Synthesized low-pressure bleed air scheme for aircraft bleed air network

Patent metadata

Field	Value
Publication number	US-11180259-B2
Application number	US-201815927653-A
Country	US
Kind code	B2
Filing date	Mar 21, 2018
Priority date	Mar 21, 2018
Publication date	Nov 23, 2021
Grant date	Nov 23, 2021

Abstract

An aircraft includes one or more engines configured to generate high-pressure bleed air and low-pressure bleed air. An aircraft environmental control system (ECS) is in fluid communication with one or more of the engines to receive the high-pressure bleed air and the low-pressure bleed air. The ECS calculates a synthesized low-pressure value associated with the low-pressure bleed air while still providing bleed air using the high pressure bleed air. The ECS further switches from the high pressure bleed air to the low-bleed pressure air through the ECS while blocking flow of the high-pressure bleed air through the ECS based on the synthesized low-pressure value.

First claim

What is claimed is:

1. A method of controlling an aircraft environmental control system (ECS), the method comprising:
selectively generating high-pressure bleed air and low-pressure bleed air using at least one engine installed on an aircraft;
selectively delivering at least one of the high-pressure bleed air and the low-pressure bleed air to an air conditioning unit installed on the aircraft;
measuring, via a pressure sensor, a pressure of the high-pressure bleed air;
determining a predetermined schedule of bleed air pressure ratio values by simulating a plurality of high-pressure bleed air values with respect to a plurality of simulated low-pressure bleed air values over a plurality of operating conditions, and storing the schedule of bleed air pressure ratio values in an electronic ECS controller,
calculating, via the electronic ECS controller, a synthesized low-pressure value associated with the low-pressure bleed air while delivering the high-pressure bleed air to the air conditioning unit, wherein the synthesized low-pressure value is calculated as the measured pressure of the high-pressure bleed air divided by a maximum value of the bleed air pressure ratio values; and
switching from delivering the high-pressure bleed air to the air conditioning unit to delivering the low-pressure bleed air to the air conditioning unit while blocking flow of the high-pressure bleed air through the ECS based on the synthesized low-pressure value.

2. The method of claim 1 , wherein the synthesized low-pressure value is indicative of the pressure at the low-pressure bleed air duct after switching to delivering the low-pressure bleed air to the air conditioning unit while blocking flow of the high-pressure bleed air through the ECS.

3. The method of claim 1 , wherein selectively delivering at least one of the high-pressure bleed air and the low-pressure bleed air to the air conditioning unit comprises:
delivering the high-pressure bleed air to a high-pressure bleed air duct;
delivering the low-pressure bleed air to a low-pressure bleed air duct;
adjusting at least one valve that is in fluid communication with the high-pressure bleed air duct into a first position to control flow of the high-pressure bleed air through the air condition unit; and
adjusting the at least one valve into a second position to control flow of the low-pressure bleed air through the air condition unit,
wherein the ECS controller adjusts the at least one valve into the first and second positions based on the synthesized low-pressure value.

4. The method of claim 3 , wherein adjusting the at least one valve further comprises:
comparing, via the ECS controller, the synthesized low-pressure value to a low-pressure (LP) threshold value; and
adjusting the at least one valve into the second position to output the low-pressure bleed air in response to the synthesized low-pressure value being greater than the LP threshold value.

5. The method of claim 4 , wherein adjust the at least one valve further comprises:
adjusting the at least one valve to invoke the first position to output the high-pressure bleed air in response to a ECS minimum pressure required at a bleed manifold being greater than the bleed manifold pressure; and
after invoking the first position of the valve, returning the at least one valve to the second position to output the low-pressure bleed air in response to the synthesized low-pressure value being greater than the LP threshold value.

