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An emergency lubrication system for a turbine engine includes a reservoir 50 containing a reserve quantity of lubricant 52 and having a lubricant inlet 54 and a lubricant outlet 56. A lubricant supply line 62 and a lubricant outlet line 66 each have a respective valves 64, 68 for regulating lubrican

An emergency lubrication system for a turbine engine includes a reservoir 50 containing a reserve quantity of lubricant 52 and having a lubricant inlet 54 and a lubricant outlet 56. A lubricant supply line 62 and a lubricant outlet line 66 each have a respective valves 64, 68 for regulating lubricant flow into and out of the reservoir. A fluid supply line 70 includes a valve 72 for selectively establishing communication between the reserve quantity of lubricant and a source of pressurized fluid. During normal operation the lubricant outlet valve continuously releases lubricant at a normal rate to the component requiring lubrication while the lubricant inlet valve concurrently admits fresh lubricant into the reservoir. During abnormal operation, the lubricant inlet valve closes in response to abnormally low lubricant pressure outside the reservoir thereby preventing backflow of reserve lubricant out of the reservoir. The fluid inlet valve opens to admit pressurized fluid into the reservoir thus pressurizing the reserve lubricant. The lubricant outlet valve opens or cycles open and closed in response to a command from a controller 26 so that the pressurized fluid forces lubricant through the outlet 56 as a subnormal rate, which persists until the lubricant reserve is substantially depleted. The subnormal rate is ideally achieved by intermittently releasing lubricant from the reservoir, but may also be achieved by releasing a continuous stream of lubricant at a rate less than the normal rate of release.

대표청구항 ▼

We claim: 1. In a gas turbine engine having a controller which receives feedback signals from said engine and issues control signals in response thereto, a lubrication system lubricating a component during both normal operating conditions of said engine wherein a normal flow of lubricant is supplie

We claim: 1. In a gas turbine engine having a controller which receives feedback signals from said engine and issues control signals in response thereto, a lubrication system lubricating a component during both normal operating conditions of said engine wherein a normal flow of lubricant is supplied to said component by said lubrication system, and malfunctioning conditions of said engine wherein said normal flow of lubricant supplied to said component by said lubrication system is disrupted, said lubrication system comprising: a reservoir for holding a reserve quantity of lubricant, said reservoir having an inlet and an outlet; said inlet being closed during said malfunctioning condition to prevent backflow of lubricant from said reservoir through said inlet thereof; an air conduit providing fluid communication between a supply of pressurized air and the interior of said reservoir and a control valve responsive to signals provided by said engine controller to effect lubricant flow from the interior of said reservoir through said outlet to said component, said control valve being disposed in said air conduit and being closed for blocking flow of said pressurized air to the interior of said reservoir during normal engine operating conditions and opening to allow pressurization of said reservoir by said pressurized air during said malfunctioning conditions to establish an emergency flow of lubricant to said component. 2. The lubrication system of claim 1 wherein said inlet comprises a removable cap. 3. The lubrication system of claim 1 and further including a check valve in said reservoir outlet for maintaining said outlet closed during said normal engine operating conditions, whereby said component is lubricated entirely independently from said reservoir during said normal operating conditions. 4. The lubrication system of claim 1 wherein said inlet is provided with lubricant from a conduit providing pressurized lubricant for lubricating said component during normal engine operating conditions. 5. The lubrication system of claim 4 and further including a normally open check valve disposed in said inlet conduit, said check valve closing during said engine malfunctioning condition. 6. The lubrication system of claim 5 wherein said reservoir outlet remains in fluid communication with said component during both normal and malfunctioning engine operating conditions. 7. In a gas turbine engine having a controller which receives feedback signals from said engine and issues control signals in response thereto, or said lubrication system lubricating a component during both normal operating conditions of said engine wherein a normal flow of lubricant is supplied to said component by said lubrication system, and malfunctioning conditions of said engine wherein said normal flow of lubricant supplied to said component by said lubrication system is disrupted, said lubrication system comprising: a reservoir for holding a reserve quantity of lubricant, said reservoir having an inlet and an outlet; said inlet being closed during said malfunctioning condition to prevent backflow of lubricant from said reservoir through said inlet thereof; an air conduit providing fluid communication between a supply of pressurized air and the interior of said reservoir and a control valve responsive to signals provided by said engine controller to effect lubricant flow from the interior of said reservoir through said outlet to said component, said control valve being disposed in said reservoir outlet and being open for allowing a normal flow of lubricant from said reservoir during normal engine operating conditions as well as during said engine malfunctioning conditions. 8. The lubrication system of claim 7 wherein said Inlet is provided with lubricant from a conduit providing pressurized lubricant for lubricating said component during normal engine operating conditions. 9. The lubrication system of claim 8 and further including a normally open check valve disposed in said reservoir inlet, said check valve closing in response to said engine malfunctioning condition. 10. The lubrication system of claim 7 and further including a normally closed check valve in said air conduit, said normally closed check valve opening, to allow pressurization of said reservoir by said pressurized air during said engine malfunctioning condition. 11. The lubrication system of claim 7 wherein said component is provided with lubricant from said outlet as well as from said conduit during normal engine operating conditions. 12. The lubrication system of claim 7 wherein under normal engine operating conditions, said component is lubricated by lubricant flow sequentially from said reservoir inlet, through said reservoir and finally, through said reservoir outlet. 13. The lubrication system of claim 7 wherein said control valve opens to a first position to allow normal lubricant flow to said component during normal operating conditions and a second position allowing a less-than-normal lubricant flow through said outlet during said engine malfunctioning conditions. 14. The lubrication system of claim 8 wherein said control valve repeatedly opens and closes to provide an intermittent release of lubricant flow from said reservoir during said engine malfunction conditions. 15. The lubrication system of claim 1 wherein the pressurized air is buffer air supplied by the compressor of said gas turbine engine. 16. The lubrication system of claim 1 wherein said lubricated component comprises a bearing.