FAIRING OF EXTENSION AND RETRACTION MECHANISM FOR EXTENSION FLAPS Russian patent published in 1997 - IPC

Abstract RU 2085441 C1

FIELD: aeronautical engineering; manufacture of aircraft with extension flaps. SUBSTANCE: tail section of fairing has end shear from trailing edge of flap at angle of ±45^° relative to plane perpendicular to wing chord smoothly changing to smooth lines at altitudes exceeding its width. EFFECT: reduction of mass and simplification of construction of fairing. 9 dwg

Similar patents RU2085441C1

Title	Year	Author	Number
CONTROL SURFACES WITH AXIAL COMPENSATION	1997	Frolishchev B.N.	RU2116222C1
ADAPTIVE WING	1990	Amir'Jants G.A.	SU1762488A1
SHORT TAKE-OFF AND LANDING AIRCRAFT	1996	Zhulev Ju.G. Zaretskij S.A. Kazhan V.G.	RU2103199C1
DEVICE FOR ATTENUATION OF VORTEX WAKE OF HIGH-LIFT WING (VERSIONS)	1998	Vozhdaev E.S. Golovkin M.A. Golovkin V.A. Gorban' V.P. Kaljavkin V.M.	RU2174483C2
AIRCRAFT WING	2003	Frolishchev B.N.	RU2242400C1
METHOD OF ENHANCING LIFT QUALITIES OF WINGS	1995	Zhulev Ju.G. Inshakov S.I. Kazhan V.G.	RU2104220C1
AIRCRAFT WING TIP	2000	Frolishchev B.N.	RU2173655C1
ACTIVE SYSTEM FOR CONTROL OF LIFTING FORCE	1994	Vlasov V.A. Ganich G.A. Zhulev Ju.G.	RU2086469C1
AIRCRAFT	1993	Konovalov S.F.	RU2076826C1
VERSATILE AERODYNAMIC MODEL AND METHOD OF ITS PRODUCTION	1994	Amir'Jants G.A.	RU2083967C1

RU 2 085 441 C1

Authors

Frolishchev B.N.

Vorob'Ev Ju.V.

Dzhamgarov S.G.

Dates

1997-07-27—Published

1995-04-18—Filed