This invention relates to a compressor that is used, for example, in an aircraft for supplying compressed air to a cabin air conditioning system.
In some compressor applications in aircraft, air entering a compressor inlet contains water and operates at temperatures below freezing. Ice forming at the inlet reduces the thermodynamic performance of the compressor, can cause damage to the compressor as the ice sheds and can damage the bearing and support structure of the compressor.
Compressors may occasionally operate in an undesirable surge condition in which the ratio between compressor outlet and compressor inlet pressures is undesirable. To avoid surge it is desirable to either lower the compressor outlet pressure or raise the compressor inlet pressure to obtain a pressure ratio within a desired range.
What is needed is a deicing and surge control device that is capable of deicing the compressor inlet and controlling surge in efficient, rapid manner.
The invention provides a compressed air system that includes a compressor having an inlet and an outlet. A duct fluidly connects the outlet to the inlet and has a valve arranged in the duct. A controller communicates with the valve and commands the valve to move between first and second positions in response to a surge condition and/or for an add-heat condition to regulate an amount of fluid flowing through the duct. The valve opens to provide hot air from the compressor outlet to deice the inlet or to provide the higher pressure compressor outlet air to the lower pressure compressor inlet air to obtain a pressure ratio in a desired range.
The inventive compressed air unit is designed to provide a compact arrangement so that the valve providing the heated, pressurized air to the inlet is located in close proximity to the inlet for a rapid response time. The duct comprises a relatively short length of tubing interconnecting an add-heat supply outlet and an add-heat plenum inlet, which are provided by a housing of the compressor. The housing also includes an add-heat plenum having an annular wall arranged at the inlet to provide an annular cavity. Hot air from the compressor outlet is provided to the plenum to heat the annular wall quickly at the inlet to prevent deicing.
Accordingly, the present invention provides a deicing and surge control device that deices the compressor and prevents surge.
These and other features of the present invention can be best understood from the following specification and drawings, the following of which is a brief description.
A compressed air system is shown schematically at 10 in
The present invention utilizes a duct 30 to fluidly connect the inlet 20 and outlet 22. A valve 32 is arranged between the inlet 20 and outlet 22 within the duct 30. The controller 34 is in communication with the valve 32 to move it between first and second positions F and S in response to the surge and add-heat conditions. According to this invention, only one valve is used for these conditions. In one example, the valve 32 is a butterfly valve.
Referring to
An impeller 66 is secured to the rotor 64. The impeller 66 has an inlet side 65 and outlet side 67. The diffuser 18 is arranged on the outlet side 67 between the impeller 66 and the outlet 22. The housing 40 includes a diffuser shroud 68 in close proximity to the impeller 66. The diffuser shroud 68 extends beyond an end 69 of the impeller 66.
The housing 40 provides an add-heat plenum 72 formed by the diffuser shroud 68 and the add-heat housing 46. The diffuser shroud 68 provides a curved annular wall 70 that tapers radially outwardly as it extends axially away from the end 69 of the impeller 66.
The outlet housing 44 provides an add-heat supply outlet 74 (best shown in
Although a preferred embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.
The present application is a continuation-in-part application of U.S. application Ser. No. 10/978,641 filed on Nov. 1, 2004 that claims priority to U.S. Provisional Patent Application Ser. No. 60/611,992, filed Sep. 22, 2004.
Number | Date | Country | |
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60611992 | Sep 2004 | US |
Number | Date | Country | |
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Parent | 10978641 | Nov 2004 | US |
Child | 11269082 | Nov 2005 | US |