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Patent drawing for Three spool gas turbine engine having a clutch and compressor bypass
US 8,887,485 B2
Mechanical US 8,887,485 B2 Not in force

Three spool gas turbine engine having a clutch and compressor bypass

This is a complex gas turbine engine designed for adaptability. It features three main rotating shafts and a fan with two stages that can spin in opposite directions, where one stage can be selectively engaged or disengaged with a clutch. The engine also includes a system to bypass air around its highest-pressure compressor.

Why it matters: The demand for highly fuel-efficient and multi-mission capable aircraft engines has intensified significantly since 2009. Advances in high-temperature materials and sophisticated engine control systems could now make the complex adaptive features, like the clutched counter-rotating fan and compressor bypasses, more practical and reliable to implement.

Status
Not in forceListed as no longer active. The specific reason is not in the record we hold.
How hard to build
SpecializedHigh-temperature alloys, precision machining, complex controls.

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