US157527A - Improvement in expanding nozzles for hose - Google Patents

Improvement in expanding nozzles for hose Download PDF

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Publication number
US157527A
US157527A US157527DA US157527A US 157527 A US157527 A US 157527A US 157527D A US157527D A US 157527DA US 157527 A US157527 A US 157527A
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hose
improvement
expanding
lining
expanding nozzles
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B1/00Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means
    • B05B1/30Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to control volume of flow, e.g. with adjustable passages
    • B05B1/32Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to control volume of flow, e.g. with adjustable passages in which a valve member forms part of the outlet opening

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  • a patent which has recently been allowed me describes a series of expanding staves, hinged at one end to the end of a fixed tube or nozzle, and caused to overlap more or less upon eachother by suitable means, as the nozzle is desired to be expanded or contracted. It also describes a lining of thin sheet metal, in four or other convenient number of pieces, adapted to be pressed outward by the force of the issuing jet, and to form a smooth lining material for what would otherwise be the ridged edges of the staves.
  • Figure l is a vertical section
  • Fig. 2 is an end view
  • Fig. 3 is a section of a portion on a larger scale.
  • A is the fixed tube, which forms the foundation for my peculiar construction.
  • A is the stout outer thread thereon, which secures it within the ordinary butt, (not represented.)
  • B are the staves.
  • G are the thin sheet-metal lining pieces before referred to.
  • M is a tapering tube of soft vulcanized rubbermolded or otherwise produced, with the interior formed as smooth as the skill of workers in this material can attain. 'The elasticity of the material allows the small end to be contracted into less than its diameter as the staves are compressed together, and allows it to be expanded tomore than its normal diameter by the stream of water when the parts are properly conditioned therefor.
  • a shoulder, ct is formed in the inte-rior of the portion A, preferably by means of aring riveted in to confine the sheet metal D, and a ring, m, is pressed down upon this so as to apply within the rubber M, and to force it outward against the interior of A,
  • Thisring may be without threads. It may be armed with small points or Toughened like a file on its exterior surface to aid in holding the rubber more firmly, but my experiments indicate no necessity for such nicety. I believe it will hold the rubber with perfect firmness Without even rougliening or cementing. It is pressed down by a follower-rin g, m ,which is formed with a fine screw-thread on its exterior, which engageswith a corresponding screw-thread in the interior of the part A.

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Description

w,` LEYGGETT. Expanding-Nozzles for Hose.
Patented Dec. 8,1874.
l \\\\\\\\\\\\\\\\\\\\\\\\\\\\ll A.
nu 01X or:
NITED STATES PATENT OFFICE.
WILLIAM LEGGETT, OF NEW YORK, N. Y.
IMPROVEMENT IN EXPANDING NOZZLES FOR HOS-E.
Specification forming part of Letters Patent No. 157,527, dated December 8, 1874; application filed September 30, 1874.
To all whom it may concern.'
Be it known that I, WILLIAM LEGGETT, of New York city, in the State of New York, have invented certain Improvements in Expanding Nozzles for Hose, of which the following is a specification:
A patent which has recently been allowed me describes a series of expanding staves, hinged at one end to the end of a fixed tube or nozzle, and caused to overlap more or less upon eachother by suitable means, as the nozzle is desired to be expanded or contracted. It also describes a lining of thin sheet metal, in four or other convenient number of pieces, adapted to be pressed outward by the force of the issuing jet, and to form a smooth lining material for what would otherwise be the ridged edges of the staves.
. I have discovered, by my experiments therewith, that water is liable to leak laterally outward through the joints, even when thus guarded by the overlapping thin lining. The loss of tbe water is not `of importance, but the annoyance to the operator, in consequence of water trickling down on the nozzle, is considerable under ordinary conditions, and in intense freezing weather may become serious. My present invention provides for stopping all this lateral escape. Y
I have devised a continuous lining of rubber, with ecient means for holding it firmly in place at or near the hinged ends of the staves. This lining is pressed outward by the force of the water against the inner surface' of the thin sheet-metal lining previously hdescribed. The rubbershould be glazed or made as smooth as possible, and its outer end should coincide or be fiush with the outerends ofthe lining metal.
The following is a description of what I consider the best means of carrying out the invention. The accompanyin gdrawin gs form a part of this specification.
Figure l is a vertical section, and Fig. 2 is an end view. Fig. 3 is a section of a portion on a larger scale.
Similar letters of reference indicate corresponding parts in both figures.
A is the fixed tube, which forms the foundation for my peculiar construction. A is the stout outer thread thereon, which secures it within the ordinary butt, (not represented.) B are the staves. Dis a movable ring, moved outward and inward by any suitable means which controls the position of the bars B. G are the thin sheet-metal lining pieces before referred to. M is a tapering tube of soft vulcanized rubbermolded or otherwise produced, with the interior formed as smooth as the skill of workers in this material can attain. 'The elasticity of the material allows the small end to be contracted into less than its diameter as the staves are compressed together, and allows it to be expanded tomore than its normal diameter by the stream of water when the parts are properly conditioned therefor. The rubber M is held at the large end by the following means: A shoulder, ct, is formed in the inte-rior of the portion A, preferably by means of aring riveted in to confine the sheet metal D, and a ring, m, is pressed down upon this so as to apply within the rubber M, and to force it outward against the interior of A,
Aand also'endwise against the shoulder a.
Thisring may be without threads. It may be armed with small points or Toughened like a file on its exterior surface to aid in holding the rubber more firmly, but my experiments indicate no necessity for such nicety. I believe it will hold the rubber with perfect firmness Without even rougliening or cementing. It is pressed down by a follower-rin g, m ,which is formed with a fine screw-thread on its exterior, which engageswith a corresponding screw-thread in the interior of the part A.
I claim as my invention- The elastic liningpiece M, secured within the expanding nozzle B D G, and serving, in combination therewith, to prevent any leakage through the same, substantially as and for the purposes herein specified.
In testimony whereof I have hereunto set my hand this 26th day of September, 1874, in the presence of two subscribing witnesses.
WILLIAM LEGGETT. Witnesses: Y
W. C. DEY, E. VOLKMANN.
US157527D Improvement in expanding nozzles for hose Expired - Lifetime US157527A (en)

