SYSTEM OF EMERGENCY RESCUE OF AIRCRAFT

The system of emergency rescue of aircraft contains a rescue parachute device for smooth descent of the aircraft in emergency situation and a device of limitation of impact loads on it at landing. Rescue parachute device is made of two parachutes, one of which is connected by a halyard with the forw...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: CHORNYI ANATOLII PETROVYCH, CAZACHEVICI ANDREI VEACESLAV, CAZACEVICI ALINA VEACESLAV
Format: Patent
Sprache:eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:The system of emergency rescue of aircraft contains a rescue parachute device for smooth descent of the aircraft in emergency situation and a device of limitation of impact loads on it at landing. Rescue parachute device is made of two parachutes, one of which is connected by a halyard with the forward section of the aircraft, and other - with the rear section and which in value corresponds to thetorque, acting on these parts relative to the center of gravity of the aircraft. The device of limitation of impact loads at landing of aircraft is located from below the fuselage.