弾性翼の英語

この部材４２は、全体が矩形状で、中央に「コ」字状の切込み４３をもつ取付部を設け、その両翼４４を折り曲げてトラフ状に形成したもので、両翼４４は曲げ弾性を有し、弾性的に変位自在である。例文帳に追加

The member 42 has a rectangular shape as a whole, and is fitted with a mounting part having in the center a cut 43 in a channel shape, and the two wings 44 are folded so as to assume a trough shape, wherein the wings 44 have flexural elasticity and are displaceable elastically. - 特許庁

１０‥ゴムクローラ、１１‥ゴム弾性体、１２‥ゴムラグ、１３‥芯金、１４‥翼部、１５‥メインコード、１６‥角部、Ａ１、Ａ２、Ａ３‥翼部とメインコードに挟まれた部位のゴム材の硬度、Ｂ‥ゴムクローラの基体をなすゴム弾性体の硬度。例文帳に追加

A rubber material with low hardness (hardness A1) is arranged on the center side between the main cords 15 and the wing sections 14 of the mandrels 13, and a rubber material with high hardness (hardness A2) is arranged on the tip side of the wing sections 14. - 特許庁

これにより、弾性接触部２８と翼部材１７、１８の内面２１、２２との弾性接触面積が広くなって、静翼に生じる自励振動を確実に抑制することができる。例文帳に追加

Thus, the elastically contacting area between the elastic contact portion 28 and the inner surfaces 21 and 22 of the blade members 17 and 18 is expanded, and the self-excited vibration generated in the stator blade can be surely restrained. - 特許庁

軸方向に異方性を有する複数のＣＦＲＰロッド１を翼の翼幅方向に対し平行になるように配設してＣＦＲＰロッド１の隙間に弾性部材２を充填しながら翼を成形する。例文帳に追加

A wing is formed by arranging a plurality of CFRP rods 1 having anisotropy in the axial direction so as to be parallel to the width direction of the wing, and filling an elastic member 2 in spaces between the CFRP rods 1. - 特許庁

１‥芯金、２、３‥翼部、４‥ゴム弾性体、５‥スチールコード、６、７‥翼部の先端、８‥翼部の先端の外周面、９、１０‥肉盛部、１４‥ゴムラグ、１５、１６‥ゴムラグの両端。例文帳に追加

Width ends of the core metal are continuously curved toward the inner circumference to curve the outer circumferential surface at the width ends of the core metal. - 特許庁

弾性部材２１は、水平翼本体２０が所定形状に成形されたのち、水平翼本体２０の開口端２０ａから水平翼本体２０の内部に挿入される。例文帳に追加

The elastic member 21 is inserted into the inside of the horizontal wing body 20 from an opening end 20a of the horizontal wing body 20 after the horizontal wing body 20 is molded in a predetermined shape. - 特許庁

翼布３の後縁３ｂは、回転主軸１の回転逆方向側に隣接して位置した翼支持棒１との間が、弾性引張線部材７で連結され、翼布３の後縁３ｂを引張状に結合している。例文帳に追加

In the rear edge 3b of the blade cloth 3, a space with the blade support bar 1 positioned adjacent to the side in the rotation inverse direction of the rotary main shaft 1, is connected by means of an elastic tension wire member 7, and the rear edge 3b of the blade cloth 3 is joined in a tensile manner. - 特許庁

剛性可変フィンおよび、剛性可変フィンを備えた高粘性流体内推進機構、弾性翼流体内推進機構例文帳に追加

RIGIDITY VARIABLE FIN, PROPULSION MECHANISM IN HIGHLY VISCOUS FLUID EQUIPPED WITH RIGIDITY VARIABLE FIN, AND ELASTIC VANE IN-FLUID PROPULSION MECHANISM - 特許庁