Compressor and gas turbine

US2016169241A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016169241-A1
Application numberUS-201414907987-A
CountryUS
Kind codeA1
Filing dateFeb 12, 2014
Priority dateOct 17, 2013
Publication dateJun 16, 2016
Grant date

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A compressor includes a rotor rotating about an axis thereof; a rotor casing surrounding the rotor from an outer circumferential side of the rotor and forming a main flow passage of a fluid between the rotor; an extraction-chamber casing provided at an outer circumferential side of the rotor casing, and forming an extraction chamber that communicates with the main flow passage between the rotor casing; and an extraction nozzle connected to the extraction-chamber casing from an outer circumferential side of the extraction-chamber casing and guiding the fluid inside the extraction chamber to an outside of the compressor. A gap in a radial direction between the extraction-chamber casing and the rotor casing is larger at a side of the extraction nozzle in a rearward rotation direction of the rotor than at a side of the extraction nozzle in the forward rotation direction of the rotor.

First claim

Opening claim text (preview).

1 . A compressor comprising: a rotor rotating about an axis thereof; a rotor casing surrounding the rotor from an outer circumferential side of the rotor and forming a main flow passage of a fluid between the rotor; an extraction-chamber casing provided at an outer circumferential side of the rotor casing, and forming an extraction chamber that communicates with the main flow passage between the rotor casing; and an extraction nozzle connected to the extraction-chamber casing from an outer circumferential side of the extraction-chamber casing and guiding the fluid inside the extraction chamber to an outside of the compressor, wherein an inner circumferential surface of the extraction nozzle and the outer circumferential surface in the radial direction of the extraction chamber are connected with a smooth curve surface that is convex toward the flow passage of the fluid, and wherein a gap in a radial direction between the extraction-chamber casing and the rotor casing is larger at a side of a position where the extraction nozzle is provided in a rearward rotation direction of the rotor than at a side of the position where the extraction nozzle is provided in the forward rotation direction of the rotor. 2 . The compressor according to claim 1 , wherein the gap, in the radial direction between the extraction-chamber casing and the rotor casing and at the side of the extraction nozzle in the rearward rotation direction, is formed so as to become gradually larger toward the forward rotation direction of the rotor. 3 . The compressor according to claim 1 , wherein the gap, in the radial direction between the extraction-chamber casing and the rotor casing and at the side of the extraction nozzle in the forward rotation direction, is formed so as to become gradually smaller toward the rearward rotation direction of the rotor. 4 . (canceled) 5 . A gas turbine comprising: the compressor according to claim 1 and configured to compress an air as the fluid by the rotation of the rotor; a combustor generating combustion gas by burning a fuel in a compressed air compressed by the compressor; and a turbine driven by the combustion gas from the combustor.

Assignees

Inventors

Classifications

  • F04D27/023Primary

    Details or means for fluid extraction · CPC title

  • especially adapted for elastic fluid pumps · CPC title

  • Arrangements therefor, e.g. bleed or by-pass valves · CPC title

  • Heating air supply before combustion, e.g. by exhaust gases · CPC title

  • the gas being bled from the gas-turbine compressor · CPC title

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What does patent US2016169241A1 cover?
A compressor includes a rotor rotating about an axis thereof; a rotor casing surrounding the rotor from an outer circumferential side of the rotor and forming a main flow passage of a fluid between the rotor; an extraction-chamber casing provided at an outer circumferential side of the rotor casing, and forming an extraction chamber that communicates with the main flow passage between the rotor…
Who is the assignee on this patent?
Mitsubishi Heavy Ind Ltd
What technology area does this patent fall under?
Primary CPC classification F04D27/023. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Thu Jun 16 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).