Aeroplane and Commercial Aviation News, 113. kötet1967 |
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1 - 3 találat összesen 97 találatból.
31. oldal
... engine . None of these subsonic engines possessed turbine cooling or afterburning systems . The two - spool layout allowed each of the separate compressors to operate at its own optimum rpm and best efficiency for a given flight ...
... engine . None of these subsonic engines possessed turbine cooling or afterburning systems . The two - spool layout allowed each of the separate compressors to operate at its own optimum rpm and best efficiency for a given flight ...
34. oldal
... engine proved invaluable as a development tool in proving basic integrity of the system before the full - size engine was manufactured . The high pressure turbine stator blade inner sheath is manufactured with a patter of dimples on the ...
... engine proved invaluable as a development tool in proving basic integrity of the system before the full - size engine was manufactured . The high pressure turbine stator blade inner sheath is manufactured with a patter of dimples on the ...
16. oldal
... engine for normal overhaul cycles . This saves the operator the cost of investing in spares - a significant factor in reducing his total engine ... Engine overhaul - continued use while customers ' engines are 16 JUNE 21 1967 AEROPLANE.
... engine for normal overhaul cycles . This saves the operator the cost of investing in spares - a significant factor in reducing his total engine ... Engine overhaul - continued use while customers ' engines are 16 JUNE 21 1967 AEROPLANE.
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