Prijava za pregled ovog predmeta na drugim jezicima
AIRCRAFT ENGINE SPEED REGULATOR MECHANISM
Upon an increase in engine speed, weights 1 of the centrifugal governor move outward and, turning about axes O, compress conical spring 2. This raises valve spool 3 and hydraulic fluid from sleeve 4 is discharged through channel 5 to the engine crankcase. As a result, the propeller pitch increases, increasing the power required to drive the propeller and, consequently, reducing the engine speed. A…
Stvorio/la
- Europeana
Vrsta predmet
- image
Stvorio/la
- Europeana
Vrsta predmet
- image
Institucija iz koje dolazi
Agregator
Uvjeti korištenja medija u ovom zapisu (osim ako nije drugačije navedeno)
- http://creativecommons.org/licenses/by-nc-nd/3.0/
- http://creativecommons.org/licenses/by-nc-nd/3.0/
Prava
- http://www.dmg-lib.org/dmglib/main/portal.jsp?mainNaviState=site.oairights
Identifikator
- dmg:26958023
- http://www.dmg-lib.org/dmglib/handler?image=26958023
Odnosi
- Ilmenau University of Technology, Germany
Država iz koje dolazi
- Europe
Naziv zbirke
Prvi put objavljeno na Europeana
- 2013-11-25T17:57:15.665Z
Zadnji put ažurirano od institucije koja pruža podatke
- 2013-11-25T17:57:15.665Z