wing fuselageとは 意味・読み方・使い方

The wing can extend outwardly from the fuselage at least proximate to the second fuselage portion and can include a leading edge region and a trailing edge region.例文帳に追加

翼は、第２の胴体部分に少なくとも隣接した胴体から外側に向かって延び、前縁領域および後縁領域を含み得る。 - 特許庁

The noise reduction device 100 including a leading edge sweep back angle which is larger than a wing 1 and a wing with width of 5-15% of a whole wing semi-span is attached to a tip end of a connection part of the wing 1 and a fuselage 2.例文帳に追加

翼１と胴体２の結合部先端に、前縁後退角が翼１より大きく且つ翼幅が全翼セミ・スパンの５〜１５％である騒音低減デバイス１００を取り付ける。 - 特許庁

The main wing is made of the elastic body, the elastic body and a fuselage of the machine are fixed, weights are imparted to the middle of the wing and wing end, and thereby vertical vibration is facilitated.例文帳に追加

本発明は主翼を弾性体で構成し、この弾性体と機の胴体を固定すると共に、翼の途中や翼端に錘を付けて上下の振動を容易にするものである。 - 特許庁

The propulsion system can include an engine nacelle fixedly attached to the wing and laterally aligned with the second fuselage portion.例文帳に追加

推進システムは、翼に固定して取付けられ、さらには第２の胴体部分と横方向に整合するエンジンナセルを含み得る。 - 特許庁

The unmanned aircraft 200 is provided with an unmanned aircraft main wing 220, an unmanned aircraft fuselage 210, an unmanned landing system 270, and an unmanned aircraft combining mechanism 280 provided at a ceiling 211 of the unmanned aircraft fuselage 210.例文帳に追加

無人機２００は、無人機主翼２２０と、無人機胴体２１０と、無人機降着系統２７０と、無人機胴体２１０の天井部２１１に設けられた無人機結合機構２８０とを備える。 - 特許庁

The manned aircraft 100 is provided with a manned aircraft main wing 120, a manned aircraft fuselage 110, a manned aircraft landing system, and a manned aircraft combining mechanism 180 provided at a bottom 111 of the manned aircraft fuselage 110.例文帳に追加

有人機１００は、有人機主翼１２０と、有人機胴体１１０と、有人機降着系統と、有人機胴体１１０の底部１１１に設けられた有人機結合機構１８０とを備える。 - 特許庁

Additionally, sensors (40/42) are provided in an engine (34) and/or a wing/fuselage structure (32) to provide control signals to the active vibration mechanisms (36) so that the active vibration mechanisms (36) react to the sensed data to minimize vibration transmissibility from the engine (34) into the wing/fuselage (32).例文帳に追加

さらに、センサ（４０／４２）がエンジン（３４）および／または翼／機体構造物（３２）上に設けられて、能動振動機構（３６）に制御信号を供給し、能動振動機構（３６）は、その検知データに対して、エンジン（３４）から翼／機体（３２）への振動伝達率が最小になるように反応する。 - 特許庁

On one plate material, setting is performed so as to segment a main wing, a horizontal tail plane and a tail fin in the form of being continued to a fuselage horizontal part respectively.例文帳に追加

一枚の板材に、主翼、水平尾翼、垂直尾翼がそれぞれ胴体水平部に対して連続する形態で切り出されるように設定する。 - 特許庁