COMPRESSOR/TURBINE ARRANGEMENT, AIR CONDITIONING UNIT AND METHOD FOR OPERATING A COMPRESSOR/TURBINE ARRANGEMENT

• US 20130067945A1
• Filed: 04/05/2011
• Published: 03/21/2013
• Est. Priority Date: 04/06/2010
• Status: Active Grant

• Current Assignee: Airbus Operations GmbH (Airbus SE)
• Original Assignee: Airbus Operations GmbH (Airbus SE)
• Inventors: Kelnhofer, Juergen
• Granted Patent: US 9,221,543 B2
• Time in Patent Office: Days
• US Class Current: 62/186
• CPC Class Codes: B60H 1/00021 Air flow details of HVAC devices
• CPC Class Codes: B60H 1/00028 Constructional lay-out of the devices in the vehicle
• CPC Class Codes: B60H 2001/00092 of air deflecting or air directing means inside the device
• CPC Class Codes: B60H 2001/0015 Temperature regulation
• CPC Class Codes: B64D 13/06 the air being conditioned pressurising B64D13/02
• CPC Class Codes: B64D 13/08 the air being heated or cooled
• CPC Class Codes: B64D 2013/0688 with means for recirculating cabin air
• CPC Class Codes: F25B 11/00 Compression machines, plants or systems, using turbines, e.g. gas turbines
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

The invention relates to a compressor/turbine arrangement for use in an air conditioning unit of an aircraft air conditioning system comprising a process air supply line which is designed to supply process air generated by a process air source to a compressor. A detection device is designed to detect a characteristic signal for the temperature of the process air flowing through the process air supply line. A turbine is designed to drive the compressor. A cooling device is disposed in a process air line connecting the compressor to the turbine and is designed to cool the process air coming out of the compressor and flowing through the process air line in the direction of the turbine. Downstream of the cooling device a connecting line branches off from the process air line and opens into the process air supply line. A control device is designed to control a process air flow through the connecting line in dependence on the signal detected by the detection device.

Claims

1. Compressor/turbine arrangement for use in an air conditioning unit of an aircraft air conditioning system, having:

a process air supply line which is designed to supply process air generated by a process air source to a compressor,

a detection device which is designed to detect a signal characteristic of the temperature of the process air flowing through the process air supply line,

a turbine which is designed to drive the compressor,

a cooling device which is arranged in a process air line connecting the compressor to the turbine and is designed to cool the process air exiting the compressor and flowing through the process air line in the direction of the turbine,

a connecting line which branches off from the process air line downstream of the cooling device and opens into the process air supply line,

a control device which is designed to control a process air flow through the connecting line in dependence on the signal detected by the detection device and characteristic of the temperature of the process air flowing through the process air supply line, there being no cooling device interposed in the process air supply line, so that the process air flowing through the process air supply line in the region of an end connected to the process air source has substantially the same temperature as the process air flowing through the process air supply line in the region of an end connected to the compressor.

2. Compressor/turbine arrangement according to claim 1, characterised in that the control device is designed to control the process air flow through the connecting line and/or the operation of the cooling device in dependence on the signal detected by the detection device and characteristic of the temperature of the process air flowing through the process air supply line in such a manner as to prevent the temperature of the process air flowing through the process air supply line from exceeding a predetermined maximum value, and/or in that the control device is designed to control the operation of the compressor in dependence on the signal detected by the detection device and characteristic of the temperature of the process air flowing through the process air supply line, in such a manner that a temperature increase which the process air undergoes on compression in the compressor does not exceed a permissible maximum value.

3. Compressor/turbine arrangement according to claim 1, characterised in that the control device is designed, for controlling the process air flow through the connecting line, to control a valve arranged in the connecting line.

4. Compressor/turbine arrangement according to claim 1, characterised by a fan which is designed to be driven by the turbine of the compressor/turbine arrangement.

5. Compressor/turbine arrangement according to claim 1, characterised by a further turbine which is designed to drive the compressor and/or the fan, the process air line connecting the compressor either to the turbine or to the further turbine.

6. Air conditioning unit for an aircraft air conditioning system, characterised by a compressor/turbine arrangement according to claim 1.

7. Air conditioning unit according to claim 6, characterised by a motor which is designed to drive the compressor and/or the fan of the compressor/turbine arrangement.

8. Method for operating a compressor/turbine arrangement provided for use in an air conditioning unit of an aircraft air conditioning system, having the steps:

supplying process air, generated by a process air source, to a compressor through a process air supply line in which no cooling device is provided,

detecting a signal characteristic of the temperature of the process air flowing through the process air supply line,

cooling the process air exiting the compressor by means of a cooling device which is arranged in a process air line connecting the compressor to a turbine, the turbine being designed to drive the compressor

supplying the cooled process air to the turbine

controlling a process air flow through a connecting line, branching off from the process air line downstream of the cooling device and opening into the process air supply line in dependence on the detected signal characteristic of the temperature of the process air flowing through the process air supply line, the process air flowing through the process air supply line in the region of an end connected to the process air source having substantially the same temperature as the process air flowing through the process air supply line in the region of an end connected to the compressor.

9. Method according to claim 8, characterised in that the process air flow through the connecting line and/or the operation of the cooling device is/are controlled in dependence on the detected signal characteristic of the temperature of the process air flowing through the process air supply line in such a manner as to prevent the temperature of the process air flowing through the process air supply line from exceeding a predetermined maximum value, and/or in that the operation of the compressor is controlled in dependence on the signal detected by the detection device and characteristic of the temperature of the process air flowing through the process air supply line, in such a manner that a temperature increase which the process air undergoes on compression in the compressor does not exceed a permissible maximum value.

10. Method according to claim 8, characterised in that the process air flow through the connecting line is controlled by the control of a valve arranged in the connecting line.

11. Method according to claim 8, characterised in that a fan is driven by the turbine of the compressor/turbine arrangement.

12. Method according to claim 8, characterised in that a further turbine drives the compressor and/or the fan, the process air line connecting the compressor either to the turbine or to the further turbine.