Abstract An ornithopter aircraft which flys by flapping a wing. The wing is flapped by a constructively sympathetically forced dampened harmonic oscillation induced in a leading edge strut which preferable is a single flexible steel rod extending the length of the wing. The wing releases the air on its upward recovery stroke by means of flexible flaps which uncover holes in a structural flexible web forming the wing. On the downward power stroke of the wing, the flaps sealingly abut and occlude the holes of the web, forming a wing surface relatively impermeable to the passage of air. An inner section of the wing, on both sides of the aircraft, where relatively little flapping motion displacement occurs, has a flexible layer which permanently covers and seals the holes of the web. This area of the wing generates lift during both upward and downward motion of the wing, due to the forward motion of the ornithopter and due to the capture of pressurized air from the downstroke of the wing.
Inventors
👤 Kenneth R. Bowers, Jr.
Bibliographic Details
Application Number—
JurisdictionUS
Data Sourcegoogle_patents
Last Synchronized2026-11-03 00:28
CPC Classifications
B; B64; B64C; B64C33/00; B64C33/02
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
122 words
A method for flapping an ornithopter wing, said wing being herein defined as extending across and beyond both sides of said ornithopter fuselage thereby encompassing what is elsewhere considered two wings, said wing having an elongated strut extending substantially the entire length of said wing, which method comprises: a) seizing said strut by impelling means at a position approximately in the center of said strut, and b) sympathetically impelling in said strut extending on both sides of the ornithopter a harmonic oscillation by constructive movement of said impelling means, thereby c) flapping said wing with each end of said wing moving in phase with and with the amplitude of the opposite end, this being a characteristic of harmonic motion in said strut.
Claim 2
Independent Claim
122 words
A method for flapping an ornithopter wing, said wing being herein defined as extending across and beyond both sides of said ornithopter fuselage thereby encompassing what is elsewhere considered two wings, said wing having an elongated strut extending substantially the entire length of said wing, which method comprises: a) seizing said strut by impelling means at a position approximately in the center of said strut, and b) sympathetically impelling in said strut extending on both sides of the ornithopter a harmonic oscillation by constructive movement of said impelling means, thereby c) flapping said wing with each end of said wing moving in phase with and with the amplitude of the opposite end, this being a characteristic of harmonic motion in said strut.
Claim 3
Dependent Claim
16 words
The ornithopter of claim 1 wherein said strut is the leading edge member of said wing.
Claim 4
Dependent Claim
31 words
The ornithopter of claim 1 wherein said strut is seized at two locations by said means to induce in said strut a constructively sympathetically forced harmonic oscillation for flapping said wing.