IP Library Granted Patent US 9,395,128
Granted Patent B2
US 9,395,128 · App. 13/853,313 · Granted Jul 19, 2016

Projectile launching devices and methods and apparatus using same

Inventors: Sean K. Treadway (Mooresville, NC); Andrew N. Lloyd (Mooresville, NC)
Assignee: Corvid Technologies, Inc.
F41A1/00F41F7/00F42B3/22F42D5/04
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Quick Facts
Patent No.
US 9,395,128
App. No.
13/853,313
Granted
Jul 19, 2016
Kind
B2
Abstract

A projectile launching device includes a reactive driver, a flyer housing, a flyer and a compressible buffer member. When detonated, the reactive driver will generate a detonation shock wave. The flyer housing defines a bore. The flyer is disposed in the bore and has a rear surface. The buffer member is interposed between the reactive driver and the flyer. The buffer member has a front surface in direct contact with the rear surface of the flyer. The buffer member is configured and arranged to: receive the detonation shock wave from the reactive driver; modify the detonation shock wave to generate a modified shock wave; and transmit the modified shock wave directly to the flyer to thereby propel the flyer away from the buffer member.

Claims (101)

1. A projectile launching device comprising:

a reactive driver containment structure;

a reactive driver contained in the reactive driver containment structure and that, when detonated, will generate a detonation shock wave;

a flyer housing defining a bore;

a disc-shaped flyer disposed in the bore, the flyer having a rear surface; and

a buffer member interposed between the reactive driver and the flyer, the buffer member having a front surface in direct contact with the rear surface of the flyer;

wherein the buffer member is configured and arranged to:

receive the detonation shock wave from the reactive driver;

modify the detonation shock wave to generate a modified shock wave; and

transmit the modified shock wave directly to the flyer to thereby propel the flyer away from the buffer member.

2. The projectile launching device of claim 1 wherein the shock impedance of the buffer member is less than the shock impedance of the flyer.

3. The projectile launching device of claim 1 wherein a section of the bore immediately surrounding the flyer has an inner diameter that forms an interference fit with an outer diameter of the flyer.

4. The projectile launching device of claim 1 wherein the buffer member extends into the bore of the flyer housing.

5. The projectile launching device of claim 4 wherein the buffer member extends into the reactive driver.

6. The projectile launching device of claim 1 wherein:

the flyer has a mass of at least about 0.05 grams; and

the projectile launching device is configured to propel the flyer at a velocity of at least about 2.0 kilometers/second.

7. The projectile launching device of claim 1 wherein:

the reactive driver containment structure circumferentially surrounds and is radially spaced apart from the buffer member; and

the reactive driver circumferentially surrounds the buffer member and fills a space between the reactive driver containment structure along the length of the buffer member.

8. The projectile launching device of claim 7 wherein:

the reactive driver containment structure extends fully from at least a location rearward of a rear end of the buffer member to the flyer housing; and

the reactive driver extends fully from at least a location rearward of the rear end of the buffer member to the flyer housing.

9. The projectile launching device of claim 1 wherein:

the flyer bore includes:

a main bore on a rear end of the flyer bore; and

a front bore on a front end of the flyer bore;

the flyer is disposed in the main bore; and

the inner diameter of the front bore is greater than the inner diameter of the main bore and the outer diameter of the flyer.

10. The projectile launching device of claim 9 wherein:

the main bore includes:

a buffer seat section; and

a flyer seat section;

the flyer is disposed in the flyer seat section; and

a front portion of the buffer member is disposed in the buffer seat section.

11. The projectile launching device of claim 9 wherein the front bore includes:

a muzzle section on a front end of the front bore; and

a tapered transition section interposed between the main bore and the muzzle section.

12. The projectile launching device of claim 1 wherein:

the shock impedance of the buffer member is less than the shock impedance of the flyer;

the front surface of the buffer member is substantially coextensive with the rear surface of the flyer;

a rear section of the buffer member is axially tapered and circumferentially surrounded by the reactive driver;

a total length of the buffer member is less than a maximum diameter of the buffer member;

the reactive driver containment structure circumferentially surrounds and is radially spaced apart from the buffer member;

the reactive driver circumferentially surrounds the buffer member and fills a space between the reactive driver containment structure along the length of the buffer member;

the reactive driver containment structure extends fully from at least a location rearward of a rear end of the buffer member to the flyer housing;

the reactive driver extends fully from at least a location rearward of the rear end of the buffer member to the flyer housing;

the flyer bore includes:

a main bore on a rear end of the flyer bore, the main bore including a buffer seat section and a flyer seat section; and

a front bore on a front end of the flyer bore;

the inner diameter of the front bore is greater than the inner diameter of the main bore and the outer diameter of the flyer;

the flyer is disposed in the flyer seat section; and

a front portion of the buffer member is disposed in the buffer seat section.

