RU95106048A - Extension flap operating mechanism fairing - Google Patents

Extension flap operating mechanism fairing

Info

Publication number
RU95106048A
RU95106048A RU95106048/11A RU95106048A RU95106048A RU 95106048 A RU95106048 A RU 95106048A RU 95106048/11 A RU95106048/11 A RU 95106048/11A RU 95106048 A RU95106048 A RU 95106048A RU 95106048 A RU95106048 A RU 95106048A
Authority
RU
Russia
Prior art keywords
fairing
operating mechanism
extension flap
flap operating
flap
Prior art date
Application number
RU95106048/11A
Other languages
Russian (ru)
Other versions
RU2085441C1 (en
Inventor
Б.Н. Фролищев
Ю.В. Воробьев
С.Г. Джамгаров
Original Assignee
Центральный аэрогидродинамический институт им.проф.Н.Е.Жуковского
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Центральный аэрогидродинамический институт им.проф.Н.Е.Жуковского filed Critical Центральный аэрогидродинамический институт им.проф.Н.Е.Жуковского
Priority to RU9595106048A priority Critical patent/RU2085441C1/en
Publication of RU95106048A publication Critical patent/RU95106048A/en
Application granted granted Critical
Publication of RU2085441C1 publication Critical patent/RU2085441C1/en

Links

Classifications

    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Tires In General (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

FIELD: aeronautical engineering. SUBSTANCE: tail section of fairing has end shear from trailing edge of flap at angle of $$$ relative to plane perpendicular to wing chord smoothly changing to shedding outline at heights exceeding its width. EFFECT: reduced mass and simplified construction. 2 cl, 6 dwg

Claims (1)

Изобретение относится к области авиационной техники и может быть использовано при создании самолетов с выдвижными закрылками. С целью снижения веса и упрощения конструкции обтекателя механизма уборки и выпуска закрылков, хвостовая часть обтекателя имеет торцевой срез от задней кромки закрылка под углом ±45° к плоскости, перпендикулярной хорде крыла, с переходом в плавный обвод схода при высотах, больших его ширины.The invention relates to the field of aviation technology and can be used to create aircraft with retractable flaps. In order to reduce weight and simplify the design of the fairing mechanism for flaps cleaning and release, the tail section of the fairing has an end cut from the trailing edge of the flap at an angle of ± 45 ° to the plane perpendicular to the wing chord, with a transition to a smooth contour of the descent at heights greater than its width.
RU9595106048A 1995-04-18 1995-04-18 Fairing of extension and retraction mechanism for extension flaps RU2085441C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU9595106048A RU2085441C1 (en) 1995-04-18 1995-04-18 Fairing of extension and retraction mechanism for extension flaps

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU9595106048A RU2085441C1 (en) 1995-04-18 1995-04-18 Fairing of extension and retraction mechanism for extension flaps

Publications (2)

Publication Number Publication Date
RU95106048A true RU95106048A (en) 1996-12-20
RU2085441C1 RU2085441C1 (en) 1997-07-27

Family

ID=20166879

Family Applications (1)

Application Number Title Priority Date Filing Date
RU9595106048A RU2085441C1 (en) 1995-04-18 1995-04-18 Fairing of extension and retraction mechanism for extension flaps

Country Status (1)

Country Link
RU (1) RU2085441C1 (en)

Also Published As

Publication number Publication date
RU2085441C1 (en) 1997-07-27

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Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20100419