HEATING INSTALLATION FOR AN AIRCRAFT COMPRISING A DIHYDROGEN TANK, AN ENGINE AND DIHYDROGEN-HEATING SYSTEMS

The invention relates to a heating installation (150) for an aircraft, the installation being arranged between a dihydrogen tank (104) and an engine (108) with a first supply pipe (152a) connected to the tank (104) and a second supply pipe (152b) connected to the engine (108) and comprising two bran...

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Bibliographic Details
Main Authors BELLEVILLE, Mathieu, KLEINERMANN, Cédric, MABILLE DE LA PAUMELIERE, Louis Vianney, MARTIN, Pierre-Olivier, PARMENTIER, Nicolas Claude, BRICHLER, Thierry, MENAGER, Simon
Format Patent
LanguageEnglish
French
Published 27.06.2024
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
WEAPONS
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Summary:The invention relates to a heating installation (150) for an aircraft, the installation being arranged between a dihydrogen tank (104) and an engine (108) with a first supply pipe (152a) connected to the tank (104) and a second supply pipe (152b) connected to the engine (108) and comprising two branch pipes (154a-b) connected in parallel between the first supply pipe (152a) and the second supply pipe (152b), wherein a first valve (156a-b), a heating system (158a-b) and a second valve (160a-b) are mounted, in series, from upstream to downstream, on each branch pipe (154a-b) . L'invention concerne une installation de réchauffement (150) pour aéronef disposée entre un réservoir (104) de dihydrogène et un moteur (108) avec une première canalisation d'apport (152a) connectée au réservoir (104) et une deuxième canalisation d'apport (152b) connectée au moteur (108) et comportant deux canalisations de dérivation (154a-b) connectées en parallèle entre la première canalisation d'apport (152a) et la deuxième canalisation d'apport (152b) où sur chaque canalisation de dérivation (154a-b) sont montés en série de l'amont vers l'aval, une première vanne (156a-b), un système de réchauffement (158a-b) et une deuxième vanne (160a-b).
Bibliography:Application Number: WO2023EP87061