13. A projectile launching device comprising:

a reactive driver containment structure;

a reactive driver contained in the reactive driver containment structure and that, when detonated, will generate a detonation shock wave;

a flyer housing defining a bore;

a flyer disposed in the bore, the flyer having a rear surface; and

a buffer member interposed between the reactive driver and the flyer, the buffer member having a front surface in direct contact with the rear surface of the flyer;

wherein the buffer member is configured and arranged to:

receive the detonation shock wave from the reactive driver;

modify the detonation shock wave to generate a modified shock wave; and

transmit the modified shock wave directly to the flyer to thereby propel the flyer away from the buffer member; and

wherein the front surface of the buffer member is substantially coextensive with the rear surface of the flyer.

14. A projectile launching device comprising:

a reactive driver containment structure;

a reactive driver contained in the reactive driver containment structure and that, when detonated, will generate a detonation shock wave;

a flyer housing defining a bore;

a flyer disposed in the bore, the flyer having a rear surface; and

a buffer member interposed between the reactive driver and the flyer, the buffer member having a front surface in direct contact with the rear surface of the flyer, wherein a rear section of the buffer member is axially tapered and circumferentially surrounded by the reactive driver;

wherein the buffer member is configured and arranged to:

receive the detonation shock wave from the reactive driver;

modify the detonation shock wave to generate a modified shock wave; and

transmit the modified shock wave to the flyer to thereby propel the flyer away from the buffer member; and

wherein a total length of the buffer member is less than a maximum diameter of the buffer member.

15. The projectile launching device of claim 14 wherein the ratio of the total length of the buffer member to the maximum diameter of the buffer member is in the range of from about 4 to 20.

16. A projectile launching device comprising:

a reactive driver containment structure;

a reactive driver contained in the reactive driver containment structure and that, when detonated, will generate a detonation shock wave;

a flyer housing defining a bore;

a flyer disposed in the bore, the flyer having a rear surface; and

a buffer member interposed between the reactive driver and the flyer, the buffer member having a front surface in direct contact with the rear surface of the flyer;

wherein the buffer member is configured and arranged to:

receive the detonation shock wave from the reactive driver;

modify the detonation shock wave to generate a modified shock wave; and

transmit the modified shock wave directly to the flyer to thereby propel the flyer away from the buffer member; and

wherein:

the flyer bore includes:

a main bore on a rear end of the flyer bore; and

a front bore on a front end of the flyer bore;

the flyer is disposed in the main bore; and

the inner diameter of the front bore is greater than the inner diameter of the main bore and the outer diameter of the flyer.

17. The projectile launching device of claim 16 wherein:

the main bore includes:

a buffer seat section; and

a flyer seat section;

the flyer is disposed in the flyer seat section; and

a front portion of the buffer member is disposed in the buffer seat section.

18. The projectile launching device of claim 16 wherein the front bore includes:

a muzzle section on a front end of the front bore; and

a tapered transition section interposed between the main bore and the muzzle section.

Assignments (5)
RELEASE OF SECURITY INTEREST Recorded Jul 2, 2026
From: TRUIST BANK, AS ADMINISTRATIVE AGENT
To: CORVID TECHNOLOGIES, LLC
Reel/Frame 075163/0652 →
SECURITY INTEREST Recorded Jun 30, 2026
From: CORVID TECHNOLOGIES LLC
To: TRUIST BANK
Reel/Frame 075136/0352 →
SECURITY INTEREST Recorded Nov 13, 2025
From: CORVID TECHNOLOGIES, LLC
To: TRUIST BANK, AS ADMINISTRATIVE AGENT
Reel/Frame 072898/0012 →
NUNC PRO TUNC ASSIGNMENT Recorded Sep 16, 2015
From: CORVID TECHNOLOGIES, INC.
To: CORVID TECHNOLOGIES, LLC
Reel/Frame 036581/0717 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 29, 2013
From: TREADWAY, SEAN K.; LLOYD, ANDREW N.
To: CORVID TECHNOLOGIES, INC.
Reel/Frame 030114/0796 →
Continuity (3)
Provisional Application 61770076 · Feb 27, 2013
Provisional Application 61694681 · Aug 29, 2012
Related Publication 20140338554A1 · Nov 20, 2014