Joseph A Simonetti

US Patent:

20080156584, Jul 3, 2008

Filed:

Dec 29, 2006

Appl. No.:

11/617864

Inventors:

Joseph Anthony Simonetti - Bellingham MA, US

International Classification:

E06C 7/42

US Classification:

182107

Abstract:

A ladder stabilizer comprises a central section and two side sections extending in substantially the direction from opposed ends of the central section. When the stabilizer is placed with the free ends of the side sections in contact with a vertical wall of a building and the side sections and the central section lying substantially in a horizontal plane, the central section provides a substantially planar surface facing away from the vertical wall and lying at an angle of from about 12 to about 23 degrees, and desirably about 17.5 degrees, to the vertical. This enables the side sections to extend horizontally even when the ladder is used at its normal inclination to the vertical.

US Patent:

20180201386, Jul 19, 2018

Filed:

Jul 20, 2016

Appl. No.:

15/744422

Inventors:

- Stratford CT, US
Michael Joseph DeVita - Cos Cob CT, US
Joseph Lawrence Simonetti - Southbury CT, US
Carl A. Palmer - Pittsford NY, US

International Classification:

B64D 31/06
B64C 27/12
F02C 7/262
B64D 45/00
B64D 27/14

Abstract:

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.