Method and system for controlling an auxiliary power unit

Patent metadata

Field	Value
Publication number	US-9976684-B2
Application number	US-201213692672-A
Country	US
Kind code	B2
Filing date	Dec 3, 2012
Priority date	Dec 6, 2011
Publication date	May 22, 2018
Grant date	May 22, 2018

Abstract

A method for controlling the operation of an auxiliary power unit supplying an aircraft air conditioning system with compressed process air includes determining a heating or cooling requirement of an aircraft region to be air-conditioned, determining a desired value of at least one process air flow parameter in dependence on the determined heating or cooling requirement of the aircraft region to be air-conditioned, controlling the operation of the auxiliary power unit in dependence on the determined process air flow parameter desired value, acquiring an actual value of the at least one process air flow parameter, comparing the process air flow parameter actual value with the process air flow parameter desired value and controlling the operation of the auxiliary power unit in dependence on the result of the comparison of the process air flow parameter actual value with the process air flow parameter desired value.

First claim

The invention claimed is:

1. A method for controlling operation of an auxiliary power unit supplying an air conditioning system of an aircraft with compressed process air in ground operation of the aircraft, comprising:
(a) determining a heating or cooling requirement of an aircraft region to be air-conditioned,
(b) determining a desired value of at least one process air flow parameter for a process air flow in a region between the auxiliary power unit and the air conditioning system in dependence on the heating or cooling requirement of the aircraft region to be air-conditioned determined in step (a), the process air flow parameter being characteristic of the properties of a flow of compressed process air which is tapped off from the auxiliary power unit and supplied to the aircraft air conditioning system, wherein at least one of a volume flow, a mass flow, a temperature and a pressure of the compressed process air supplied to the aircraft air conditioning system by the auxiliary power unit is used as the process air flow parameter,
(c) controlling the operation of the auxiliary power unit in dependence on the process air flow parameter desired value determined in step (b),
(d) acquiring an actual value of the at least one process air flow parameter characteristic of the properties of the process air flow in said region between the auxiliary power unit and the air conditioning system,
(e) comparing the process air flow parameter actual value with the process air flow parameter desired value and
(f) controlling the operation of the auxiliary power unit in dependence on a result of comparison in step (e) of the process air flow parameter actual value with the process air flow parameter desired value.

2. The method according to claim 1 , further comprising:
acquiring an actual value of at least one air conditioning system operating parameter characteristic of an operating state of the aircraft air conditioning system and
controlling the operation of the auxiliary power unit in dependence on the air conditioning system operating parameter actual value.

3. The method according to claim 2 ,
wherein at least one of the heating or cooling requirement of the aircraft region to be air-conditioned, an air conditioning system capacity utilisation parameter characteristic of a capacity utilisation state of the aircraft air conditioning system and an air conditioning system fault parameter characteristic of an apparatus fault or a system fault of the aircraft air conditioning system is used as the air conditioning system operating parameter.

4. The method according to claim 2 ,
wherein at least one of the process air flow parameter actual value and the air conditioning system operating parameter actual value is acquired by an acquiring device which is integrated in the aircraft air conditioning system and the signals of which are also used to control the operation of the aircraft air conditioning system.

5. The method according to claim 2 ,
wherein at least one of the process air flow parameter actual value and the air conditioning system operating parameter actual value is continuously acquired.

6. A system for controlling operation of an auxiliary power unit supplying an air conditioning system of an aircraft with compressed process air in ground operation of the aircraft, which comprises:
a determiner configured to determine a desired value of at least one process air flow parameter for a process air flow in a region between the auxiliary power unit and the air conditioning system in dependence on a heating or cooling requirement of an aircraft region to be air-conditioned, the process air flow parameter being characteristic of the properties of a flow of compressed process air which is tapped off from the auxiliary power unit and supplied to the aircraft air conditioning system, wherein at least one of a volume flow, a mass flow, a temperature and a pressure of the compressed process air supplied to the aircraft air conditioning system by the auxiliary power unit is used as the process air flow parameter,
an acquirer configured to acquire an actual value of the at least one process air flow parameter characteristic of the properties of the process air flow in said region between the auxiliary power unit and the air conditioning system, and
a controller configured to control the operation of the auxiliary power unit, by controlling the operation of the auxiliary power unit first in dependence on the process air flow parameter desired value determined by said determiner, and by controlling the operation of the auxiliary power unit, after the acquirer acquires the process air flow parameter actual value, in dependence on a result of a comparison of the process air flow parameter actual value with the process air flow parameter desired value.

7. The system according to claim 6 ,
wherein the system furthermore comprises an acquirer configured to acquire an actual value of at least one air conditioning system operating parameter characteristic of an operating state of the air conditioning system, and controller is further configured to control the operation of the auxiliary power unit in dependence on the actual value of the air conditioning system operating parameter.

8. The system according to claim 7 ,
wherein at least one of the heating or cooling requirement of the aircraft region to be air-conditioned, an air conditioning system capacity utilisation parameter characteristic of a capacity utilisation state of the aircraft air conditioning system and an air conditioning system fault parameter characteristic of an apparatus fault or a system fault of the aircraft air conditioning system is used as the air conditioning system operating parameter.

9. The system according to claim 6 ,
wherein the acquirer configured to acquire the process air flow parameter actual value is integrated in the aircraft air conditioning system and includes signals which are also used to control the operation of the aircraft air conditioning system.

10. The system according to claim 7 ,
wherein the acquirer configured to acquire the air conditioning system operating parameter actual value is integrated in the aircraft air conditioning system and includes signals which are also used to control the operation of the aircraft air conditioning system.

11. The system according to claim 7 ,
wherein at least one of the acquirer configured to acquire the process air flow parameter actual value and the acquirer configured to acquire the air conditioning system operating parameter actual value is configured to continuously acquire at least one of the process air flow parameter actual value and the air conditioning system operating parameter actual value.

12. Use of at least one of (a) a method for controlling operation of an auxiliary power unit supplying an air conditioning system of an aircraft with compressed process air in ground operation of the aircraft, comprising (i) determining a heating or cooling requirement of an aircraft region to be air-conditioned, (ii) determining a desired value of at least one process air flow parameter for a process air flow in a region between the auxiliary power unit and the air conditioning system in dependence on the heating or cooling requirement of the aircraft region to be air-conditioned determined in step (i), the process air flow parameter being characteristic of the properties of a flow of compressed process air which is tapped off from the auxiliary power unit and supplied to the aircraft air conditioning system, wherein at least one of a volume flow, a mass flow, a temperature and a pressure of the compressed process air supplied to the aircraft air conditioni

Assignees

• Airbus Operations Gmbh

Inventors

• Kelnhofer Jurgen
• Krakowski Dariusz

Classifications

• F02C6/06

  providing compressed gas (F02C6/10 takes precedence) · CPC title

• Y10T137/0318

  Processes · CPC title

• B64D2013/0611

  combined with auxiliary power units (APU's) · CPC title

• F05D2270/306

  Mass flow · CPC title

• Y02T50/56

  Cross-Sectional Technologies · mapped topic