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 Member since Sep '08
Working languages: German to English
|  Pavitra Baxi
India Local time: 12:18 IST (GMT+5.5)
Native in: English  | | |
Freelancer,  Verified member | | Translation, Editing/proofreading | | Specializes in: | | Construction / Civil Engineering | SAP | | Mechanics / Mech Engineering | IT (Information Technology) | | Furniture / Household Appliances | Finance (general) | | Engineering: Industrial | Engineering (general) | | Energy / Power Generation | Science (general) |
| Also works in: | | Aerospace / Aviation / Space | Computers (general) | | Tourism & Travel | Photography/Imaging (& Graphic Arts) | | Medical (general) | Management | | Investment / Securities | Insurance | | General / Conversation / Greetings / Letters | Electronics / Elect Eng | | Computers: Software | Computers: Hardware | | Business/Commerce (general) | Manufacturing |
More Less | German to English - Rates: 0.07 - 0.09 USD per word
| | PRO-level points: 23, Questions answered: 18, Questions asked: 13 | 0 projects entered
| Sample translations submitted: 1 | German to English: Technical translation | Source text - German
Der Heckrotor dient dem Ausgleich des vom angetriebenen Hauptrotor verursachten Drehmoments sowie zur Steuerung um die Hochachse. Die eingesetzten Systeme entsprechen im grundsätzlichen Aufbau denen der Hauptrotoren. Um den Aufwand möglichst gering zu halten wird nach Möglichkeit dem halbstarren Zweiblattrotor der Vorzug gegeben. Hierbei ist der Heckrotorkopf mit der Heckrotorwelle über ein zentrales Schlaggelenk verbunden, dessen Achse unter 45° zur Blattsteuerungsachse verläuft. Die 45° Schlagachse bewirkt, daß der Einstellwinkel des Blattes mit zunehmendem Schlagwinkel geringer wird (Blattwinkelrücksteuerung), wodurch die Schlagbewegung bei allen Fluggeschwindigkeiten gering gehalten wird. | Translation - English
The tail rotor compensates for the torque due to the propelled main rotor and the control over the main axis. The basic layout of the system used corresponds to that of the main rotor. In order to keep the costs low, as far as possible preference should be given to the semi-rigid two blade rotor. Here the tail rotor head is connected to the tail rotor shaft over a central flapping hinge, whose axis is at 45° to the blade control axle. The 45° flapping axis causes the rigging angle of the blade becomes smaller with the increasing flapping angle (blade pitch control), whereby the flapping is kept small by all flight speeds. |
More Less | | Years of translation experience: 6. Registered at ProZ.com: May 2008. Became a member: Sep 2008. | | N/A | | N/A | | N/A | | Adobe Acrobat, Microsoft Excel, Microsoft Word, Powerpoint, SDL TRADOS, SDLX | | English (RTF), English (PDF) | | About me Trustworthy technical and financial translator |
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Keywords: Technical, financial, science, physics, mechanical engineering, civil engineering, electronics engineering |
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