RU93018913A - FINISHING THE BEARING SURFACE - Google Patents

FINISHING THE BEARING SURFACE

Info

Publication number
RU93018913A
RU93018913A RU93018913/23A RU93018913A RU93018913A RU 93018913 A RU93018913 A RU 93018913A RU 93018913/23 A RU93018913/23 A RU 93018913/23A RU 93018913 A RU93018913 A RU 93018913A RU 93018913 A RU93018913 A RU 93018913A
Authority
RU
Russia
Prior art keywords
finishing
bearing surface
vortex
design
tip
Prior art date
Application number
RU93018913/23A
Other languages
Russian (ru)
Other versions
RU2072946C1 (en
Inventor
В.Т. Шведов
Original Assignee
В.Т. Шведов
Filing date
Publication date
Application filed by В.Т. Шведов filed Critical В.Т. Шведов
Priority to RU9393018913A priority Critical patent/RU2072946C1/en
Priority claimed from RU9393018913A external-priority patent/RU2072946C1/en
Publication of RU93018913A publication Critical patent/RU93018913A/en
Application granted granted Critical
Publication of RU2072946C1 publication Critical patent/RU2072946C1/en

Links

Claims (1)

Изобретение относится к авиации и может быть использовано в конструкции законцовок несущих поверхностей летательных аппаратов. Для создания простой, надежной конструкции законцовки, избавляющей несущую поверхность от вредного влияния концевого вихря и улучшающей ее аэродинамические характеристики законцовка снабжена генератором вихревого потока, противоположного по направлению вращения концевому вихрю, выполненным в виде гондолы, снабженной направляющим лопаточным аппаратом, работающим от набегающего потока.The invention relates to aviation and can be used in the design of the ends of the bearing surfaces of aircraft. To create a simple, reliable tip design, relieving the carrier surface from the harmful influence of an end vortex and improving its aerodynamic characteristics, the tip is equipped with a vortex flow generator opposite to the end vortex in the direction of rotation, fitted with a guide vane operating from an incident flow.
RU9393018913A 1993-04-14 1993-04-14 Flying vehicle lifting surface tip RU2072946C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU9393018913A RU2072946C1 (en) 1993-04-14 1993-04-14 Flying vehicle lifting surface tip

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU9393018913A RU2072946C1 (en) 1993-04-14 1993-04-14 Flying vehicle lifting surface tip

Publications (2)

Publication Number Publication Date
RU93018913A true RU93018913A (en) 1995-08-27
RU2072946C1 RU2072946C1 (en) 1997-02-10

Family

ID=20140185

Family Applications (1)

Application Number Title Priority Date Filing Date
RU9393018913A RU2072946C1 (en) 1993-04-14 1993-04-14 Flying vehicle lifting surface tip

Country Status (1)

Country Link
RU (1) RU2072946C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2174483C2 (en) * 1998-07-13 2001-10-10 Центральный аэрогидродинамический институт им. проф. Н.Е. Жуковского Device for attenuation of vortex wake of high-lift wing (versions)

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