首页> 外国专利> SINGLE USE AND TECHNOLOGY OF AIRCRAFT ELSAVELET (OPTIONS) BLOCK fragment WINGS TURBOROTORNY ENGINE (VARIANTS), BESSTATORNY COMPRESSOR, FAN SHELL, a way to create lift SAVELETA AND METHOD FOR OPERATING THE ENGINE TURBOROTORNOGO

SINGLE USE AND TECHNOLOGY OF AIRCRAFT ELSAVELET (OPTIONS) BLOCK fragment WINGS TURBOROTORNY ENGINE (VARIANTS), BESSTATORNY COMPRESSOR, FAN SHELL, a way to create lift SAVELETA AND METHOD FOR OPERATING THE ENGINE TURBOROTORNOGO

机译:飞机小翼(选装)机翼碎片翼形涡轮发动机(变型),贝斯特里尼压缩机,风扇壳的单一使用和技术,创建升程小翼的方法和操作发动机涡轮翼形的方法

摘要

1. require an airfield elsavelet comprising a fuselage 1 with a cockpit and passenger cabin or cargo compartment, with propulsion thrust reversers on the pylons 3 in front of the fuselage, propfan 4 and located in the air stream of the bearing surfaces, the installation of air-launch and control system, fuel , conditioning and bogie chassis with wheels on low pressure tires, characterized in that mounted on the front side pylons 3 turborotornye motors 2 are as generating sets of first and second screws, connected to an electric circuit with electric motors 12, 13, respectively first 23 and second 28 propfan 11 screw mounted on the front upper pylon 10, and blocks fragment wings 8 are mounted on the fuselage and 9 on the side of the front 3 and rear 6 pylons, the blocks 15 on the forks ends upper front and rear pylon 10 by means of longitudinal beams 5 or on brackets 16 each turborotorny engine 2 is configured besstatornym compressor 21, each shroud 4 has a profiled inner propfans poverhnos s and is provided with upper and lower block bearing sectors 20, wherein turborotornye engines made by chetyrehvalnoy circuit with turbine stages of counter-rotating, wherein the rear end of the fuselage and in the rear pylon 6 by means of brackets pivotally mounted handlebars course 17 and the pitch 18 to sequentially or simultaneous deflection of each wheel in its side. ! 2. elsavelet require an airfield according to claim 1, characterized in that mounted on the front side pylons 3 turborotornye motors 2 and n have the coupling sleeve
机译:1.要求机场的机翼小翼包括一个带有驾驶舱和乘客舱或货舱的机身1,在机身前面的吊架3上带有推进推力反向器,螺旋桨4并位于轴承表面的气流中,空气发射和控制系统,带低压轮胎的车轮的燃料,调节和转向架底盘,其特征在于,安装在前侧挂架3上的turborotornye电动机2作为第一组螺钉和第二组螺钉的发电机组,并通过电路连接到电路电动机12、13,分别将第一螺旋桨11和第二螺旋桨11安装在前上挂架10上,将块状翼片8安装在机身上,并在前3和后6挂架的侧面上安装9,将块15放在叉通过纵向梁5或在支架16的上端在前挂架10和后挂架10的两端,每个涡轮旋流式发动机2均配置有贝斯斯塔托尼压缩机21,每个护罩4均具有异型内螺旋桨hnos s并设有上,下块轴承扇区20,其中chetyrehvalnoy电路制造的涡轮旋转发动机带有反向旋转的涡轮级,其中,机身后端和后挂架6通过支架可枢转地安装在车把上在图17和俯仰18中,每个车轮在其侧面顺序地或同时地偏转。 ! 2.根据权利要求1所述的机场小飞机,其特征在于,安装在前侧挂架3上的涡轮旋转马达2和n具有连接套。

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