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RU2001120662A - Flap extension device - Google Patents

Flap extension device

Info

Publication number
RU2001120662A
RU2001120662A RU2001120662/28A RU2001120662A RU2001120662A RU 2001120662 A RU2001120662 A RU 2001120662A RU 2001120662/28 A RU2001120662/28 A RU 2001120662/28A RU 2001120662 A RU2001120662 A RU 2001120662A RU 2001120662 A RU2001120662 A RU 2001120662A
Authority
RU
Russia
Prior art keywords
link
extension device
flap
flap extension
drive lever
Prior art date
Application number
RU2001120662/28A
Other languages
Russian (ru)
Other versions
RU2214347C2 (en
Inventor
Александр Иванович Шелудько
Петр Николаевич Васильченко
Original Assignee
Открытое акционерное общество Таганрогский авиационный научно-технический комплекс им. Г.М. Бериева
Filing date
Publication date
Application filed by Открытое акционерное общество Таганрогский авиационный научно-технический комплекс им. Г.М. Бериева filed Critical Открытое акционерное общество Таганрогский авиационный научно-технический комплекс им. Г.М. Бериева
Priority to RU2001120662A priority Critical patent/RU2214347C2/en
Priority claimed from RU2001120662A external-priority patent/RU2214347C2/en
Publication of RU2001120662A publication Critical patent/RU2001120662A/en
Application granted granted Critical
Publication of RU2214347C2 publication Critical patent/RU2214347C2/en

Links

Claims (1)

Устройство для выдвижения закрылка, содержащее балку, неподвижно закрепленную на крыле, рычаг привода, несущий рычаг, шатун, два звена навески закрылка и тягу синхронизации, отличающееся тем, что звенья навески закрылка шарнирно соединены с несущим рычагом, при этом переднее звено навески соединено тягой синхронизации с рычагом привода.A flap extension device comprising a beam fixedly mounted on the wing, a drive lever, a supporting lever, a connecting rod, two flap linkages and a synchronization link, characterized in that the flap link links are pivotally connected to the link arm, while the front link link is connected by a synchronization link with drive lever.
RU2001120662A 2001-07-23 2001-07-23 Flap extending unit RU2214347C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2001120662A RU2214347C2 (en) 2001-07-23 2001-07-23 Flap extending unit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2001120662A RU2214347C2 (en) 2001-07-23 2001-07-23 Flap extending unit

Publications (2)

Publication Number Publication Date
RU2001120662A true RU2001120662A (en) 2003-06-27
RU2214347C2 RU2214347C2 (en) 2003-10-20

Family

ID=31988281

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2001120662A RU2214347C2 (en) 2001-07-23 2001-07-23 Flap extending unit

Country Status (1)

Country Link
RU (1) RU2214347C2 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005045759A1 (en) 2005-09-23 2007-04-12 Airbus Deutschland Gmbh Progressive aerofoil trailing edge for aircraft has flap, which can be adjusted both downward and upward by positive and by negative flap deflections respectively whereby aerofoil profile is closed on top side by sealing flap
CA2632619C (en) * 2005-12-29 2010-07-13 Airbus Deutschland Gmbh Airfoil for an aircraft and aircraft
DE102006036464B4 (en) * 2006-08-04 2009-08-20 Airbus Deutschland Gmbh High-lift system for an aircraft
DE102009039967A1 (en) * 2009-09-03 2011-03-10 Airbus Operations Gmbh Adjustment mechanism for the kinematic guidance of an adjusting body when it is adjusted to a supporting structural part, adjusting mechanism for kinematic adjustment of a high-lift body and high-lift system with such adjustment mechanism
RU2583239C1 (en) * 2015-03-10 2016-05-10 Общество с ограниченной ответственностью "Научно Инженерная Компания" Flap extension device

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4172575A (en) * 1975-03-24 1979-10-30 Boeing Commercial Airplane Company Airfoil flap conical extension mechanism

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