Daniel E Paxson

US Patent:

7763325, Jul 27, 2010

Filed:

Sep 28, 2007

Appl. No.:

11/864607

Inventors:

Daniel E. Paxson - Parma Heights OH, US

Assignee:

The United States of America as represented by the National Aeronautics and Space Administration - Washington DC

International Classification:

B05D 1/08
B05D 1/10
B05D 1/26
C23C 4/08
B05C 5/04

US Classification:

427449, 427455, 427456, 427225, 239 83

Abstract:

An apparatus and method for thermal spraying a metal coating on a substrate is accomplished with a modified pulsejet and optionally an ejector to assist in preventing oxidation. Metal such as Aluminum or Magnesium may be used. A pulsejet is first initiated by applying fuel, air, and a spark. Metal is inserted continuously in a high volume of metal into a combustion chamber of the pulsejet. The combustion is thereafter controlled resonantly at high frequency and the metal is heated to a molten state. The metal is then transported from the combustion chamber into a tail pipe of said pulsejet and is expelled therefrom at high velocity and deposited on a target substrate.

US Patent:

20110052825, Mar 3, 2011

Filed:

Jul 13, 2010

Appl. No.:

12/835345

Inventors:

Daniel E. Paxson - Parma Heights OH, US

International Classification:

B05D 1/02
B05B 7/18

US Classification:

427422, 118302, 118600

Abstract:

An apparatus and method for thermal spraying a metal coating on a substrate is accomplished with a modified pulsejet and optionally an ejector to assist in preventing oxidation. Metal such as Aluminum or Magnesium may be used. A pulsejet is first initiated by applying fuel, air, and a spark. Metal is inserted continuously in a high volume of metal into a combustion chamber of the pulsejet. The combustion is thereafter controlled resonantly at high frequency and the metal is heated to a molten state. The metal is then transported from the combustion chamber into a tailpipe of said pulsejet and is expelled therefrom at high velocity and deposited on a target substrate.

US Patent:

52973840, Mar 29, 1994

Filed:

Jul 6, 1993

Appl. No.:

8/086581

Inventors:

Daniel E. Paxson - Parma OH

Assignee:

The United States of America as represented by the Administrator of the
National Aeronautics & Space Administration - Washington DC

International Classification:

F02C 302

US Classification:

60 3902

Abstract:

A wave rotor system includes a wave rotor coupled to first and second end plates. Special ports are provided, one in each of the first and second end plates, to cancel expansion waves generated by the release of working fluid from the wave rotor. One of the expansion waves is reflected in the wave rotor from a reflecting portion, and provided to the special port in the second end plate. Fluid present at the special port in the second end plate has a stagnation pressure and mass flow which is substantially the same as that of the cells of the wave rotor communicating with such special port. This allows for cancellation of the expansion wave generated by the release of working fluid from the wave rotor. The special port in the second end plate has a first end corresponding substantially to the head of the expansion wave, and a second end corresponding substantially to the tail of the expansion wave. Also, the special port is configured to continually change along the circumference of the second end plate to affect expansion wave cancellation.

US Patent:

62000942, Mar 13, 2001

Filed:

Jun 18, 1999

Appl. No.:

9/350207

Inventors:

Gary J. Skoch - Chardon OH
Daniel E. Paxson - Parma Heights OH

Assignee:

The United States of America as represented by the Administrator of the
National Aeronautics and Space Administration - Washington DC

International Classification:

F04D 2944

US Classification:

4152082

Abstract:

A wave augmented diffuser for a centrifugal compressor surrounds the outlet of an impeller that rotates on a drive shaft having an axis of rotation. The impeller brings flow in in an axial direction and imparts kinetic energy to the flow discharging it in radial and tangential directions. The flow is discharged into a plurality of circumferentially disposed wave chambers. The wave chambers are periodically opened and closed by a rotary valve such that the flow through the diffuser is unsteady. The valve includes a plurality of valve openings that are periodically brought into and out of fluid communication with the wave chambers. When the wave chambers are closed, a reflected compression wave moves upstream towards the diffuser bringing the flow into the wave chamber to rest. This action recovers the kinetic energy from the flow and limits any boundary layer growth. The flow is then discharged in an axial direction through an opening in the valve plate when the valve plate is rotated to an open position.

US Patent:

52674320, Dec 7, 1993

Filed:

May 26, 1992

Appl. No.:

7/889003

Inventors:

Daniel E. Paxson - Parma Heights OH

Assignee:

The United States of America as represented by the Administrator of the
National Aeronautics & Space Administration - Washington DC

International Classification:

F02C 302

US Classification:

60 3945

Abstract:

A wave rotor system includes a wave rotor coupled to first and second end plates. Special ports are provided, one in each of the first and second end plates, to cancel expansion waves generated by the release of working fluid from the wave rotor. One of the expansion waves is reflected in the wave rotor from a reflecting portion, and provided to the special port in the second end plate. Fluid present at the special port in the second end plate has a stagnation pressure and mass flow which is substantially the same as that of the cells of the wave rotor communicating with such special port. This allows for cancellation of the expansion wave generated by the release of working fluid from the wave rotor. The special port in the second end plate has a first end corresponding substantially to the head of the expansion wave, and a second end corresponding substantially to the tail of the expansion wave. Also, the special port is configured to continually change along the circumference of the second end plate to affect expansion wave cancellation.

US Patent:

58947191, Apr 20, 1999

Filed:

Apr 18, 1997

Appl. No.:

8/846088

Inventors:

M. Razi Nalim - North Olmsted OH
Daniel E. Paxson - Parma Heights OH

Assignee:

The United States of America, as represented by the Administrator of the
National Aeronautics and Space Administration - Washington DC

International Classification:

F02C 302

US Classification:

60 3902

Abstract:

A method and apparatus for cold gas reinjection in through-flow and reverse-flow wave rotors having a plurality of channels formed around a periphery thereof. A first port injects a supply of cool air into the channels. A second port allows the supply of cool air to exit the channels and flow to a combustor. A third port injects a supply of hot gas from the combustor into the channels. A fourth port allows the supply of hot gas to exit the channels and flow to a turbine. A diverting port and a reinjection port are connected to the second and third ports, respectively. The diverting port diverts a portion of the cool air exiting through the second port as reinjection air. The diverting port is fluidly connected to the reinjection port which reinjects the reinjection air back into the channels. The reinjection air evacuates the channels of the hot gas resident therein and cools the channel walls, a pair of end walls of the rotor, ducts communicating with the rotor and subsequent downstream components. In a second embodiment, the second port receives all of the cool air exiting the channels and the diverting port diverts a portion of the cool air just prior to the cool air flowing to the combustor.