Turbine bypass working fluid admission
AssigneeUnited Technologies Corporation
InventorsChristopher McAuliffe, John F. Maher, Jr.
Life of this patent
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AssigneeUnited Technologies Corporation
InventorsChristopher McAuliffe, John F. Maher, Jr.
Estimating the term…
An air cycle machine (10) has a first stage turbine (60) mounted to a central portion of a common shaft (12), a compressor (50) mounted to the central portion of the shaft (12), a second stage turbine (30) mounted to a first end of the shaft (12), and a fan (40) mounted to a second end of the shaft (12), all for rotation therewith about a longitudinal axis (14). The first and second stage turbines (60, 30) are operative to extract energy from a flow of compressed air for driving the shaft (12), and the fan (40) and the compressor (50), in rotation about the axis (14). A bypass air discharge nozzle (20) is disposed coaxially with the turbine shroud (32) of the outboard turbine (30) at the outlet (134) thereof or downstream thereof at the discharge end (38) of the turbine diffuser (36) so as to receive in a central region the turbine exhaust (3 ) discharging from the turbine (30) and to define an annular flow inlet (28) through which a flow of bypass air (5) is directed into an outer circumferential region thereof to flow substantially parallel to and about the cooled expanded conditioning air exhaust flow (3) discharged from the turbine (30).
A turbomachine having at least a compressor wheel and a turbine wheel mounted to a common shaft for rotation therewith, said turbine wheel being operative to extract energy from a flow of compressed working fluid for driving the shaft in rotation about a longitudinally extending axis, said turbine wheel mounted to an end portion of the shaft and having a fixed stator and an outlet for directing an exhaust flow discharging from said turbine wheel along said axis, said turbomachine characterized by a bypass flow nozzle disposed coaxially about said longitudinal axis and extending coaxially along said axis, said bypass flow nozzle having a nozzle inlet including a central region for receiving the turbine exhaust flow passing from said turbine wheel outlet and an outer annular region extending circumferentially about said central region for receiving a flow of working fluid having bypassed said turbine wheel, whereby said received turbine bypass flow passes through said outer annular region as an outer annular flow stream passing substantially parallel to and about the turbine exhaust flow passing through said central region, and a nozzle outlet for directing the received turbine exhaust flow and the received turbine bypass flow therethrough.
An air cycle machine for conditioning air for supply to an enclosure, comprising:
Dependencies are inferred from the claim text.