RICHARD SCOTT KIRKENDALL
Pilots at Harmony Church Rd, Havre De Grace, MD

License number
Maryland A2574351
Issued Date
Feb 2017
Expiration Date
Aug 2017
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
3657 Harmony Church Rd, Havre De Grace, MD 21078

Professional information

Richard Kirkendall Photo 1

Pivot Ring For A Discarding Sabot

US Patent:
4450770, May 29, 1984
Filed:
Jan 31, 1983
Appl. No.:
6/462288
Inventors:
Richard D. Kirkendall - Havre de Grace MD
William H. Drysdale - Aberdeen MD
Louis D. Kokinakis - Fallston MD
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
F42B 1316
US Classification:
102523
Abstract:
The invention is an improved means for the efficient discard of multi-segt sabots. The invention consists of a ring-like mechanism that holds the aft end of the sabot segments in place around the projectile. The ring-like mechanism also serves to seal the interface between the sabot and the projectile. In operation, after the projectile and sabot exit from the muzzle of the launch device, the ring-like mechanism acts as a hinge device which causes the individual sabot segments to pivot about their aft extremity and finally discard as the pivot ring releases.


Richard Kirkendall Photo 2

Double Ramp Discarding Sabot

US Patent:
4372217, Feb 8, 1983
Filed:
May 12, 1980
Appl. No.:
6/148889
Inventors:
Richard D. Kirkendall - Havre de Grace MD
William H. Drysdale - Aberdeen MD
Louise D. Kokinakis - Fallston MD
Bruce P. Burns - Churchville MD
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
F42B 1316
US Classification:
102521
Abstract:
A segmented sabot utilizes a double ramp configuration and a centrally poioned obturating band in alignment with the center of gravity of an in-bore projectile to improve the uniformity of the shear traction forces at the interface between the sabot segments and a subcaliber projectile, to reduce propellant gas blow-by and to enhance projectile in-bore and trajectory stability. The increased uniformity of shear traction forces between sabot and projectile interfaces and propellant gas self-sealing design permits a reduction in sabot weight of sufficient magnitude to increase the velocity of the projectile at the muzzle exit.


Richard Kirkendall Photo 3

Solid Propellant-Carrying Caboted Projectile

US Patent:
4936220, Jun 26, 1990
Filed:
Jul 3, 1989
Appl. No.:
7/376090
Inventors:
Bruce P. Burns - Churchville MD
Richard D. Kirkendall - Havre de Grace MD
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
F42B 1408
US Classification:
102521
Abstract:
A saboted projectile having an elongated sub-projectile having a double-r sabot mounted thereon. The sabot includes a main body portion having a radially extending forward scoop and a central bulkhead between which a toroidal-shaped cavity is formed. A self-sealing container extending between the scoop and the bulkhead encloses the cavity in which a solid propellant is contained. A through-hole, formed in the bulkhead, extends from the cavity to the rear surface of the bulkhead. The through-hole has an opening at the rear of the bulkhead for housing a blow-out plug. An igniter is mounted in the plug for igniting the solid propellant contained in the cavity after a predetermined delay. Ignition may also be achieved via pores or openings in the container which may contain a deterred propellant.


Richard Kirkendall Photo 4

Double Ramp Discarding Sabot

US Patent:
4284008, Aug 18, 1981
Filed:
Apr 12, 1979
Appl. No.:
6/029188
Inventors:
Richard D. Kirkendall - Havre de Grace MD
William H. Drysdale - Aberdeen MD
Louise D. Kokinakis - Fallston MD
Bruce P. Burns - Harford County MD
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
F42B 1316
US Classification:
102521
Abstract:
A segmented sabot utilizes a double ramp configuration and a centrally poioned obturating band in alignment with the center of gravity of an in-bore projectile to improve the uniformity of the shear traction forces at the interface between the sabot segments and a subcaliber projectile, to reduce propellant gas blow-by and to enhance projectile in-bore and trajectory stability. The increased uniformity of shear traction forces between sabot and projectile interfaces and propellant gas self-sealing design permits a reduction in sabot weight of sufficient magnitude to increase the velocity of the projectile at the muzzle exit.


Richard Kirkendall Photo 5

Method Of Making Cast-In-Place Sabots

US Patent:
4360954, Nov 30, 1982
Filed:
Feb 17, 1981
Appl. No.:
6/235060
Inventors:
Bruce P. Burns - Churchville MD
Richard D. Kirkendall - Havre de Grace MD
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
B21K 2106, B22D 1900
US Classification:
29 123
Abstract:
The invention deals with the manufacture of fully segmented sabots used in he launching of subcaliber projectiles. The prior method required the machining of individual sabot segments and fitting them on to the sub-projectile. The improvement involves the casting of the sabot segments with the shimmed sub-projectile pre-positioned in a mold.