US 2003/0146341 A1 · Shock ( Wave) Absorber

Abstract

The Shock Wave Absorber is an inverted, rotated sinusoidal form inserted in the foremost tip of a vessel traveling in a fluid, with an opening to the nose, which provides orientation for turbulent air, water, etc . . .

Claims1

Dependent claims

A forced rotated sine wave perspective cavity for bending turbulent waves occurring at the tips of air/water craft, tuning the closed system fuselage with infinity producing an ultimate harmonic, for maximum efficiency.

Dependencies are inferred from the claim text.

Facts

Application

10/198,369Filed 18 Jul 2002

Priority

18 Jul 2001

Published

7 Aug 2003

Term ends

Not estimatedThe source records don’t support an estimate.

Classification6 codes

B64C 23/04
Influencing air flow over aircraft surfaces, not otherwise provided for: by generating shock waves
B63B 1/32
Hydrodynamic or hydrostatic features of hulls or of hydrofoils: other means for varying the inherent hydrodynamic characteristics of hulls
Y02T 70/10
Maritime or waterways transport: measures concerning design or construction of watercraft hulls
B64C
Aeroplanes

Shock ( Wave) Absorber

Life of this patent

Abstract

Claims1

Shock ( Wave) Absorber

Life of this patent

Abstract

Claims1