-
1 inlet
nAUTO admisión f, entrada fHYDRAUL canalización fHYDROL boca de entrada f, bocatoma f (AmL), ensenada fMECH boca de entrada f, entrada f, orificio de entrada m, tubo de entrada mMECH ENG entrada f, orificio de admisión m, orificio de entrada m, oído m, tragante mMINE caleta f, entrada f, orificio de entrada mOCEAN caleta fTELECOM entrada fWATER admisión f, entrada f, toma f, bocatoma fWATER TRANSP geography angostura f, ancón m -
2 nozzle
nAIR TRANSP tobera fAUTO, C&G boquilla fCHEM TECH tobera fCOAL boquilla f, buza f, inyector m, tobera fCONST, FUELLESS boquilla fGAS boquilla f, inyector mHYDRAUL tobera fLAB type of fixing of rail to rail boquilla fMECH tobera f, boquilla fMECH ENG pitón m, boca f, boquilla f, inyector m, lanza f, nariz f, boquerel m, tobera fP&R pico mPHYS tobera fPROD of branch pipe lanza f, of impulse turbine, diesel tobera f, boca f, of bellow, injector, oxyacetylene blowpipe boquilla f, lanza de agua f, inyector mSPACE boquilla f, orificio m, tobera f, inyector m, embocadura f
См. также в других словарях:
Characteristic velocity — or c * is a measure of the combustion performance of a rocket engine independent of nozzle performance, and is used to compare different propellants and propulsion systems. Formula c * is the characteristic velocity (meters/second) p1 is the… … Wikipedia
Jet engine performance — This article describes how jet engine performance is estimated during the design phase. Similar techniques are used once the engine has been built and is being tested, except the performance of individual components, rather than being assumed, is … Wikipedia
скорость среды на выходе из горловины горелки топки котла — — [А.С.Гольдберг. Англо русский энергетический словарь. 2006 г.] Тематики энергетика в целом EN boiler burner throat velocity … Справочник технического переводчика
Components of jet engines — Diagram of a typical gas turbine jet engine. Air is compressed by the fan blades as it enters the engine, and it is mixed and burned with fuel in the combustion section. The hot exhaust gases provide forward thrust and turn the turbines which… … Wikipedia
Venturi scrubber — A venturi scrubber is designed to effectively use the energy from the inlet gas stream to atomize the liquid being used to scrub the gas stream. This type of technology is a part of the group of air pollution controls collectively referred to as… … Wikipedia
Rocket engine — RS 68 being tested at NASA s Stennis Space Center. The nearly transparent exhaust is due to this engine s exhaust being mostly superheated steam (water vapor from its propellants, hydrogen and oxygen) … Wikipedia
Turbofan — [ CFM56 3 turbofan, lower half, side view.] A turbofan is a type of jet engine, similar to a turbojet. It essentially consists of a ducted fan with a smaller diameter turbojet engine mounted behind it that powers the fan. Part of the airstream… … Wikipedia
de Laval nozzle — Diagram of a de Laval nozzle, showing approximate flow velocity (v), together with the effect on temperature (t) and pressure (p) A de Laval nozzle (or convergent divergent nozzle, CD nozzle or con di nozzle) is a tube that is pinched in the… … Wikipedia
De Laval nozzle — A de Laval nozzle (or convergent divergent nozzle, CD nozzle or con di nozzle) is a tube that is pinched in the middle, making an hourglass shape. It is used as a means of accelerating the flow of a gas passing through it to a supersonic speed.… … Wikipedia
Accurizing — is the process of improving the accuracy of a firearm or airgun.cite web |url=http://saami.org/Glossary/index.cfm |title=SAAMI glossary |accessdate=2007 08 30] For firearms, accuracy is defined as the ability to hit exactly what you re aiming at … Wikipedia
Rocket engine nozzle — A rocket engine nozzle is a propelling nozzle usually of the de Laval type used in a rocket engine to expand and accelerate the combustion gases, from burning propellants, so that the exhaust gases exit the nozzle at hypersonic… … Wikipedia