Flugzeugklimaanlagensteuerungssystem mit Ventildiagnose ohne Positionsrückkopplung
Anmelder: Hamilton Sundstrand Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP3543148
- Aktenzeichen
- EP19164324
- Anmeldetag
- 21. März 2019
- Veröffentlichung
- 20. Januar 2021
- Erteilung
- 20. Januar 2021
- Rechtsraum
- EP
- IPC
- B64F5/60B64D13/06
Abstract
An aircraft environmental control system (ECS) includes a first valve (110) that is adjustable between a plurality of first positions to open or shut-off a bleed air flow that flows from an inlet of the first valve to an outlet of the first valve. A second valve (116) includes an inlet in fluid communication with the first valve outlet, and is adjustable between a plurality of second positions to throttle the bleed air that flows from the inlet of the second valve to an outlet of the second valve. A valve position sensor (125) outputs a position signal indicating a measured position among the plurality of second positions. A controller (150) is in signal communication with the valve position sensor. The controller is configured to determine a primary effective area of the second valve based on the measured position, and to diagnose operation of the first valve based on the primary effective area.
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.
4.459 Patente in unserer Datenbank