Valve for diverting fluid flows in turbomachines
AssigneeROLLS-ROYCE plc
InventorsDouglas J. Nightingale, Benjamin D. Ward
Life of this patent
Estimating the term…
Loading patent…
AssigneeROLLS-ROYCE plc
InventorsDouglas J. Nightingale, Benjamin D. Ward
Estimating the term…
A valve for selectively changing the direction of flow of working fluid through a variable cycle engine which comprises a first and second compressor 14,16 spaced along a flow duct 26. The duct 26 having air intakes 42 leading to the second compressor 16 and outlets leading to nozzles 44. The valve comprising a sleeve 30 axially movable along the duct. The sleeve 30 having openings 31 in it in which are located doors 32. Links 36 are connected to each of the doors 32 so that as the sleeve 30 is moved axially the doors 32 are pulled open to open the air inlets 42 and the outlets and simultaneously obturate the flow duct 26. In a second position of the sleeve 30 the doors 32 and the sleeve 30 close off the air inlets and outlets and open the duct to allow the first compressor to supercharge the second compressor.
A fluid flow diverter valve for a gas turbine engine of the type that comprises a fluid flow duct, first and second axial flow compressors spaced along the duct, a combustible means downstream of the compressors, turbine means downstream of the combustion means connected to the compressors to drive the compressors, one or more air outlet openings in the duct wall of a region between the first and second compressors, and an auxilliary air intake in the duct wall spaced along the duct from the one or more outlet openings and located at a region between the one or more outlet openings and the second compressor, the valve comprising:
Dependencies are inferred from the claim text.