JPH02147750U - - Google Patents

Info

Publication number
JPH02147750U
JPH02147750U JP5679889U JP5679889U JPH02147750U JP H02147750 U JPH02147750 U JP H02147750U JP 5679889 U JP5679889 U JP 5679889U JP 5679889 U JP5679889 U JP 5679889U JP H02147750 U JPH02147750 U JP H02147750U
Authority
JP
Japan
Prior art keywords
fuselage
steel plates
flange
shaped cross
section
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.)
Pending
Application number
JP5679889U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP5679889U priority Critical patent/JPH02147750U/ja
Publication of JPH02147750U publication Critical patent/JPH02147750U/ja
Pending legal-status Critical Current

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  • Air-Flow Control Members (AREA)

Description

【図面の簡単な説明】[Brief explanation of drawings]

第1図は本考案の一実施例を示す全体斜視図、
第2図は同要部側面図、第3図は第2図B−B線
に於ける断面説明図、第4図は従来例の全体斜視
図である。 図中、A:ダンパー、1:胴体、2:外板、3
:連結部材、4,4’:溝部、5:フランジ。
FIG. 1 is an overall perspective view showing an embodiment of the present invention;
FIG. 2 is a side view of the same essential parts, FIG. 3 is an explanatory cross-sectional view taken along the line BB in FIG. 2, and FIG. 4 is an overall perspective view of the conventional example. In the diagram, A: damper, 1: fuselage, 2: outer plate, 3
: Connecting member, 4, 4': Groove, 5: Flange.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 断面L字状の2枚の鋼板を組み合わせてなる胴
体と、同胴体の両端に外嵌した等辺山形鋼等のフ
ランジ部とからなり、しかも同胴体と同フランジ
部とは、気密状となるべくスポツト溶接されたダ
ンパーにおいて、上記2枚の鋼板が相対して上記
胴体の稜部を形成する部分に、両鋼板を気密状に
嵌合する断面U字状の溝部が、互いに略直角状に
向き合う如く一体的に内側に折曲形成された連結
部材を設けたことを特徴とするダンパーの構造。
It consists of a fuselage made by combining two steel plates with an L-shaped cross section, and a flange made of equilateral angle iron or the like fitted externally to both ends of the fuselage, and the fuselage and the flange are made in a spot as much as possible to be airtight. In the welded damper, a groove portion having a U-shaped cross section that airtightly fits the two steel plates in a portion where the two steel plates face each other to form the ridge of the body is arranged so that they face each other at approximately right angles. A damper structure characterized by providing a connecting member that is integrally bent inside.
JP5679889U 1989-05-16 1989-05-16 Pending JPH02147750U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5679889U JPH02147750U (en) 1989-05-16 1989-05-16

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5679889U JPH02147750U (en) 1989-05-16 1989-05-16

Publications (1)

Publication Number Publication Date
JPH02147750U true JPH02147750U (en) 1990-12-14

Family

ID=31580947

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5679889U Pending JPH02147750U (en) 1989-05-16 1989-05-16

Country Status (1)

Country Link
JP (1) JPH02147750U (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4730769U (en) * 1971-04-26 1972-12-07

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4730769U (en) * 1971-04-26 1972-12-07

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