Sikorsky Aircraft Corporation

Carl A Palmer

Cody Michael Ture

Joseph Lawrence Simonetti

Michael Peter Strauss

Mark Denton Bystry

Michael Joseph DeVita

Ronald Moffatt

Avinash Sarlashkar, Jr

Carl S Byington

Myra Torres

Michael J Moore

Maksim Bobrov

Jeremy W Sheaffer

Ryan Brewer

David Ortiz

Michael J Bluett

Craig D Reed

John R Farnach

A control system for an in-flight engine restart system of a rotorcraft includes an engine control unit that controls and detects status of an engine. The control system also includes a flight control computer that communicates with the engine control unit, an engine operation control system, and a pilot interface including pilot controls. The engine operation control system includes a processor that initiates a health check of the in-flight engine restart system to determine an in-flight engine restart system status. The engine operation control system processes engine mode of operation commands to establish an engine mode of operation, and delivers commands to aspects of the in-flight engine restart system including the engine control unit based on processing of the engine mode of operation commands. The engine operation control system reports the in-flight engine restart system status and results of the engine mode of operation commands to the flight control computer.

Control system for rotorcraft in-flight engine restarting

A corrosion management method is provided and includes storing an asset fleet at a location, generating a corrosion rate stressor by reference to models for any component of an asset of the asset fleet corresponding to the location and storage practice of the asset, predicting an accumulated corrosion stressor severity from the generated corrosion rate stressor, measuring an actual corrosion rate stressor at the location and revising the models in accordance with a difference between the predicted accumulated corrosion stressor severity and the measured actual corrosion rate stressor.

Method for predicting corrosion potential, monitoring contaminant load and optimizing corrosion maintenance

An integrated inspection system including at least one surface defining an enclosed space, at least one camera mounted in the enclosed space, and an interrogator device operatively coupled to the at least one camera. The interrogator device provides power to and receives images from the camera.

Wireless battery-less mini camera and system for interior inspection of closed spaces

A fluid condition monitoring device includes a sensing assembly including a sensor and a transducer, the sensor to sense a property of the fluid and the transducer to apply a test signal to the fluid and receive a return signal from the fluid; a control assembly coupled to the sensing assembly, the control assembly including a controller and an input/output interface, the controller interfacing with the transducer to generate fluid condition information in response to the return signal; and an interface assembly coupled to the control assembly, the interface assembly including a connection to the input/output interface to transmit the fluid condition information to an external system.

Fluid condition monitoring device

A system and method of detecting, quantifying, and characterizing corrosion and degradation of an article, includes receiving signals indicative of a stack of images of a surface of the article; determining depth and nature of features in the stack of images; generating a surface model of the article in response to the determination of the depth and the nature of features; determining features of interest from the surface model; comparing the features of interest with predetermined information on the article; and characterizing the article as corroded or degraded in response to the comparisons of the features of interest.

Apparatus for detecting corrosion in an article

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Pittsford, NY, United States of America

Carl A Palmer