Environmental control system for supersonic commercial aircraft

Patent metadata

Field	Value
Publication number	US-12162607-B2
Application number	US-202117176655-A
Country	US
Kind code	B2
Filing date	Feb 16, 2021
Priority date	Nov 12, 2020
Publication date	Dec 10, 2024
Grant date	Dec 10, 2024

Abstract

An environmental control system includes a cooling circuit having at least one heat exchanger for cooling a first medium therein. At least one compressing device is operably coupled to the cooling circuit. The at least one compressing device includes a first compressor and a second compressor, wherein the first medium is provided to the first compressor and the second compressor in series, and a temperature of the first medium provided to an inlet of the second compressor is less than the temperature of the first medium at an outlet of the first compressor.

First claim

What is claimed is:

1. An environmental control system comprising:
a cooling circuit including at least one heat exchanger, wherein a first medium is cooled within the at least one heat exchanger by a second medium, the at least one heat exchanger including a first heat exchanger, an intercooler heat exchanger, and a second heat exchanger, and
at least one compressing device operably coupled to the cooling circuit, the at least one compressing device including a first compressor and a second compressor, wherein the first medium is provided to the first compressor and the second compressor in series;
wherein the first heat exchanger is arranged upstream from the first compressor relative to a flow of the first medium, the second heat exchanger is arranged downstream from the second compressor and upstream from the first turbine relative to the flow of the first medium, and the intercooler heat exchanger is positioned downstream from the first compressor and upstream from the second compressor relative to the flow of the first medium such that a temperature of the first medium provided to an inlet of the second compressor is less than the temperature of the first medium at an outlet of the first compressor;
wherein the second medium is fuel.

2. The environmental control system of claim 1 , wherein within the cooling circuit, the primary heat exchanger and the intercooler heat exchanger are arranged in parallel relative to a flow of the second medium.

3. The environmental control system of claim 1 , wherein within the cooling circuit, the secondary heat exchanger and the intercooler heat exchanger are arranged in parallel relative to the flow of the second medium.

4. An environmental control system of comprising:
an inlet for receiving a first medium and an outlet for delivering a conditioned flow of the first medium to one or more loads; and
a first compressing device and a second compressing device arranged in fluid communication with the inlet and the outlet and with each other, each of the first compressing device and the second compressing device including a compressor and a turbine operably coupled via a shaft;
at least one heat exchanger fluidly connected to at least one of the first compressing device and the second compressing device;
a dehumidification system fluidly connected directly to an outlet of the turbine of the first compressing device and fluidly connected directly to the at least one heat exchanger via a valve;
wherein in a first mode of operation, the first medium output from the compressor of the first compressing device bypasses both the compressor and the turbine of the second compressing device and in a second mode of operation, the first medium is provided to the turbines of both the first compressing device and the second compressing device in series with the turbine of the second compressing device being arranged upstream from the turbine of the first compressing device relative to a flow of the first medium.

5. The environmental control system of claim 4 , wherein in the second mode of operation, the first medium is provided to the turbine of the first compressing device and the turbine of the second compressing device in series.

6. The environmental control system of claim 4 , wherein the first medium is provided from the turbine of the first compressing device directly to the turbine of the second compressing device.

7. The environmental control system of claim 4 , wherein in the second mode of operation, the first medium is provided to the compressor of the first compressing device and the compressor of the second compressing device in series.

8. The environmental control system of claim 7 , wherein in the second mode of operation, wherein the first medium is cooled between the compressor of the first compressing device and the compressor of the second compressing device.

9. The environmental control system of claim 8 , further comprising a cooling circuit including at least one heat exchanger, wherein the at least one heat exchanger includes an intercooler heat exchanger located between the compressor of the first compressing device and the compressor of the second compressing device relative to a flow of the first medium.

10. The environmental control system of claim 9 , wherein the first medium is cooled within the at least one heat exchanger by a flow of fuel.

11. The environmental control system of claim 4 , wherein the environmental control system is part of an aircraft and first mode of operation is associated with operation of the aircraft at ground conditions or at subsonic flight.

12. The environmental control system of claim 4 , wherein the second mode of operation is associated with operation of the aircraft at supersonic flight or climb.

13. An environmental control system comprising:
an inlet for receiving a first medium and an outlet for delivering a conditioned flow of the first medium to one or more loads including a cabin;
a cooling circuit including a plurality of heat exchangers, wherein the first medium is cooled within the plurality of heat exchangers by a second medium, the plurality of heat exchanger including at least two heat exchangers; and
at least one compressing device operably coupled to the cooling circuit, the at least one compressing device including at least one compressor and at least one turbine operably coupled by a shaft, the at least two heat exchangers being arranged downstream from the at least one compressor relative to a flow of the first medium, wherein the environmental control system is operable in a plurality of modes, and in each of the plurality of modes the second medium is fuel and is provided to each of the at least two heat exchangers in parallel.

14. The environmental control system of claim 13 , wherein the at least one compressing device includes a first turbine and a second turbine, and in a first mode of the plurality of modes, the first medium bypasses one of the first turbine and the second turbine, and in a second mode of the plurality of modes, the first medium is provided to the first turbine and the second turbine in series.

15. The environmental control system of claim 13 , wherein the at least one compressing device includes a first compressor and a second compressor, and in a first mode of the plurality of modes, the first medium is provided to at least one of the first compressor and the second compressor, and in a second mode of the plurality of modes, the first medium is provided to the first compressor and the second compressor in series.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Ho Tony
• Pess Matthew

Classifications

• B64D2013/0659

  comprising provisions for cooling fuel systems · CPC title

• B64D2013/0648

  with energy recovery means, e.g. using turbines · CPC title

• B64D2013/0618

  with arrangements for reducing or managing bleed air, using another air source, e.g. ram air · CPC title

• B64C30/00

  Supersonic type aircraft · CPC title

• Y02T50/50

  On board measures aiming to increase energy efficiency · CPC title