6. An aircraft environmental control system (ECS) comprising:
an airflow network including:
a high-pressure bleed air duct configured to receive high-pressure bleed air generated by at least one aircraft engine;
a pressure sensor configured to measure a pressure of the high-pressure bleed air;
a low-pressure bleed air duct configured to receive low-pressure bleed air generated by the at least one aircraft engine;
at least one air condition unit configured to generate temperature-regulated air using either the high-pressure bleed air or the low-pressure bleed air;
at least one valve configured to receive the high-pressure bleed air, the at least one valve configured to operate in a first position to control flow of the high-pressure bleed air through the air conditioning unit, and a second position to control flow of the low-pressure bleed air through the air conditioning unit; and
an electronic ECS controller in signal communication with the airflow network, the electronic ECS controller configured store a predetermined schedule of bleed air pressure ratio values between simulated high-pressure bleed air values and simulated low-pressure bleed air values, to calculate a synthesized low-pressure value associated with the low-pressure bleed air, and to adjust a position of the at least one valve based on the synthesized low-pressure value,
wherein the synthesized low-pressure value is calculated as the measured pressure of the high-pressure bleed air divided by a maximum value of the bleed air pressure ratio values.

7. The ECS of claim 6 , wherein the synthesized low-pressure value is indicative of the pressure at the low-pressure bleed air duct after the at least one valve is adjusted to operate in the second position.

8. The aircraft ECS of claim 6 , wherein the ECS controller compares the synthesized low-pressure value to a low-pressure (LP) threshold value, and adjusts the at least one valve into the second position to output the low-pressure bleed air in response to the synthesized low-pressure value being greater than the LP threshold value.

9. The aircraft ECS of claim 8 , wherein the ECS controller calculates the synthesized low-pressure value based on a required amount of airflow through the at least one engine, ambient temperature, ambient pressure, ECS operating mode, and the measured pressure of the high-pressure bleed air.

10. The aircraft ECS of claim 9 , wherein the aircraft includes a plurality of engines, and wherein the ECS is configured to operate in a plurality of different operating modes, a first mode among the plurality of operating modes configured to generate the high-pressure bleed air and the low-pressure bleed air from at least two engines among the plurality of engines, and a second operating mode among the plurality of operating modes configured to generate the high-pressure bleed air and the low-pressure bleed air from a single engine among the plurality of engines.

11. The aircraft ECS of claim 10 , wherein the ECS controller determines the LP threshold value based on a current operating mode among the plurality of different operating modes of the ECS.

12. The aircraft ECS of claim 11 , wherein the ECS controller adjusts the at least one valve into the first position to output the high-pressure bleed air in response to an ECS minimum pressure required at a bleed manifold being greater than the bleed manifold pressure, and after invoking the first position of the valve, returns the at least one valve to the second position to output the low-pressure bleed air in response to the synthesized low-pressure value being greater than the LP threshold value.

13. An aircraft comprising:
at least one engine configured to generate high-pressure bleed air and low-pressure bleed air; and
an aircraft environmental control system (ECS) in fluid communication with the at least one engine to receive the high-pressure bleed air and the low-pressure bleed air, the ECS including:
an airflow network including a high-pressure bleed air duct to receive the high-pressure bleed air, a low-pressure bleed air duct to receive the low-pressure bleed air;
at least one valve that receives the high-pressure bleed air, the at least on

Assignees

• Hamilton Sundstrand Corp

Inventors

• Kamenetz Jeffry K
• Kline Erin G
• Ernst Jeffrey
• Schroder Bruce R
• Deroy Kevin R
• Vessella Vince
• Mcgrath Darragh
• Fagnani Adam
• Labrecque Michel

Classifications

• B64D13/06 Primary

  the air being conditioned (pressurising B64D13/02) · CPC title

• F02C6/08

  the gas being bled from the gas-turbine compressor · CPC title

• B64D2013/0618

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

• F02C7/08

  Heating air supply before combustion, e.g. by exhaust gases · CPC title

• F02C9/18

  by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages {(F02C3/113 takes precedence)} · CPC title