wing lengthとは 意味・読み方・使い方

To reduce the manhour for piping and the cost by disposing a hydraulic device for driving a wing in a position for decreasing the length of an oil pressure hose.例文帳に追加

油圧ホースの長さを短くできる位置にウイング駆動用の油圧装置を配設して配管工数の削減とコストダウンを図ること。 - 特許庁

A sewing needle 31 with protrusion ridges which has the wing-shaped protruded ridges protruded in the needle diameter direction and extended in the needle length direction is attached to a sewing machine.例文帳に追加

まず、針径方向に突出し針長方向に延びる翼状突条が形成された突条付縫針３１をミシンに取り付ける。 - 特許庁

The wing member terminates at an engagement edge, and is constituted to be interengaged with the structure at a position along length of the engagement edge.例文帳に追加

ウィング部材は、係合縁部で終端し、該係合縁部の長さに沿った位置で構造体に相互係合するように構成される。 - 特許庁

The turbine aerofoil 10 includes at least one wing spar structure 11 having a shorter length than the length of a related turbine aerofoil.例文帳に追加

タービンエーロフォイル（１０）は関連するタービンエーロフォイルの長さよりも短い長さ（９２）を有する少なくとも１つの翼桁構造（１１）を含む。 - 特許庁

The stretching/contraction mechanism is formed as a fixed wing structure so that it is not turned by the joint by enhancing pendulum stability by being elongated to the longest length at the low-speed flight including taking-off and landing, and reducing air resistance by being contracted to the shortest length at a high-speed flight.例文帳に追加

前記伸縮機構は、離着陸を含む低速飛行時に最も長くして振子安定性を向上し、高速飛行時に最も短くして空気抵抗を減少し、前記関節で回動しない固定翼構造とする。 - 特許庁

The first anchor body includes a central portion 12 that is adapted to receive a suture, and opposite wing members 14 extending from opposed sides of the central portion, the wing members defining a length that is greater than a height of the central portion.例文帳に追加

第１のアンカー本体は、縫合糸を受容するように適合された中心部分１２、およびその中心部分の両側から延出した相反するウイング部材１４を備え、ウイング部材は中心部分の高さよりも大きい長さを持つ。 - 特許庁

Since a connection part between the leading edge structure 11 and the wing center structure 12 is disposed at a position near 20% of the chord length C, an increase in drag due to a clearance or a step at the connection part between the leading edge structure 11 and the wing center structure 12 can be minimized.例文帳に追加

前縁構造体１１と翼中央構造体１２との結合部を翼弦長Ｃの２０％の位置に配置することにより、前縁構造体１１と翼中央構造体１２との結合部の隙間や段差による抗力の増加を最小限に抑えることができる。 - 特許庁

In such a stator core 1, split-core plates 2a adjoining each other in a stacking direction are integrated in the position of L/5 or its vicinity from the end 5b of the wing part 5 when defined that the length of a wing-shaped part 5 jutted out circumferentially from the tooth 4 of the yoke 3 of the split core 2 is L.例文帳に追加

このようなステータ１において、分割コア２のヨーク部３の、ティース４から周方向に張り出した翼状部５の長さをＬとすると、翼状部５の端部５ｂからＬ／５近傍の位置で、積層方向に隣り合う分割コアプレート２ａを一体化する。 - 特許庁