ESC energy recovery system for fuel-efficient aircraft

• US 4,419,926 A
• Filed: 09/02/1980
• Issued: 12/13/1983
• Est. Priority Date: 09/02/1980
• Status: Expired due to Term

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Cronin, Michael J., Seid, Gordon
• Primary Examiner(s): Makay, Albert J.
• Assistant Examiner(s): Joyce, Harold
• Application Number:
  US06/183,499
• Time in Patent Office: 1,197 Days
• Field of Search: 98/1.5, 165/15, 237/11
• US Class Current: 454/74
• CPC Class Codes: B64D 13/06 the air being conditioned pressurising B64D13/02
• CPC Class Codes: B64D 2013/0644 including electric motors or generators
• CPC Class Codes: B64D 2013/0648 with energy recovery means, e.g. using turbines
• CPC Class Codes: Y02T 50/50 On board measures aiming to increase energy efficiency

Abstract

The invention is an energy recovery system (20) which uses excess air emanating from an aircraft cabin (16) to drive a turbo-compressor unit (30). The outlet air from the compressor (26) of turbo-compressor unit (30) is optionally fed, either around or through heat exchanger (24), back into the aircraft cabin (16) inlet line, reducing the amount of bleed air required to power the aircraft ECS. Mass flow sensors (34) and (38) are used, via flow control valve (36) and flow control valve control unit (40), to monitor and control the amount of engine bleed air required at any point in time to satisfy overall ECS requirements. The energy recovery system (20") may be utilized in conjunction with a motor driven cabin compressor (42) to reduce the output air requirements of the compressor and thus the weight and horsepower requirements of the compressor motor. In another embodiment, the outlet of the compressor (26) is used to supercharge the inlet of the motor driven cabin compressor (42), reducing the weight and horsepower motor requirements of the ECS.

Claims

1. An aircraft environmental control system for supplying a predetermined amount of conditioned air to an aircraft cabin, comprising:

an electric motor;

a cabin compressor arranged to be driven by said electric motor, said cabin compressor having an outlet adapted and arranged to supply heated and pressurized air to said cabin;

a supercharging compressor connected in series between a source of fresh air and an inlet of said motor-driven cabin compressor;

a free-running turbine mechanically coupled to said supercharging compressor to form a turbo-compressor arranged and adapted to be driven solely by discharge air emanating from said cabin, whereby the inlet of said motordriven cabin compressor may be provided with pressurized fresh air when said cabin is discharging pressurized air overboard.

2. An environmental control system as in claim 1 wherein said predetermined amount of conditioned air exceed the amount of air desired in said aircraft cabin during flight, said turbo-compressor being arranged so as to be driven by said excess air as it is discharged from said cabin.

3. An environmental control system as in claim 2 including a heat exchanger interposed between said supercharging compressor and said motor-driven cabin compressor.

4. An environmental control system as in claim 3 including means for optionally directing the heated air output of said supercharging compressor through said heat exchanger.

5. An environmental control system as in claim 4 including means for directing said discharge air through said heat exchanger after it has passed through said turbo-compressor.

6. An environmental control system as in claim 2 wherein said turbo-compressor includes means for bypassing said excess discharged air.

7. An environmental control system as in claim 2 wherein said motor-driven cabin compressor includes inlet guide vane means for controlling the pressure rise across said motor-driven cabin compressor.

8. An environmental control system as in claim 7 including control means for monitoring the air pressure at the input to said cabin and for adjusting said inlet guide vane means in response to said monitored data, so that the desired input of conditioned air to said cabin is maintained.

9. A process for supplying a predetermined amount of conditioned air to an aircraft cabin during flight, comprising the following steps:

providing an electric motor;

providing a primary cabin compressor;

adapting and arranging said cabin compressor to be driven by said motor with an inlet and an outlet respectively in communication with a source of fresh air and with said cabin;

connecting said motor to a continuing supply of electrical power to thereby drive said cabin compressor and provide a supply of heated and pressurized fresh air to said cabin;

providing a supercharging compressor;

connecting said supercharging compressor in series between said cabin compressor and said source of fresh air; and

driving said supercharging compressor solely with energy extracted from discharge air emanating from said cabin to thereby reduce the electrical energy required to operate said motor.

10. A process as in claim 9 wherein the amount of conditioned air supplied to said cabin exceeds the amount of air desired in said cabin, said driving of said supercharging compressor further comprising the steps of:

discharging said excess air from said cabin;

providing a turbine adapted to be driven by said discharged air, said supercharging compressor being arranged so as to be driven by said turbine;

supplying the inlet of said supercharging compressor with ram air; and

driving said turbine with said excess discharged air to drive said supercharging compressor and supercharge said inlet of said motor-driven cabin compressor.

11. A process as in claim 10 further including the steps of:

providing a heat exchanger in series between said supercharging compressor and said motor-driven cabin compressor;

passing the outlet air from said turbine through said heat exchanger; and

cooling the hot-pressurized fresh-air from the outlet of said supercharging compressor by passing it through said heat exchanger prior to being introduced into said inlet of said motor-driven cabin compressor.

12. A process as in claim 10 further including the steps of:

providing means to monitor the pressure of the output of said supercharging compressor and the input pressure of conditioned air to said cabin;

providing inlet guide vanes on said motor-driven cabin compressor;

monitoring the values of the output pressure of said supercharging compressor and the input pressure of conditioned air to said cabin; and

in response to said values, controlling the pressure rise across said motor-driven cabin compressor by adjusting said inlet vanes such that the desired input of conditioned air to said cabin is attained.