AIRCRAFT BLEED SYSTEM
AIRCRAFT BLEED SYSTEM
- Neue Suche nach: PAPA FEDERICO
- Neue Suche nach: FARNUM BRADLEY C
- Neue Suche nach: KOPP-VAUGHAN KRISTIN
- Neue Suche nach: ROE NATHAN
- Neue Suche nach: PAPA FEDERICO
- Neue Suche nach: FARNUM BRADLEY C
- Neue Suche nach: KOPP-VAUGHAN KRISTIN
- Neue Suche nach: ROE NATHAN
A method of controlling an aircraft bleed may include the steps of monitoring (302) a temperature of a precooled airflow (140) exiting a precooler (106), and determining (304) a status of a wing anti-ice system (102) of an aircraft. The wing anti-ice system (102) may be configured to receive the precooled airflow (140) from the precooler (106). The method may further comprise the steps of determining (306) whether an engine operating condition of the aircraft is within an icing envelope (200), selecting (308) a temperature set point for the precooled airflow based on the status of the wing anti-ice system (102) and whether the aircraft is within an icing envelope (200), and modulating (310) a fan airflow from a fan (42) to the precooler (106) to adjust the temperature of the precooled airflow to the temperature set point.
Dokumentinformationen
AIRCRAFT BLEED SYSTEM
FLUGZEUGZAPFSYSTEM
SYSTÈME DE PURGE D'AÉRONEF
2019-06-19
Patent
Elektronische Ressource
Englisch
Ähnliche Titel
Aircraft bleed system and method of controlling an aircraft bleed system
| Europäisches Patentamt | 2015
Aircraft Bleed Air Leaf Detection System
British Library Online Contents | 1993
Synthesized low-pressure bleed air scheme for aircraft bleed air network
| Europäisches Patentamt | 2021