公开(公告)号：US20180149524A1

公开(公告)日：2018-05-31

申请号：US15824119

申请日：2017-11-28

Applicant: Airbus Operations SAS

Inventor： Yannick SOMMERER

IPC: G01K1/08 ,  G01K1/14 ,  G01K13/02 ,  F01D17/02

CPC classification number: G01K1/08 ,  F01D17/02 ,  F01D17/085 ,  F05D2260/80 ,  G01K1/14 ,  G01K1/20 ,  G01K13/02 ,  G01K2013/024

Abstract: A system for protecting a thermocouple placed in an environment comprising at least one radiative element, comprising a plate positioned between the thermocouple and the radiative element. The plate has an overall surface condition of an internal face facing towards the thermocouple such that the internal face absorbs radiation coming from the radiative element more than the internal face reflects the radiation.

公开(公告)号：US20210261267A1

公开(公告)日：2021-08-26

申请号：US17181585

申请日：2021-02-22

Applicant: Airbus Operations SAS

Inventor： Yannick SOMMERER ,  Maxime ZEBIAN

IPC: B64D33/02 ,  B64D33/04 ,  B64D31/06

Abstract: A propulsion assembly with a primary duct and a secondary duct, an outer fairing delimiting an outer compartment with an inlet opening, an inner fairing delimiting an inner compartment with an air exhaust aperture, a suction system having an inlet, an outlet and mobile elements that draw the air in via the inlet and deliver the air via the outlet, a drive that drives the mobile elements, a transfer pipe connected to the outlet, a distribution pipe disposed in the inner compartment, connected to the transfer pipe and having nozzles, a supply pipe that opens into the outer compartment and is connected to the inlet, and a regulator that regulates the flow rate of air in the suction system. The outside air is then driven by the suction system and passes through the two compartments in a forced manner.