Pneumatisches Servoventil mit Einstellbarer Antriebseinheit
Anmelder: Hamilton Sundstrand Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP3409989
- Aktenzeichen
- EP17461541
- Anmeldetag
- 31. Mai 2017
- Veröffentlichung
- 15. September 2021
- Erteilung
- 15. September 2021
- Rechtsraum
- EP
- IPC
- F16K41/12F02K1/00F16K11/07F16K27/04F16K31/06H01F7/13
Abstract
A servo valve for an actuator is described. The servo valve comprises a housing (4), a sleeve (12) provided within the housing comprising an axis (A) and having a plurality of metering holes (26, 28, 30, 32) for communication with a cavity (16) within. A metering rod (42) extends within the cavity for metering flow of pneumatic fluid through the metering holes. The metering rod is coupled to a drive unit (48) for axial movement within the cavity, the drive unit comprising a drive unit housing (50), a solenoid (68) and an adjustable core (54). The adjustable core comprises a threaded first portion (56) having a thread (59) and a second portion (58). The thread of the first portion engages a thread (51) extending through the drive unit housing for adjustment of the relative position of the adjustable core with respect to the solenoid. The drive unit can be calibrated by adjusting the relative position of the adjustable core to alter current/displacement characteristics of the drive unit.
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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