Logáil isteach chun an mhír seo a fheiceáil i dteangacha eile
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…
Cruthaitheoir
- Europeana
Cineál míre
- image
Cruthaitheoir
- Europeana
Cineál míre
- image
Institiúidí soláthartha
Comhbhailitheoir
Ráiteas um Chearta Ceadúnas do na meáin sa mhír seo (mura sonraítear a mhalairt)
- http://creativecommons.org/licenses/by-nc-nd/3.0/
- http://creativecommons.org/licenses/by-nc-nd/3.0/
Cearta
- http://www.dmg-lib.org/dmglib/main/portal.jsp?mainNaviState=site.oairights
Aitheantóir
- dmg:26958023
- http://www.dmg-lib.org/dmglib/handler?image=26958023
Caidrimh
- Ilmenau University of Technology, Germany
Tír sholáthair
- Europe
Ainm bailiúcháin
Ar fáil den chéad uair ar Europeana
- 2013-11-25T17:57:15.665Z
An uair dheireanach a nuashonraíodh ón institiúid sholáthartha
- 2013-11-25T17:57:15.665Z