Pneumatic nozzle

Nathenson , et al. April 27, 1

Patent Grant D408830

U.S. patent number D408,830 [Application Number D/068,056] was granted by the patent office on 1999-04-27 for pneumatic nozzle. This patent grant is currently assigned to Concept Engineering Group, Inc.. Invention is credited to Paul M. Brumbaugh, Richard D. Nathenson.


United States Patent D408,830
Nathenson ,   et al. April 27, 1999

Pneumatic nozzle

Claims

The ornamental design for a pneumatic nozzle, as shown.
Inventors: Nathenson; Richard D. (Pittsburgh, PA), Brumbaugh; Paul M. (Trafford, PA)
Assignee: Concept Engineering Group, Inc. (Verona, PA)
Appl. No.: D/068,056
Filed: March 20, 1997

Current U.S. Class: D15/21
Current International Class: 1504
Field of Search: ;D32/25,32,31,33-15,17 ;D23/223,200,213,225 ;239/589,601,532,590,592,594,DIG.7,DIG.8,DIG.22 ;D15/21,28,127,139 ;175/424,393 ;299/81.1,81.3,17

References Cited [Referenced By]

U.S. Patent Documents
D147125 July 1947 Harvuot
D269348 June 1983 Strohmaier
D269519 June 1983 Braun
D269520 June 1983 Braun
D275333 August 1984 Williams et al.
D308211 May 1990 Magnera
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D369648 May 1996 Fowler
D388914 January 1998 McKnight
D391349 February 1998 Chih
2175160 October 1939 Zobel et al.
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5782414 July 1998 Nathenson

Other References

Ascher H. Shapiro, "The Dynamics and Thermodynamics of Compressible Fluid Flow", Robert E. Krieger Publishing Company, vol. I and II, 1983, pp. 139, 141, 143 and 676-681, 694-695, 700-701. .
A. E. Puckett, "Supersonic Nozzle Design", Journal of Applied Mechanics, vol. 13, No. 4, Dec. 1946, pp. A-265-A-270. .
K. Foelsch, "The Analytical Design of an Axially Symmetric Laval Nozzle for a Parallel and Uniform Jet", Journal of the Aeronautical Sciences, Mar. 1949, pp. 161-166 and 185. .
G.V.R. Rao, "Approximation of Optimum Thrust Nozzle Contour", ARS Journal, vol. 30, No. 6, Jun. 1960, p. 561. .
Sinyarev and Doborovolskii, "Zhidkostne Raketne Drigateli", Moscow, 1957 (in Russian), pp. 366-367 and 370-371 and one page of translation. .
R.E. Wilson, "Turbulent Boundary Layer Growth with Favorable Static Pressure Gradient at Supersonic Speeds", Proceedings of the Second Midwestern Conference on Fluid Mechanics, The Ohio State University, 1952, pp. 277-289..

Primary Examiner: McInroy; Ruth
Attorney, Agent or Firm: Webb Ziesenheim Bruening Logsdon Orkin & Hanson, P.C.

Description



FIG. 1 is a top perspective view of a pneumatic nozzle showing our new design;

FIG. 2 is a top plan view thereof;

FIG. 3 is a left side elevational view thereof;

FIG. 4 is a front elevational view thereof;

FIG. 5 is a right side elevational view thereof;

FIG. 6 is a rear elevational view thereof; and,

FIG. 7 is a bottom plan view thereof.

* * * * *


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