Integral add heat and surge control valve for compressor

a compressor and control valve technology, applied in the field of compressors, can solve the problems of reducing thermodynamic performance, damage to the compressor, damage to the bearing and support structure of the compressor, etc., and achieves the effects of preventing deicing, rapid response time, and preventing surg

Inactive Publication Date: 2006-03-30
HAMILTON SUNDSTRAND CORP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0007] 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 ...

Problems solved by technology

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 struc...

Method used

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  • Integral add heat and surge control valve for compressor
  • Integral add heat and surge control valve for compressor
  • Integral add heat and surge control valve for compressor

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Embodiment Construction

[0013] A compressed air system is shown schematically at 10 in FIG. 1. The compressed air system 10 includes a compressed air unit 12 comprising a compressor 14 driven by an electric motor 16. A diffuser 18 is arranged before an outlet 22 of the compressor 14, as is known in the art. The diffuser 18 is manipulated by an actuator 19 to vary its area. Air enters the compressor 14 through an inlet 20. Pressure and temperature inlet sensors 24 and 26 are arranged at the inlet 20, and a pressure outlet sensor 28 is arranged at the outlet 22. The actuator 19 and sensors 24, 26 and 28 are schematically shown in communication with a controller 34. The controller 34 uses the sensors 24, 26 and 28 to determine surge and add-heat conditions. The compressed air system 10 described above is suitable for providing, for example, compressed air to an air cycle machine for producing conditioned cabin air.

[0014] The present invention utilizes a duct 30 to fluidly connect the inlet 20 and outlet 22. ...

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Abstract

A compressed air system 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 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.

Description

[0001] 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.BACKGROUND OF THE INVENTION [0002] This invention relates to a compressor that is used, for example, in an aircraft for supplying compressed air to a cabin air conditioning system. [0003] 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. [0004] 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...

Claims

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Application Information

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IPC IPC(8): F04B49/10F04B49/00
CPCB64D13/02B64D13/06B64D2013/0607B64D2013/0644Y02T50/56F04D27/0269F04D29/462F04D29/584F04D27/0215F04D27/0238F04D25/06F04D29/4213F04D29/5806Y02T50/50
Inventor MCAULIFFE, CHRISTOPHERBEERS, CRAIG M.
Owner HAMILTON SUNDSTRAND CORP
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