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Controlled overspray spray nozzleA spray system for a multi-ingredient ablative material wherein a nozzle A is utilized for suppressing overspray is described. The nozzle includes a cyclindrical inlet which converges to a restricted throat. A curved juncture between the cylindrical inlet and the convergent portion affords unrestricted and uninterrupted flow of the ablative material. A divergent bell-shaped chamber and adjustable nozzle exit B is utilized which provides a highly effective spray pattern in suppressing overspray to an acceptable level and producing a homogeneous jet of material that adheres well to the substrate.
Document ID
19820005503
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Prasthofer, W. P.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
November 17, 1981
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
Patent Number: US-PATENT-4,300,723
Patent Application Number: US-PATENT-APPL-SN-126138
Patent Number: NASA-CASE-MFS-25139-1
Accession Number
82N13376
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,300,723|NASA-CASE-MFS-25139-1
Patent Application
US-PATENT-APPL-SN-126138
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