Abstract: The disclosure of this specification illustrates and teaches the use of a self contained breathing apparatus for attachment to a user's back and incorporates a plurality of tanks having a manifold between them that is common to all with a single filling block leading thereto, and a reserve system mounted at one end thereof. The reserve system comprises a poppet valve which signals a loss in pressure by closing, after which it can then be actuated to open it for supplying the remaining portion of the reserve breathing gas through the manifold.The system also has a first and second stage regulator to provide regulated breathing gas to a user. The first stage regulator incorporates a dynamically balanced piston which is supported by an O-ring that is deformed through its cross section to provide movement to the valving piston.The entire system is encapsulated within a package or casing which can be opened along a parting line thereof and which is secured by over-center latches.
Abstract: The following specification teaches a drip controlling spout with a downwardly oriented opening. The rim of the upper leading edge projects below the rim of the under or trailing edge, so that liquid flowing through the spout will fall off the upper projecting rim avoiding drips down the neck of the spout.
Abstract: A jet drive boat propulsion unit cover for purposes of covering the fluid intake of a jet powered boat. The cover accommodates itself to the intake opening including the grillwork thereof, in a manner whereby it covers and seals the intake from foreign objects which might contaminate and adversely affect the wear and operation of the jet power unit, such as the impeller, bearing surface, and other wear areas. The cover is secured by means of an overcenter latching linkage having a member that moves eccentrically around an axis to cause a hook to engage the grating or grillwork of the opening so that it can be easily latched and unlatched. The foregoing provides a generally sealed relationship around the edges of the opening to prevent the migration of foreign matter into the jet drive unit.