Aeronautics and astronautics – Aircraft structure – Fuselage and body construction
Patent
1992-05-21
1993-06-08
Peters, Jr., Joseph F.
Aeronautics and astronautics
Aircraft structure
Fuselage and body construction
244158R, 89 3602, B64D 700
Patent
active
052171850
ABSTRACT:
A hypervelocity projectile shield which includes a hollow semi-flexible housing fabricated from a plastic like, or otherwise transparent membrane which is filled with a fluid (gas or liquid). The housing has a inlet valve--similar to that on a tire or basketball, to introduce an ablating fluid into the housing. The housing is attached by a Velcro mount or double-sided adhesive tape to the outside surface of a structure to be protected. The housings are arrayed in a side-by-side relationship and may be in layers and in an over-lapping relationship for complete coverage of the surface to be protected. In use, when a hypervelocity projectile penetrates the outer wall of a housing it is broken up and then the projectile is ablated as it travels through the fluid, much like a meteorite "burns up" as it enters the earth's atmosphere, and the housing is deflated. The deflated housing can be easily spotted for replacement, even from a distance. Replacement is then accomplished by simply pulling a deflated housing off the structure and installing a new housing.
REFERENCES:
patent: 3649426 (1972-03-01), Gates, Jr.
patent: 3896758 (1975-07-01), Di Battista
patent: 4194431 (1980-03-01), Markus et al.
patent: 4925057 (1990-05-01), Childress et al.
patent: 4936528 (1990-06-01), Butner et al.
patent: 5067388 (1991-11-01), Crews et al.
Bidwell Anne E.
Fein Edward K.
Miller Guy M.
Peters Jr. Joseph F.
Schlorff Russell E.
LandOfFree
Ablative shielding for hypervelocity projectiles does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Ablative shielding for hypervelocity projectiles, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Ablative shielding for hypervelocity projectiles will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-1928869