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2569996A (en) * 1945-08-20 1951-10-02 Kollsman Paul Self-adjusting reaction nozzle
US2682147A (en) * 1951-06-16 1954-06-29 Rohr Aircraft Corp Adjustable nozzle for exhaust gas
US2813395A (en) * 1951-06-29 1957-11-19 United Aircraft Corp Flap type variable area thrust nozzle having an actuating mechanism including a movable duct
US2865165A (en) * 1950-03-17 1958-12-23 Solar Aircraft Co Variable nozzle for jet engine
US20050258275A1 (en) * 2004-05-07 2005-11-24 Jeffrey Marc Williams Adjustable solid-flow nozzle and method
US20130341432A1 (en) * 2005-01-14 2013-12-26 Elkhart Brass Manufacturing Company, Inc. Adjustable smooth bore nozzle
US8882002B2 (en) 2001-11-29 2014-11-11 Watershield Llc Adjustable smooth bore nozzle
US9138754B2 (en) 2012-03-27 2015-09-22 Task Force Tips, Incorporated Adjustable firefighting nozzle

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2569996A (en) * 1945-08-20 1951-10-02 Kollsman Paul Self-adjusting reaction nozzle
US2865165A (en) * 1950-03-17 1958-12-23 Solar Aircraft Co Variable nozzle for jet engine
US2682147A (en) * 1951-06-16 1954-06-29 Rohr Aircraft Corp Adjustable nozzle for exhaust gas
US2813395A (en) * 1951-06-29 1957-11-19 United Aircraft Corp Flap type variable area thrust nozzle having an actuating mechanism including a movable duct
US8882002B2 (en) 2001-11-29 2014-11-11 Watershield Llc Adjustable smooth bore nozzle
US9259746B2 (en) 2001-11-29 2016-02-16 Watershield Llc Adjustable smooth bore nozzle
US20050258275A1 (en) * 2004-05-07 2005-11-24 Jeffrey Marc Williams Adjustable solid-flow nozzle and method
US7445166B2 (en) * 2004-05-07 2008-11-04 Jeffrey Marc Williams Adjustable solid-flow nozzle and method
US20130341432A1 (en) * 2005-01-14 2013-12-26 Elkhart Brass Manufacturing Company, Inc. Adjustable smooth bore nozzle
US9010664B2 (en) * 2005-01-14 2015-04-21 Elkhart Brass Manufacturing Company, Inc. Adjustable smooth bore nozzle
US20090050707A1 (en) * 2005-05-06 2009-02-26 Jeffrey Marc Williams Adjustable solid-flow nozzle and method
US9138754B2 (en) 2012-03-27 2015-09-22 Task Force Tips, Incorporated Adjustable firefighting nozzle

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