AIRCRAFT ICE PROTECTION SYSTEM AND AIRCRAFT PROVIDED WITH SAME

An aircraft ice protection system (A) is provided for preventing ice accretion on a wing (2) of an aircraft or removing the accreted ice. Bleed air (S2) extracted from a main engine (3) of the aircraft and air (S1') introduced from an air intake (31) installed on an airframe (28) and heated by...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	ISHIGURO Tatsuo, SAITO Isao, ATSUMI Motohiro, NAKANISHI Masakazu, TAKASU Toru, KAMOGARI Minoru, ABE Shigeki, TANAKA Hideaki
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINE PLANTS IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PARACHUTES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	An aircraft ice protection system (A) is provided for preventing ice accretion on a wing (2) of an aircraft or removing the accreted ice. Bleed air (S2) extracted from a main engine (3) of the aircraft and air (S1') introduced from an air intake (31) installed on an airframe (28) and heated by a heat source (26) of the airframe of the aircraft are selectively supplied to a hot air chamber (32) formed inside the wing (2), thereby carrying out ice protection.