FIELD: mechanical engineering; aircraft hydraulic systems. SUBSTANCE: variable-capacity pump has spool and piston which are installed in fuel feed regulator structure for direct engagement and are spring loaded relative to pump housing. Invention makes it possible to decrease working pressure, irregularity of feed and pressure fluctuations, as well at heat generation at long operation of pump and hydraulic system. EFFECT: increased service life and reliability of aircraft hydraulic system. 2 dwg
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| AXIAL PISTON PUMP | 2001 |
|
RU2193109C1 |
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|
RU1660423C |
