JPS6290899U - - Google Patents

Info

Publication number
JPS6290899U
JPS6290899U JP18380085U JP18380085U JPS6290899U JP S6290899 U JPS6290899 U JP S6290899U JP 18380085 U JP18380085 U JP 18380085U JP 18380085 U JP18380085 U JP 18380085U JP S6290899 U JPS6290899 U JP S6290899U
Authority
JP
Japan
Prior art keywords
stiffening plate
supporting
flange portion
support
plate structure
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
JP18380085U
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 JP18380085U priority Critical patent/JPS6290899U/ja
Publication of JPS6290899U publication Critical patent/JPS6290899U/ja
Pending legal-status Critical Current

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Landscapes

  • Reinforcement Elements For Buildings (AREA)

Description

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

第1図はこの考案に係る面圧支持用防撓板構造
の基本的な一実施例による概要を示す断面図、第
2図a,bおよび第3図a,bは同上各別の実施
例態様を示すそれぞれ断面図であり、また第4図
は代表的な防撓板構造における面圧荷重状態図、
第5図は同上荷重状態における曲げモーメント図
、第6図および第7図は従来の各別例による面圧
支持用防撓板構造を示すそれぞれ断面図である。 1……防撓板、2……支持部材、2a……支持
部材のウエブ部、2b,2b……支持部材の左右
フランジ部。
Fig. 1 is a sectional view showing an outline of one basic embodiment of the stiffening plate structure for supporting surface pressure according to this invention, and Figs. 2 a, b and 3 a, b are different embodiments of the same. FIG. 4 is a diagram showing the state of surface pressure load in a typical stiffening plate structure.
FIG. 5 is a bending moment diagram in a loaded state, and FIGS. 6 and 7 are cross-sectional views showing different examples of conventional stiffening plate structures for supporting surface pressure. DESCRIPTION OF SYMBOLS 1... Stiffening plate, 2... Supporting member, 2a... Web portion of the supporting member, 2b, 2b... Left and right flange portions of the supporting member.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 面圧荷重が負荷される防撓板と、この防撓板を
所定方向、間隔毎に支持する複数の支持部材とに
よつて構成する面圧支持用防撓板構造において、
前記防撓板面に当接させる各支持部材に、それぞ
れ支持方向に沿う所定幅のフランジ部を設け、同
防撓板面にこれらの各フランジ部面を結合固定さ
せたことを特徴とする面圧支持用防撓板構造。
In a stiffening plate structure for supporting surface pressure, which is constituted by a stiffening plate to which a surface pressure load is applied, and a plurality of support members supporting the stiffening plate in a predetermined direction and at intervals,
A surface characterized in that each support member that is brought into contact with the stiffening plate surface is provided with a flange portion having a predetermined width along the supporting direction, and each of these flange portion surfaces is coupled and fixed to the stiffening plate surface. Stiffening plate structure for pressure support.
JP18380085U 1985-11-29 1985-11-29 Pending JPS6290899U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18380085U JPS6290899U (en) 1985-11-29 1985-11-29

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18380085U JPS6290899U (en) 1985-11-29 1985-11-29

Publications (1)

Publication Number Publication Date
JPS6290899U true JPS6290899U (en) 1987-06-10

Family

ID=31130869

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18380085U Pending JPS6290899U (en) 1985-11-29 1985-11-29

Country Status (1)

Country Link
JP (1) JPS6290899U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002053098A (en) * 2000-06-28 2002-02-19 Eads Airbus Gmbh Structural member for airplane, manufacturing method thereof and reinforcement deformed member for the structural member

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002053098A (en) * 2000-06-28 2002-02-19 Eads Airbus Gmbh Structural member for airplane, manufacturing method thereof and reinforcement deformed member for the structural member

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