Filteranordnung für ein Servoventil
Anmelder: Hamilton Sundstrand Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP4141263
- Aktenzeichen
- EP21461579
- Anmeldetag
- 25. August 2021
- Veröffentlichung
- 25. September 2024
- Erteilung
- 25. September 2024
- Rechtsraum
- EP
- IPC
- F15B13/043F15B21/041B01D36/00
Abstract
A filter assembly for a servo valve comprising: a first fluid nozzle (70') defining a first fluid passage therethrough between a first fluid inlet and a first fluid outlet; a second fluid nozzle (80') defining a second fluid passage therethrough between a second fluid inlet and a second fluid outlet; the first and second fluid nozzles arranged in end to end abutment with each other to form a tubular fluid nozzle unit in which the first and second fluid inlets are adjacent each other, and the first and second fluid passages align to form a common fluid passage through the tubular fluid nozzle unit, the first fluid outlet being at a first end of the tubular fluid nozzle unit and the second fluid passage being at a second, end of the tubular fluid nozzle unit; a recess (320) formed around an outer surface of the tubular fluid nozzle unit in a region where the first and second fluid inlets are located; and a perforated filter member (500) provided in the recess around the tubular fluid nozzle unit and across the first and second fluid inlets.
Anmelder
- Firma
- Hamilton Sundstrand Corporation
- Land
- 🇺🇸 USA
US-amerikanisches Unternehmen der Luft- und Raumfahrtindustrie, das Flugzeugsysteme wie Umweltkontroll-, Energie- und Antriebssysteme entwickelt; heute Teil von Collins Aerospace innerhalb von RTX.
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