Method for preventing an over temperature condition in a gas turbine engine
AssigneeGeneral Eletric Company
InventorDaniel Drew Smith
Life of this patent
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Abstract
Method comprising providing a signal tube extending generally from an engine component disposed on a hot side of a firewall in a gas turbine engine to at least one engine control mechanism disposed on a cool side of the firewall. A fuse in the signal tube is operable responsive to a breach in the signal tube to change from a first condition to a second condition to prevent an over-temperature situation on the cool side of the firewall. The engine control mechanism operates the engine according to a first operating logic utilizing a pressure signal related to a static pressure of a fluid in the signal tube. Loss of the pressure signal causes the engine control mechanism to change to a second operating logic which does not utilize the pressure signal.
Claims11
A method comprising:
- providing a signal tube extending generally from an engine component disposed on a hot side of a firewall in a gas turbine engine to at least one engine control mechanism disposed on a cool side of the firewall, wherein a first portion of the signal tube is generally disposed on the hot side and a second portion of the signal tube is generally disposed on the cool side;
- and
- providing a fuse in the first portion of a signal tube, wherein the signal tube includes a flow path therethrough at least partly defined by a pathway through the fuse.
A method comprising:
- providing at least one engine control mechanism disposed on a cool side of a firewall in a gas turbine engine, wherein the engine control mechanism is operative to selectively control the gas turbine engine according to a first operating logic or a second operating logic, wherein the first operating logic utilizes a pressure signal, and wherein the second operating logic does not utilize the pressure signal;
- providing a signal tube extending generally from an engine component disposed on a hot side of the firewall in a gas turbine engine to the at least one engine control mechanism, wherein a first portion of the signal tube is generally disposed on the hot side and a second portion of the signal tube is generally disposed on the cool side;
- and
- providing a fuse in a first portion of a signal tube, wherein the signal tube includes a flow path therethrough at least partly defined by a pathway through the fuse, wherein when the fuse is in a first condition, the pathway is substantially unobstructed such that the signal tube is operable to provide the pressure signal related to a static pressure of a fluid in the signal tube to the at least one engine control mechanism, and wherein when the fuse is in a second condition, the pathway is substantially obstructed so that the signal tube does not provide the pressure signal to the at least one engine control mechanism.
Dependencies are inferred from the claim text.