JPS56134660A - Link mechanism - Google Patents

Link mechanism

Info

Publication number
JPS56134660A
JPS56134660A JP3870080A JP3870080A JPS56134660A JP S56134660 A JPS56134660 A JP S56134660A JP 3870080 A JP3870080 A JP 3870080A JP 3870080 A JP3870080 A JP 3870080A JP S56134660 A JPS56134660 A JP S56134660A
Authority
JP
Japan
Prior art keywords
rocking
links
members
link
linkages
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
JP3870080A
Other languages
Japanese (ja)
Other versions
JPH0234838B2 (en
Inventor
Yuzo Nakagami
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
National Aerospace Laboratory of Japan
Subaru Corp
Original Assignee
National Aerospace Laboratory of Japan
Fuji Heavy Industries Ltd
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 National Aerospace Laboratory of Japan, Fuji Heavy Industries Ltd filed Critical National Aerospace Laboratory of Japan
Priority to JP3870080A priority Critical patent/JPH0234838B2/en
Publication of JPS56134660A publication Critical patent/JPS56134660A/en
Publication of JPH0234838B2 publication Critical patent/JPH0234838B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Transmission Devices (AREA)

Abstract

PURPOSE: To easily provide a link mechanism of desired characteristic and facilitate analysis, by combining a plurality of four-joint linkages with rocking members.
CONSTITUTION: The first, the second and the third four-joint linkages are composed of reference links A0-B0, A1-B1, A2-B2, the first rocking links A0-D0, A1-D1, A2-D2, the second links B0-C0, B1-C1, B2-C2 and intermediate links C0-D0, C1-D1, C2-D2, respectively. Since the change (α0) in the angle of the first rocking link A0-D0 of the first linkage and that (β2) in the angle of the second rocking link B2-C2 of the third linkage are correlative to each other, the swing angles of two members can be controlled in a prescribed relation by causing both of the rocking links to support the members. As a result, a desired characteristic can be simply attained when the linkages are applied to the multistage flap actuation mechanism of aircraft, for example.
COPYRIGHT: (C)1981,JPO&Japio
JP3870080A 1980-03-26 1980-03-26 KOKUKINOTADANFURATSUPUKIKO Expired - Lifetime JPH0234838B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3870080A JPH0234838B2 (en) 1980-03-26 1980-03-26 KOKUKINOTADANFURATSUPUKIKO

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3870080A JPH0234838B2 (en) 1980-03-26 1980-03-26 KOKUKINOTADANFURATSUPUKIKO

Publications (2)

Publication Number Publication Date
JPS56134660A true JPS56134660A (en) 1981-10-21
JPH0234838B2 JPH0234838B2 (en) 1990-08-07

Family

ID=12532582

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3870080A Expired - Lifetime JPH0234838B2 (en) 1980-03-26 1980-03-26 KOKUKINOTADANFURATSUPUKIKO

Country Status (1)

Country Link
JP (1) JPH0234838B2 (en)

Also Published As

Publication number Publication date
JPH0234838B2 (en) 1990-08-07

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