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Fire extinguishing apparatus having a slidable mass for a penetrator nozzleA fire extinguishing apparatus for delivering an extinguishing agent through a tarrier surrounding a structure into its interior includes an elongated tubular nozzle body which has a pointed penetrating head carried on one end of the tubular body. A source of extinguishing agent coupled to the opposite end of the tubular body is fed through and passes through passages adjacent the head for delivering the extinguishing agent to the interior of the structure. A slidable mass is carried on the tubular body on a remote end of the tubular body from the penetrating head. By manipulating the slidable mass and bringing such in contact with an abutment the force imparted to the tubular body causes the head to penetrate the structure.
Document ID
19810005625
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Gray, N. C.
(NASA John F. Kennedy Space Center Cocoa Beach, FL, United States)
Senseny, R. M.
(Boeing Aerospace Co. Seattle, Wash., United States)
Bolton, P. N.
(Boeing Aerospace Co. Seattle, Wash., United States)
Date Acquired
September 4, 2013
Publication Date
August 26, 1980
Subject Category
Engineering (General)
Report/Patent Number
Patent Number: US-PATENT-4,219,084
Patent Application Number: US-PATENT-APPL-SN-897840
Patent Number: NASA-CASE-KSC-11064-1
Accession Number
81N14137
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,219,084|NASA-CASE-KSC-11064-1
Patent Application
US-PATENT-APPL-SN-897840
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