aileron

美 [?e?l?rɑn] 　英 [?e?l?r?n]

• n.（飛機(jī)的）副翼
• 網(wǎng)絡(luò)飛機(jī)的副翼；輔助翼；襟翼

詞形變化

復(fù)數(shù)：ailerons  

英漢雙解

英漢解釋

n.	1. 【航】副翼,輔(助)翼

英英解釋

n.	1. a part on the back edge of an aircraft’s wing that is used in making one side of the aircraft move higher than the other

例句

After depends on the reason verticalmast also to be allowed to be hanging the flap and the aileron.

靠后緣的縱檣還可以懸掛襟翼和副翼。

The main elevator control system, including control systems, rudder and aileron control system to manipulate the system.

主操縱系統(tǒng)包括升降舵操縱系統(tǒng)、副翼操縱系統(tǒng)和方向舵操縱系統(tǒng)。

Two circular vents highlight the side of the car with a duck tail spoiler topping the C8 Aileron's aggressive rear-end.

兩個(gè)圓形通風(fēng)口強(qiáng)調(diào)一方的汽車(chē)與ducktail擾流突破將其命名為C8副翼的侵略尾部。

AILERON, A hinged moveable part on the trailing edge of each wing for airplane roll (wing up and wing down) control.

副翼，鉸連在每個(gè)機(jī)翼后緣的可動(dòng)部件，用于控制飛機(jī)的滾轉(zhuǎn)（機(jī)翼向上和向下）。

The aileron control system provides the means of rotating the airplane about the longitudinal axis .

副翼控制系統(tǒng)提供飛機(jī)縱向轉(zhuǎn)動(dòng)的方式。

AILERON FORCE LIMITER, An electro-mechanical device for limiting the control wheel movement by the autopilot during autopilot operation.

副翼操縱力限制器，一種機(jī)電裝置。在自動(dòng)駕駛工作期間，用來(lái)限制駕駛盤(pán)的動(dòng)作量。

The outboard hinged part of the wing is called the aileron: it is used to roll the wings from side to side.

在舷外鉸鏈的機(jī)翼部分稱(chēng)為副翼：它是用來(lái)從一邊滾展翅一邊。

Aileron, which holds patent rights from Harvard and the Dana-Farber Cancer Institute, hopes to start clinical trials next year.

副翼醫(yī)療公司擁有來(lái)自哈佛大學(xué)和達(dá)納法伯癌癥研究所（Dana-FarberCancerInstitute）的該技術(shù)的專(zhuān)利權(quán)，并且他們希望明年能夠進(jìn)行相應(yīng)的臨床試驗(yàn)。

Aileron rolls are flown with the rudder and elevator in the neutral position during the roll.

副翼橫滾在橫滾期間使用方向舵操縱，升降舵位于初始平衡位置，不參與操縱。

Further, the reconfigurable control law is designed undergoing the elevator and aileron failures.

并研究了升降舵、副翼發(fā)生失效和卡死時(shí)的控制律重構(gòu)方法。

The aileron is fully deflected in the direction of the roll. This is the easiest of the rolls to fly.

兩個(gè)副翼在相反方向上完全放開(kāi)，這時(shí)最容易的一種滾轉(zhuǎn)。

Sales of the Spyker C8 Aileron are expected to kick off this summer, although no pricing has been released.

銷(xiāo)售的世爵C8副翼預(yù)計(jì)今年夏天開(kāi)始，雖然沒(méi)有定價(jià)已被釋放。

The design of the aero servo aileron hinges are machined from solid billet and have a self aligning ball bearing pressed into the arm.

氣動(dòng)伺服副翼由整體坯料加工而成，設(shè)計(jì)在轉(zhuǎn)臂上有自動(dòng)對(duì)準(zhǔn)滾珠軸承。

Design-wise, the C8 Aileron is pure Spyker, combining an almost industrial look with sport and class.

設(shè)計(jì)角度看，將其命名為C8副翼是純粹的世爵，結(jié)合工業(yè)外觀幾乎與運(yùn)動(dòng)和階級(jí)。

Dr. Garaud said Roche's chief executive has approved the deal with Aileron.

Garaud博士稱(chēng)羅氏的首席執(zhí)行官已經(jīng)批準(zhǔn)了同副翼醫(yī)療公司的交易。

Pullup, Backflip, And Aileron Roll.

拉起，斤斗，副翼滾轉(zhuǎn)。

Shake the control wheel to center the aileron system.

搖動(dòng)控制輪使得副翼系統(tǒng)居中。

Aileron, founded in 2005, has about 40 employees.

創(chuàng)立于2005年的副翼醫(yī)療公司只有40名員工。

Semi-active flutter suppression for wing aileron system using stepped MR damper--numeric simulation and tunnel experiments

基于多級(jí)磁流變阻尼器的操縱面振動(dòng)半主動(dòng)抑制--數(shù)值仿真與風(fēng)洞試驗(yàn)

The numerical calculation research of two dimensional aileron by solving N-S equation

二維舵面繞流的N-S方程數(shù)值計(jì)算研究

Semi-active flutter suppression for wing aileron system using stepped MR damper--design and modeling of MR damper

基于多級(jí)磁流變阻尼器的操縱面振動(dòng)半主動(dòng)抑制--阻尼器設(shè)計(jì)與試驗(yàn)建模

Simulation of Static Test of Composite Aileron and Consistent Evaluation of Test and Analysis Results

復(fù)合材料副翼試驗(yàn)仿真及試驗(yàn)與分析一致性評(píng)估

The feasibility analysis of aileron manpower control in a fighter

某型殲擊機(jī)副翼人力操縱可行性分析

Check elevator, aileron, and rudder controls for full travel and smooth operation

檢查起落架，副翼，方向舵以保證飛行完整且操作順暢；

Leak detection in reaction control system that controls movement of aileron and tail fin

飛機(jī)副翼和尾翼密封性檢測(cè)

Semi-Active Flutter Suppression for Wing Aileron with Framework System

帶有傳動(dòng)機(jī)構(gòu)的翼段顫振半主動(dòng)抑制

Leading-edge of Aileron with Variable Attached Weights of Flutter Analysis

前緣變配重顫振分析

FMEA The FMEA for aileron control system of a new type light aircraft

某新研輕型飛機(jī)副翼操縱系統(tǒng)

in mode 2 , the right control stick operates the aileron and elevator and the left stick operates the rudder and throttle

在模式2中，右邊的操縱桿控制副翼和升降舵，左邊的操縱桿控制方向舵和油門(mén)。

SYSTEM A AILERON POWER CONTROL UNIT;

使用A系統(tǒng)壓力的副翼動(dòng)力控制組件；

Left Arrow Aileron Trim Right

副翼右配平