초록 ▼

An environmental control system has a cooling loop including a cooling turbine which, in use, drives a compressor, and an intercooler apparatus, for cooling air compressed by the compressor prior to the air being expanded and cooled over the cooling turbine, and a heat exchanger to which at least a

An environmental control system has a cooling loop including a cooling turbine which, in use, drives a compressor, and an intercooler apparatus, for cooling air compressed by the compressor prior to the air being expanded and cooled over the cooling turbine, and a heat exchanger to which at least a proportion of the cooled and expanded air from the turbine is fed to cool a heat load, and wherein, in a first mode of operation, the cooling loop is closed so that the air circulates around the closed loop from the compressor to the intercooler apparatus to the cooling turbine, and thence to the heat exchanger, and back to the compressor, and in a second mode of operation the cooling loop is open to allow working fluid to pass from the system whilst further working fluid is introduced into the cooling loop, and wherein an ambient air inlet valve is provided to provide for the admission of ambient air to the cooling loop, when the system is operating in the second mode of operation.

대표청구항 ▼

1. An environmental control including a power turbine over which, in use, high pressure air from a pressurized air supply is passed, the power turbine driving a compressor, a cooling turbine over which compressed air is expanded and cooled, an intercooler apparatus for cooling air compressed by the

1. An environmental control including a power turbine over which, in use, high pressure air from a pressurized air supply is passed, the power turbine driving a compressor, a cooling turbine over which compressed air is expanded and cooled, an intercooler apparatus for cooling air compressed by the compressor prior to the air being expanded and cooled over the cooling turbine, and a heat exchanger to which at least a proportion of the cooled and expanded air from the cooling turbine is fed to cool a heat load, and wherein the system is operable in each of first and second modes of operation, during each of which the compressor is driven by the high pressure air passing over the power turbine, and in the first mode of operation, there is a closed cooling loop around which the air circulates from the compressor to the intercooler apparatus to the cooling turbine, and thence to the heat exchanger, and back to the compressor, and in the second mode of operation the cooling loop is open to allow air to pass from the system whilst further air is introduced into the cooling loop, and wherein an ambient air inlet valve is provided to provide for the admission of ambient air to the cooling loop, when the system is operating in-the-second mode of operation. 2. A system according to claim 1 wherein the system includes a pressure regulating valve between the cooling loop and a high pressure inlet for air, the pressure regulating valve permitting the introduction of high pressure air into the cooling loop when the pressure in the cooling loop is below a predetermined pressure. 3. A system according to claim 2 wherein the ambient air inlet valve is provided downstream of the pressure regulating valve. 4. A system according to claim 1 wherein the cooling loop is closed and opened by a mode valve in the cooling loop. 5. A system according to claim 4 wherein the ambient air inlet valve is provided upstream of the mode valve. 6. A system according to claim 1 wherein the system includes a pressure regulating valve between the cooling loop and an inlet for high pressure air, the pressure regulating valve permitting the introduction of high pressure air into the cooling loop when the pressure in the cooling loop is below a predetermined pressure the ambient air inlet valve is provided downstream of the pressure regulating valve, and wherein the cooling loop is closed and opened by a mode valve in the cooling loop, the ambient air inlet valve being provided upstream of the mode valve. 7. A system according to claim 1 wherein the system includes a driving device to provide additional drive power to drive the compressor. 8. A system according to claim 7 wherein the driving device is a power turbine over which high pressure air is passed, the power turbine and the cooling turbine and the compressor being provided on a common shaft and being rotatable together. 9. A system according to claim 8 wherein the system includes a pressure regulating valve between the cooling loop and a high pressure inlet for air, the pressure regulating valve permitting the introduction of high pressure air into the cooling loop when the pressure in the cooling loop is below a predetermined pressure, high pressure air for the power turbine being provided to the power turbine from upstream of the pressure regulating valve. 10. A system according to claim 8 wherein cooled and expanded air from the power turbine is fed to the intercooler apparatus to cool compressed air in the cooling loop. 11. A system according to claim 10 wherein the intercooler apparatus includes a ram air heat exchanger for cooling the compressed air. 12. A system according to claim 8 wherein cooled and expanded air from the power turbine is fed to a pre-cooling apparatus to pre-cool high pressure air from an inlet for high pressure air to the system. 13. A system according to claim 12 wherein the pre-cooling apparatus includes a ram air heat exchanger. 14. A aircraft including an environmental control sy stem including a power turbine over which, in use, high pressure air from a pressurized air supply is passed, the power turbine driving a compressor, a cooling turbine over which compressed air is expanded and cooled, an intercooler apparatus for cooling air compressed by the compressor prior to the air being expanded and cooled over the cooling turbine, and a heat exchanger to which at least a proportion of the cooled and expanded air from the cooling turbine is fed to cool a heat load, and wherein the system is operable in each of first and second modes of operation, during each of which the compressor is driven by the high pressure air passing over the power turbine, and in the first mode of operation, there is a closed cooling loop around which the air circulates from the compressor to the intercooler apparatus to the cooling turbine, and thence to the heat exchanger, and back to the compressor, and in the second mode of operation the cooling loop is open to allow air to pass from the system whilst further air is introduced into the cooling loop, and wherein an ambient air inlet valve is provided to provide for the admission of ambient air to the cooling loop, when the system is operating in the second mode of operation.