Ornithopter aircraft
OwnerDongxiu Luinventor
Life of this patent
Estimating the term…
Abstract
An ornithopter aircraft has a main body. A first wing frame mount and a second wing frame mount are mounted to the main body. A first wing frame is rotably mounted to a first wing frame axle on the first wing frame mount. The first wing frame is configured to rotate relative to the main body and the rotation can be powered. The first wing frame feathers are rotably mounted to the first wing frame at first feather axles and the first wing frame feather rotation can be powered. The first wing frame feathers are configured to rotate relative to the first wing frame and the first wing frame feather rotation can be powered. A second wing frame is configured to be rotably mounted to a second wing frame axle on the second wing frame mount.
Claims12
An ornithopter aircraft comprising:
- a. a main body;
- b. a first wing frame mount and a second wing frame mount mounted to the main body;
- c. a first wing frame rotably mounted to a first wing frame axle on the first wing frame mount, wherein the first wing frame rotates relative to the main body wherein the first wing frame rotates continuously 360 degrees in only one direction on the first wing frame axle when in operation;
- d. first wing frame feathers rotably mounted to the first wing frame at first feather axles, wherein the first wing frame feathers rotate relative to the first wing frame, wherein the first wing frame feathers rotate continuously 360 degrees in only one direction on the first feather axles when in operation;
- e. a second wing frame rotably mounted to a second wing frame axle on the second wing frame mount, wherein the second wing frame rotates relative to the main body when in operation, wherein the second wing frame rotates continuously 360 degrees in only one direction on the second wing frame axle when in operation;
- and
- f. second wing frame feathers rotably mounted to the second wing frame at second feather axles, wherein the second wing frame feathers rotate relative to the second wing frame, wherein the second wing frame feathers rotate continuously 360 degrees in only one direction on the second feather axles when in operation.
An ornithopter aircraft comprising:
- a. a main body;
- b. a first wing frame mount and a second wing frame mount mounted to the main body;
- c. a first wing frame rotably mounted to a first wing frame axle on the first wing frame mount, wherein the first wing frame rotates relative to the main body;
- d. a first wing frame feather mounted to a first wing frame conveyor belt, wherein the first wing frame conveyor belt is mounted to the first wing frame, wherein the first wing frame feather rotates relative to the first wing frame along the first wing frame conveyor belt, wherein the first wing frame feather is formed as a rolling soft board of conveyor belt material;
- e. a second wing frame rotably mounted to a second wing frame axle on the second wing frame mount, wherein the second wing frame rotates relative to the main body;
- and
- f. a second wing frame feather mounted to a second wing frame conveyor belt, wherein the second wing frame conveyor belt is mounted to the second wing frame, wherein the second wing frame feathers rotate relative to the second wing frame along the second wing frame conveyor belt, wherein the second wing frame feather is formed as a rolling soft board of conveyor belt material.
An ornithopter aircraft comprising:
- a. a main body;
- b. a first wing frame mount and a second wing frame mount mounted to the main body;
- c. a first wing frame rail mounted to the first wing frame mount, and a second wing frame rail mounted to the second wing frame mount;
- d. a first wing frame slidingly mounted to the main body at the first wing frame rail, wherein the first wing frame moves up and down relative to the main body in linear reciprocation when in operation;
- e. first wing frame feathers rotably mounted to the first wing frame at first feather axles, wherein the first wing frame feathers rotate relative to the first wing frame;
- f. a second wing frame slidingly mounted to the main body at a second wing frame rail, wherein the second wing frame moves up and down relative to the main body in linear reciprocation when in operation;
- and
- g. second wing frame feathers rotably mounted to the second wing frame at second feather axles, wherein the second wing frame feathers rotate relative to the second wing frame.
Dependencies are inferred from the claim text.