MX338204B - Rotor de compresor supersonico y metodo para comprimir un fluido. - Google Patents

Rotor de compresor supersonico y metodo para comprimir un fluido.

Info

Publication number
MX338204B
MX338204B MX2013013944A MX2013013944A MX338204B MX 338204 B MX338204 B MX 338204B MX 2013013944 A MX2013013944 A MX 2013013944A MX 2013013944 A MX2013013944 A MX 2013013944A MX 338204 B MX338204 B MX 338204B
Authority
MX
Mexico
Prior art keywords
compressor rotor
flow channel
supersonic compressor
supersonic
compressing
Prior art date
Application number
MX2013013944A
Other languages
English (en)
Other versions
MX2013013944A (es
Inventor
Douglas Carl Hofer
Dhananjayarao Gottapu
Original Assignee
Gen Electric
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Gen Electric filed Critical Gen Electric
Publication of MX2013013944A publication Critical patent/MX2013013944A/es
Publication of MX338204B publication Critical patent/MX338204B/es

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00—Axial-flow pumps
    • F04D19/02—Multi-stage pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00—Axial-flow pumps
    • F04D19/02—Multi-stage pumps
    • F04D19/024—Multi-stage pumps with contrarotating parts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D21/00—Pump involving supersonic speed of pumped fluids

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)

Abstract

Un rotor de compresor supersónico. El rotor del compresor supersónico incluye un cuerpo (56) de disco esencialmente cilíndrico que incluye una superficie (68) corriente arriba, una superficie (70) corriente abajo y una superficie (66) radialmente externa que se extiende generalmente en forma axial entre la superficie (68) corriente arriba y la superficie corriente abajo. El cuerpo de disco define un eje (62) de línea central. Una pluralidad de aletas (54) está acoplada con la superficie radialmente externa. Las aletas adyacentes forman un par y están orientadas de tal forma que se define un canal (88) de flujo entre cada par de aletas adyacentes. El canal de flujo se extiende generalmente en forma axial entre la abertura (90) de entrada y la abertura (92) de salida. Por lo menos una rampa (112) de compresión supersónica está colocada dentro del canal de flujo. La rampa de compresión supersónica se puede colocar, en forma selectiva, en una primera posición (156), en una segunda posición (158) y en cualquier posición entre ellas.
MX2013013944A 2011-05-27 2012-05-25 Rotor de compresor supersonico y metodo para comprimir un fluido. MX338204B (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/117,878 US8770929B2 (en) 2011-05-27 2011-05-27 Supersonic compressor rotor and method of compressing a fluid
PCT/US2012/039492 WO2012166564A1 (en) 2011-05-27 2012-05-25 Supersonic compressor rotor and method of compressing a fluid

Publications (2)

Publication Number Publication Date
MX2013013944A MX2013013944A (es) 2014-01-23
MX338204B true MX338204B (es) 2016-04-07

Family

ID=46178863

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2013013944A MX338204B (es) 2011-05-27 2012-05-25 Rotor de compresor supersonico y metodo para comprimir un fluido.

Country Status (10)

Country Link
US (1) US8770929B2 (es)
EP (1) EP2715143B1 (es)
JP (1) JP6078053B2 (es)
KR (1) KR20140024911A (es)
CN (1) CN103597213B (es)
AU (1) AU2012262564A1 (es)
BR (1) BR112013029742A2 (es)
CA (1) CA2836303A1 (es)
MX (1) MX338204B (es)
WO (1) WO2012166564A1 (es)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202991533U (zh) * 2011-07-09 2013-06-12 拉姆金动力系统有限责任公司 超音速压缩机
US9909597B2 (en) 2013-10-15 2018-03-06 Dresser-Rand Company Supersonic compressor with separator
US20160281727A1 (en) * 2015-03-27 2016-09-29 Dresser-Rand Company Apparatus, system, and method for compressing a process fluid
CN110360130B (zh) * 2018-04-09 2022-12-27 开利公司 可变扩压器驱动系统
WO2024096946A2 (en) 2022-08-11 2024-05-10 Next Gen Compression Llc Variable geometry supersonic compressor

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Also Published As

Publication number Publication date
EP2715143B1 (en) 2021-03-10
KR20140024911A (ko) 2014-03-03
US20120301271A1 (en) 2012-11-29
AU2012262564A1 (en) 2013-12-12
CN103597213A (zh) 2014-02-19
WO2012166564A1 (en) 2012-12-06
CN103597213B (zh) 2016-02-17
CA2836303A1 (en) 2012-12-06
BR112013029742A2 (pt) 2018-04-24
EP2715143A1 (en) 2014-04-09
JP6078053B2 (ja) 2017-02-08
US8770929B2 (en) 2014-07-08
JP2014515455A (ja) 2014-06-30
MX2013013944A (es) 2014-01-23

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