system component attached to bearing surface, aerodynamic surface attached to bearing surface and sliding turbulence promoter connected to bearing surface, front edge high-lift system component or to both of them. Method of bearing surface controlling at low speeds of comprises enabling bearing surface flowing with flowing medium, lowering of front edge high-lift system component leading edge pivotally connected to bearing surface from nominal position into deflected position; opening of several retractable turbulators through slots in first bearing surface in response to lowering of deflected leading edge high-lift system component. Extending turbulence promoters are made with possibility of their closure under high-lift system component rear edge while front edge high-lift system component is in nominal position.

EFFECT: group of inventions is aimed at high efficiency of bearing surface operation at low speed.

20 cl, 10 dwg

Similar patents RU2600014C2

Title Year Author Number
AIRCRAFT WITH AERODYNAMIC ELEMENT AND METHOD OF ITS FLYING 2012
  • Arvin Shmilovich
  • Abdollakh Kkhodadoust
RU2597046C2
SPOILER AILERON OF AIRCRAFT AIRFRAME STREAMLINED SECTION 2008
  • Foss Timo
  • Lerke Joakhim
RU2452657C2
ROTARY-WINGED AIRCRAFT MAIN ROTOR BLADE WITH IMPROVED AIRCRAFT PERFORMANCE 2013
  • David L. Perlman
RU2631758C2
ROTATION-DRIVEN AILERON, SET WITH A GAP AND CREATING HIGH LIFT 2013
  • Kordel Dzhen A.
  • Sakuraj Sejya
RU2625384C2
ROTABLE INCLINED WING END 2013
  • Dis Pol V
  • Gud Mark S
  • Sakurai Sejya
  • Kordel Yan A
  • Foks Stefen Dzhej
  • Lassen Mettyu A
  • Foks Bryus Robert
  • Uolker Stiven Pol
  • Santini Gregori M
RU2648303C2
DEVICE AND METHOD TO DESCRIBE LIFT 2006
  • Bender Klaus
  • Boehttger Ole
RU2399553C2
AIRCRAFT CONFIGURATION HAVING SPIN RESISTANCE 2013
  • Dzhionta Mettyu
  • Karkov Zhon
  • Ronts Dzhon
  • Keler Diter
  • Lednitser Devid
RU2640669C2
WINGLET ATTACH FITTING AND METHOD FOR ATTACHING SPLIT WINGLET TO WING 2014
  • Vitte Filipp
  • Kempbell Darrel D. Dzhr.
  • Tang Billi P.
  • Kleshchev Fedor
RU2667437C2
ELASTOMER CONTROL SURFACE BASED ON CONTINUOUS BYPASSING PROCESSING TECHNOLOGY 2013
  • Dzheders Pol F.
RU2625478C2
SYSTEM OF STREAMLINED BODY WITH VARIABLE PROFILE CURVATURE AND CONTROL METHOD OF ITS CONFIGURATION (VERSIONS) 2012
  • Mushumi Shoum
  • Frederik T. Kalkins
  • Dzhejms Khenri Mejb
  • Mattyu Todd Grimsho
RU2597624C2

RU 2 600 014 C2

Authors

Bryus R. Foks

Stiven Dzh. Foks

Dates

2016-10-20Published

2012-07-03Filed