Shock wave generator

• US 5,430,691 A
• Filed: 05/27/1994
• Issued: 07/04/1995
• Est. Priority Date: 05/27/1994
• Status: Expired due to Fees

• Current Assignee: Fridman, Igor
• Original Assignee: Fridman, Igor
• Inventors: Fridman, Igor
• Primary Examiner(s): ELDRED, JOHN W
• Application Number:
  US08/250,010
• Time in Patent Office: 403 Days
• Field of Search: 116/137 R, 116/137 A, 367/145, 367/147, 181/116, 181/117, 181/118
• US Class Current: 367/145
• CPC Class Codes: B08B 7/0007 by explosions
• CPC Class Codes: F23C 15/00 Apparatus in which combustion takes place in pulses influenced by acoustic resonance in a gas mass for generating combustion products of high pressure or high velocity F23R7/00; starting devices F23D11/42
• CPC Class Codes: F23M 9/06 in fire-boxes

Abstract

A two-phase shock wave generator including a combustion chamber including a first, combustion, portion having an input port and a second, detonation, portion downstream of the first portion and having an output aperture; an air-fuel supply line, operative to feed the input port with an air-fuel mixture, an igniter, associated with the air-fuel supply line, which ignites the air-fuel mixture in the supply line and initiates a burning front which propagates towards the input port and a turbulence stimulator, fixedly mounted in the combustion chamber, which enhances and controls burning of the air-fuel mixture and includes a first section, situated within the combustion portion of the combustion chamber and having a preselected first gas dynamic resistance and a second section, situated within the detonation portion of the combustion chamber and having a preselected second gas dynamic resistance, lower than the first resistance, wherein the first resistance is such that burning of the air-fuel mixture in the combustion portion yields a predetermined pressure level suitable for initiating detonation of the remaining air-fuel mixture, in the detonation portion, and wherein the second resistance supports continued detonation of the remaining air-fuel mixture in the detonation portion.

Claims

1. A two-phase shock wave generator comprising:

a combustion chamber including a first, combustion, portion having an input port and a second, detonation, portion downstream of said first portion and having an output aperture;

an air-fuel supply line, operative to feed said input port with an air-fuel mixture;

an igniter, associated with said air-fuel supply line, which ignites the air-fuel mixture in said supply line and initiates a burning front which propagates towards said input port; and

a turbulence stimulator, fixedly mounted in said combustion chamber, which enhances and controls burning of said air-fuel mixture and comprises;

a first section, situated within the combustion portion of the combustion chamber and having a preselected first gas dynamic resistance; and

a second section, situated within the detonation portion of the combustion chamber and having a preselected second gas dynamic resistance, lower than the first resistance,

wherein said first resistance is such that burning of the air-fuel mixture in said combustion portion yields a predetermined pressure level suitable for initiating detonation of the remaining air-fuel mixture, in said detonation portion, and wherein said second resistance supports continued detonation of the remaining air-fuel mixture in the detonation portion.

2. A shock wave generator according to claim 1 wherein said air-fuel supply line is associated with said input port via a perforated nozzle which scatters said burning front substantially upon entry of the burning front into said combustion chamber.

3. A shock wave generator according to claim 1 wherein said turbulence generator comprises a plurality of gas dynamic obstructers positioned at fixed locations along the combustion chamber to yield said preselected first and second gas dynamic resistances along said combustion and detonation portions, respectively.

4. A shock wave generator according to claim 2 wherein said turbulence generator comprises a plurality of gas dynamic obstructers positioned at fixed locations along the combustion chamber to yield said preselected first and second gas dynamic resistances along said combustion and detonation portions, respectively.

5. A generator according to claim 3 wherein each obstructer includes a plurality of rods, generally perpendicular to the direction of propagation of the burning front in said combustion chamber.

6. A generator according to claim 5 wherein said plurality of rods are arranged such that they define a generally helical path, having a predetermined pitch.

7. A shock wave generator comprising:

a combustion chamber having an input port and an output aperture;

an air-fuel supply line operative to feed the input port with an air-fuel mixture;

an igniter, associated with said air-fuel supply line, which ignites the air-fuel mixture in said supply line and initiates a burning front which propagates towards said input port;

a turbulence stimulator, fixedly mounted in said combustion chamber, which enhances and controls burning of said air-fuel mixture; and

a perforated nozzle, associated with said input port, which scatters said burning front substantially upon entry of the burning front into said combustion chamber.

8. A method of generating a shock wave using a two-phase burning process, comprising the steps of:

supplying an air fuel mixture from an air-fuel supply line to a combustion chamber;

igniting the air-fuel mixture in said supply line when said combustion chamber is filled with a preselected amount of air-fuel mixture, thereby initiating a burning front propagating towards said combustion chamber; and

enhancing and controlling the burning process by stimulating turbulence in said combustion chamber,

wherein the turbulence is stimulated by the steps of;

imposing a preselected first gas dynamic resistance in said combustion portion during a first, combustion, phase of said burning process; and

imposing a preselected second gas dynamic resistance, lower than the first gas dynamic resistance, during a second, detonation, phase of said burning process,

and wherein said first resistance is such that burning of the air-fuel mixture during said combustion phase yields a predetermined pressure level suitable for initiating detonation of the remaining air-fuel mixture, during said detonation phase, and wherein said second resistance ensures controlled detonation of the remaining air-fuel mixture.

9. A method according to claim 8 and further comprising the step of scattering the burning front substantially upon entry of the burning front into said combustion chamber.

11. A method according to claim 8 and further comprising the step of removing the detonated mixture at an aperture to form a gas dynamic pulse thereat.

12. A method according to claim 9 and further comprising the step of removing the detonated mixture at an aperture to form a gas dynamic pulse thereat.

10. A method of generating a shock wave comprising the steps of:

supplying an air fuel mixture from an air-fuel supply line to a combustion chamber;

igniting the air-fuel mixture in said supply line when said combustion chamber is filled with a preselected amount of air-fuel mixture, thereby initiating a burning front propagating towards said combustion chamber;

scattering the burning front upon entry of the burning front into said combustion chamber;

enhancing and controlling said burning process by stimulating turbulence in said combustion chamber; and

detonating the air fuel mixture in said combustion chamber.

13. A method according to claim 10 and further comprising the step of removing the detonated mixture at an aperture to form a gas dynamic pulse thereat.