Turbomachine nozzle having fluid conduit and related turbomachine

A turbomachine diaphragm comprising:

• an inner diaphragm ring;
• an outer diaphragm ring radially outward of the inner diaphragm ring;
• and
• a set of static nozzles spanning between the inner diaphragm ring and the outer diaphragm ring, wherein at least one static nozzle in the set of static nozzles includes:
• a body having:
• a first sidewall and a second sidewall opposite the first sidewall;
• a pressure side and a suction side each extending between the first sidewall and the second sidewall;
• and
• a leading edge section at a first junction of the pressure side and the suction side, and a trailing edge section at a second junction of the pressure side and the suction side;
• and
• a bypass fluid conduit including:
• a channel having an opening to at least one of the first sidewall or the second sidewall;
• and
• an outlet passageway fluidly connected with the channel between the first sidewall and the second sidewall, the outlet passageway including a first opening on at least one of the pressure side of the body, the suction side of the body or the trailing edge section.

A turbomachine comprising:

• a rotor section;
• and
• a stator section substantially housing the rotor section, the stator section including:
• a packing section;
• and
• a set of static nozzles spanning between an inner diaphragm ring and an outer diaphragm ring, wherein at least one static nozzle in the set of static nozzles includes:
• a body having:
• a first sidewall and a second sidewall opposite the first sidewall;
• and
• a pressure side and a suction side each extending between the first sidewall and the second sidewall;
• and
• a bypass fluid conduit including:
• a channel having an opening to at least one of the first sidewall or the second sidewall proximate the packing section;
• and
• an outlet passageway fluidly connected with the channel between the first sidewall and the second sidewall, the outlet passageway including a first opening on the pressure side of the body,
• wherein the bypass fluid conduit is configured to divert a fluid from the packing section to the first opening on the pressure side of the body during operation of the turbomachine.