NL80691C - - Google Patents

Info

Publication number
NL80691C
NL80691C NL80691DA NL80691C NL 80691 C NL80691 C NL 80691C NL 80691D A NL80691D A NL 80691DA NL 80691 C NL80691 C NL 80691C
Authority
NL
Netherlands
Application number
Publication of NL80691C publication Critical patent/NL80691C/xx

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
    • F04D19/002—Axial flow fans
    • F04D19/005—Axial flow fans reversible fans
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/548—Specially adapted for liquid pumps

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
NL80691D NL80691C (en)

Publications (1)

Publication Number Publication Date
NL80691C true NL80691C (en)

Family

ID=1828841

Family Applications (1)

Application Number Title Priority Date Filing Date
NL80691D NL80691C (en)

Country Status (1)

Country Link
NL (1) NL80691C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4585391A (en) * 1982-10-06 1986-04-29 Societe Nationale Industrielle Et Aerospatiale Tail rotor arrangement with increased thrust for rotary wing aircraft and device for increasing the thrust of such an arrangement

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4585391A (en) * 1982-10-06 1986-04-29 Societe Nationale Industrielle Et Aerospatiale Tail rotor arrangement with increased thrust for rotary wing aircraft and device for increasing the thrust of such an arrangement

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