Pressure relief fins for improved roll control of precision projectiles
AssigneeThe United States of America as represented by the Secretary of the Army
InventorsThomas Recchia, Yin Chen, Mitchell Stolk, David Hosier, Sarah Hunt
Life of this patent
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Abstract
Pressure relief holes are sized and positioned on each fin of a projectile to allow high pressure from one side of the fin due to canard and fin interaction to bleed to a low pressure area on the opposite side of the fin. The location of the pressure relief holes target pressure differences due to canard roll control downwash while not affecting pressure differences due to projectile attitude. The fin planform area remains small enough to meet packaging and fire requirements for this type of munition and large enough to aerodynamically stabilize the airframe thereby enabling a more robust pitch and yaw autopilot design.
Claims10
A projectile comprising:
- a canard set for controlling projectile flight;
- a fin having one or more pressure relief holes operable during an independent controlled flight phase of the projectile, each of the one or more pressure relief holes defined by the fin and extending from a top surface to a bottom surface and allowing high pressure due to canard and fin interaction during the independent controlled flight phase from one surface of the fin to transfer to a low pressure area on an opposing side of the fin while not affecting pressure differences due to projectile attitude.
A precision guided mortar projectile comprising:
- a body housing a payload and guidance electronics;
- a canard set extending radially from the body at a nose end of the projectile for controlling projectile flight;
- a plurality of fins extending radially from the body at a tail end, each of the fins having a circular first pressure relief hole and a circular second pressure relief hole, each of the first pressure relief hole and the second pressure relief hole operable during an independent controlled flight phase of the projectile and defined by the fin and extending from a top surface to a bottom surface and allowing high pressure due to canard and fin interaction during the independent controlled flight phase from one surface of the fin to transfer to a low pressure area on an opposing side of the fin while not affecting pressure differences due to projectile attitude and
- wherein the first pressure relief hole and the second pressure relief hole are positioned on a portion of the fin which is below a central lateral axis and at the proximate end of the fin and such that their centers are substantially aligned along a central longitudinal axis of the fin.
Dependencies are inferred from the claim text.