Fairchild J44

Le compresseur

C’était un compresseur à  flux mixte, axiaux et centrifuges et à  aubes courbes. Il était construit d’une seule pièce coulée en alliage de magnésium qui ne nécessitait aucun usinage des pales.

Le diffuseur

Similaire au compresseur dans sa conception, la section de diffuseur, avec 3 rangées d’aubes de guidage, était usinée d’une seule pièce.

Combustion chamber

An annular combustion chamber was made from sheet metal and used commercialy available oil burners.

Turbin

The single stage turbine had its blades welded on to a forged steel disc. A simple, stock stainless steel tube, with a welded flange at each end, formed the rotor connecting the turbine to the compressor.

The was a bearing before the compressor and aft of the turbine and a fixed-area exhaust nozzle was used. 

In August 1948 the XJ44 made its first run.

The first flight was made in mid 1950 when it powered Fairchild’s Petrel Missile.

As service trial proceeded, so problems with J44 where thrown up, most of them attribuable to over-simplified production. A lot of changes were required, and development of J44 was completed by October 1954 under designation : J44-R-3.

The Improved engine was mounted on a Fairchild C-82 cargo aircraft, then later to each wingtips of the Fairchild C-123B cargo aircraft.

Another use of the J44 was one the experimental Bell model 65 VTOL Aircraft.

The main usage of the J44 was to power the Firebee drone, although, with a specific fuel consumption of 1,55 it could not compete with Continental’s J-69 (Licence version of Turbomeca’s Marbore) and it was taken out of production by 1959.