Rear aerodynamic fairing for an aircraft engine attachment device, comprising a heat shield capable of expanding freely

Rear aerodynamic fairing for an aircraft engine attachment device, comprising a heat shield capable of expanding freely

The fairing (30) has a main structure (60) extending along longitudinal direction (X) of the fairing and including two interconnected side panels (44). A heat protection floor is mounted on the main structure via a connecting unit. The connecting unit includes stainless steel strips (62) designed to...

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Bibliographische Detailangaben
1. Verfasser: JOURNADE, FRÉDÉRIC
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HELICOPTERS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The fairing (30) has a main structure (60) extending along longitudinal direction (X) of the fairing and including two interconnected side panels (44). A heat protection floor is mounted on the main structure via a connecting unit. The connecting unit includes stainless steel strips (62) designed to be deformable to accompany displacement of the heat protection floor relative to the main structure in case of differential thermal expansion between the heat protection floor and the main structure.