Integrated environmental control system
First Claim
1. An integrated environmental control system for providing conditioned supply air to a load, which comprises:
- a. first shaft including means for mechanically compressing and cooling the supply air;
b. second shaft including means for mechanically compressing and cooling the supply air;
c. common heat transfer component means for cooling the supply air through heat exchange relationship with a cooling fluid;
d. a supply fluid delivery means for delivering the supply air separately into the first shaft means and the second shaft means and for delivering the supply air in common through the common heat transfer component means to the load; and
e. shut off valve means for selectively shutting off delivery of the supply air to either the first shaft means or the second shaft means whenever the shut off valve means detects an interruption in flow of conditioned supply air from either the first or second shaft means so that the supply air continues to be conditioned by the non-interrupted shaft means and by heat transfer components of the common heat transfer component means.
1 Assignment
0 Petitions
Accused Products
Abstract
An integrated environmental control system is disclosed for providing conditioned supply air to loads such as a passenger cabin of an aircraft. The system comprises at least two shafts, each shaft having a fan, compressor, and turbine mechanically secured to the shaft; common heat transfer components including primary and secondary heat exchangers, a reheater, and a condenser with a water collector; lines that deliver the supply air separately through the compressors and turbines of each shaft and deliver the supply air in common through the common heat transfer components to the load; and shutoff valves secured in fluid communication with each turbine. Upon interruption in the flow of cooled supply air out of a particular turbine secured to any of the shafts, a shutoff valve shuts off transfer of the supply air to that particular turbine on that interrupted shaft and the remaining shafts and their respective fans, compressors, turbines, and the common heat transfer components continue to receive, condition and deliver the supply air to the load in a redundant operating mode. Because the total heat exchange capacity of the integrated, common heat transfer components is large enough to satisfy conditioned air requirements of the load, and in the redundant operating mode the supply air is exposed to that total heat exchange capacity, the system provides enhanced redundant operating mode performance and offers decreased weight, size, and cost over known systems having mechanical components of a comparable size, weight and work capacity.
147 Citations
18 Claims
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1. An integrated environmental control system for providing conditioned supply air to a load, which comprises:
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a. first shaft including means for mechanically compressing and cooling the supply air; b. second shaft including means for mechanically compressing and cooling the supply air; c. common heat transfer component means for cooling the supply air through heat exchange relationship with a cooling fluid; d. a supply fluid delivery means for delivering the supply air separately into the first shaft means and the second shaft means and for delivering the supply air in common through the common heat transfer component means to the load; and e. shut off valve means for selectively shutting off delivery of the supply air to either the first shaft means or the second shaft means whenever the shut off valve means detects an interruption in flow of conditioned supply air from either the first or second shaft means so that the supply air continues to be conditioned by the non-interrupted shaft means and by heat transfer components of the common heat transfer component means. - View Dependent Claims (2, 3, 4, 5)
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6. An integrated environmental control system for providing conditioned supply air to a load, which comprises:
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a. a first shaft having a first fan, first compressor and first turbine mechanically secured to the first shaft for mechanically compressing and cooling the supply air; b. a second shaft having a second fan, second compressor and second turbine mechanically secured to the second shaft for mechanically compressing and cooling the supply air; c. common heat transfer component means for cooling the supply air through heat exchange relationship with a cooling fluid; d. a supply fluid delivery means for delivering the supply air in a first compressor line to the first compressor and in a separate second compressor line to the second compressor, and for delivering the supply air in a first turbine feed line to the first turbine and in a separate second turbine feed line to the second turbine, and for delivering the supply air in common delivery lines through the common heat transfer component means to the load; e. a first shut off valve secured to the first turbine feed line and a second shut off valve secured to the second turbine feed line for selectively shutting off delivery of the supply air to either the first turbine or the second turbine; and f. detecting means in electrical communication with the first and second shut off valves for selectively shutting off delivery of supply air to either the first turbine or second turbine to stop rotation of the first or second shaft whenever the detecting means detects an interruption in flow of conditioned supply air from either the first turbine or the second turbine so that the supply air continues to be mechanically compressed and cooled by the compressor and turbine on the rotating shaft and continues to be cooled by heat transfer components of the common heat transfer component means as the system operates in a redundant operating mode. - View Dependent Claims (7, 8, 9, 10, 11, 12)
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13. An integrated environmental control system for providing conditioned supply air to an aircraft cabin, which comprises:
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a. a first shaft having a first fan, first compressor and first turbine mechanically secured to the first shaft for mechanically compressing and cooling the supply air; b. a second shaft having a second fan, second compressor and second turbine mechanically secured to the second shaft for mechanically compressing and cooling the supply air; c. a common primary heat exchanger and common secondary heat exchanger positioned within a ram air duct in heat exchange relationship with a ram air cooling fluid passing through the ram air duct; d. a supply fluid line in fluid communication with the first compressor, first turbine, second compressor, second turbine, primary heat exchanger and secondary heat exchanger that delivers the supply air in a first compressor line to the first compressor and in a separate second compressor line to the second compressor, and delivers the supply air in a first turbine feed line to the first turbine and in a separate second turbine feed line to the second turbine, and that delivers the supply air in common delivery lines through the common primary heat exchanger and common secondary heat exchanger to the aircraft cabin; e. a first shut off valve secured to the first turbine feed line and a second shut off valve secured to the second turbine feed line for selectively shutting off delivery of the supply air to either the first turbine or the second turbine; and f. detecting means in electrical communication with the first and second shut off valves for selectively shutting off delivery of supply air to either the first turbine or second turbine to stop rotation of the first or second shaft whenever the detecting means detects an interruption in flow of conditioned supply air from either the first turbine or the second turbine so that the supply air continues to be mechanically compressed and cooled by the compressor and turbine on the rotating shaft and continues to be cooled by the common primary heat exchanger and common secondary heat exchanger as the system operates in a redundant operating mode. - View Dependent Claims (14, 15, 16, 17, 18)
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Specification