United Technologies Corporation

Raytheon Technologies Corporation

Heriberto Rodriguez

Christopher T Anglin

Carney R Anderson

Peter V Tomeo

James Cosby

Angel L Santiago

An assembly for a compartment of a gas turbine engine that includes a housing, a gear, and a baffle disposed about the gear. The baffle includes an upstream portion and a downstream portion. The upstream portion includes an upstream inner wall and an upstream outer wall separated from the gear. The upstream inner wall is positioned between the upstream outer wall and the gear. An upstream flow channel is formed between the upstream inner wall and the upstream outer wall. The downstream portion of the baffle includes a downstream inner wall and a downstream outer wall separated from the gear. The downstream inner wall is positioned between the downstream outer wall and the gear. A downstream flow channel is formed between the downstream outer wall and the downstream inner wall.

Secondary flow oil separator

A thrust-sensing assembly for a bearing compartment of a gas turbine engine includes a spacer and a retaining ring. The spacer includes an outer frusto-conical portion and an inner ring. The outer frusto-conical portion includes an axial row of a plurality of slots. Each slot of the plurality of slots includes a first rounded end, a second rounded end, a first side-face, and a second side face that faces the first side-face. The retaining ring includes a plurality of axial extensions with distal ends that are in contact with the outer frusto-conical portion of the spacer.

Strain measuring device for bearing compartment

A non-ferrous shaft includes multiple non-integral ferrous tooth components, thereby allowing a sensor to detect the shaft speed.

Growing community of inventors

Moca, PR, United States of America

Heriberto Rodriguez