Abstract: A smoke evacuation nozzle for an airplane having minimum diameter at the fuselage pressure hull exit for minimum structural integrity disruption. The nozzle is a converging-diverging nozzle which maintains sonic flow down to a very low altitude, thereby obtaining maximum airflow through it at all times. The throat is located at the point where the nozzle goes through the fuselage pressure hull so that the penetration through the fuselage pressure hull is minimal.
Type:
Grant
Filed:
August 9, 1990
Date of Patent:
May 17, 1994
Assignee:
The United States of America as represented by the Secretary of Transportation
Abstract: A sensing device and an analyis process which determines the shape of the periphery of a cross-section of a body as it deforms or is defomed in time. The sensing device is a band attached to the surface of the deformable body along the external peripheral path of the desired geometrical cross-section; the band has sensing devices on it, each of which produces an output proportional to local curvature as the band is deformed. The analysis process integrates the outputs from the sensing devices to calculate the shape of the periphery of a cross-section of the body to which the band is attached.
Type:
Grant
Filed:
December 22, 1989
Date of Patent:
August 27, 1991
Assignee:
The Government of the United States as represented by the Secretary of Transportation
Abstract: An asymmetric set of pre-swirl vanes (stators) and a specially matched propeller for use on an inclined shaft. The propulsor is designed by considering the mutual interaction of the propeller on the vanes and the vanes on the propeller. The propulsor unit provides the following:1. increased propulsive efficiency due to the reduced rotational (swirl) and axial kinetic energy losses in the propulsor's slipstream;2. reduction or elimination of propeller cavitation;3. reduction or elimination of unsteady propulsor forces as well as propulsor-induced hull vibrations.A unique feature of the present invention is that a prior art flat faced commercially available propeller can be modified to match the vane flow field for optimum propulsor performance. The use of commercially available propellers reduces the installation or hardware cost significantly and allows the propeller to be repaired easily if damaged.
Abstract: The invention encompasses a removable strain gauge fixture, and a method for measuring accumulated stress in a structural component, such as a railroad rail. The strain gauge fixture generally comprises first and second side pieces connected by a strain concentrating bar of reduced cross-section, an electronic strain sensor mounted on the bar, and first and second tapered pins extending from the front faces of each of the side pieces. The tapered pins transmit accumulated strain from the component being measured to the strain focusing bar when the pins are inserted into mating holes in the component.
Type:
Grant
Filed:
June 23, 1983
Date of Patent:
July 2, 1985
Assignee:
The United States of America as represented by the Secretary of Transportation
Inventors:
Harry Ceccon, Richard A. Murphy, H. David Reed, Oscar Orringer