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
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)
Publications (1)
Publication Number | Publication Date |
---|---|
NL80691C true NL80691C (xx) |
Family
ID=1828841
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NL80691D NL80691C (xx) |
Country Status (1)
Country | Link |
---|---|
NL (1) | NL80691C (xx) |
Cited By (1)
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 |
-
0
- NL NL80691D patent/NL80691C/xx active
Cited By (1)
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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