A flapping wing driving apparatus includes at least one crank gear capstan rotatably coupled to a crank gear, the at least one crank gear capstan disposed radially offset from a center of rotation of the crank gear; a first wing capstan coupled to a first wing, the first wing capstan having a first variable-radius drive pulley portion; and a first drive linking member configured to drive the first wing capstan, the first drive linking member windably coupled between the first variable-radius drive pulley portion and one of the at least one crank gear capstan; wherein the first wing capstan is configured to non-constantly, angularly rotate responsive to a constant angular rotation of the crank gear.

A flapping wing driving apparatus includes at least one crank gear capstan rotatably coupled to a crank gear, the at least one crank gear capstan disposed radially offset from a center of rotation of the crank gear; a first wing capstan coupled to a first wing, the first wing capstan having a first variable-radius drive pulley portion; and a first drive linking member configured to drive the first wing capstan, the first drive linking member windably coupled between the first variable-radius drive pulley portion and one of the at least one crank gear capstan; wherein the first wing capstan is configured to non-constantly, angularly rotate responsive to a constant angular rotation of the crank gear.

A reciprocating lift and thrust system include at least an airfoil and a reciprocating driver configured to produce a reciprocating motion of the airfoil. The system may further include a control unit to change or maintain a suitable angle of attack of the airfoil for lift or thrust as well as to facilitate the cyclic control of the flying vehicle driven by the reciprocating system. The lift and thrust system may be deployed in a module that includes at least two reciprocating airfoils (RAs) and is configured to substantially cancel out the inertia forces and moments associated with the individual airfoils. The reciprocating driver maybe, but not limited to, a mechanical, electromagnetic, electrical, or hydraulic driver. The embodiments of the subject invention provide novel and advantageous RA-driven aircraft, RA-driven flying motor vehicles, and RA-driven watercraft.

A reciprocating lift and thrust system include at least an airfoil and a reciprocating driver configured to produce a reciprocating motion of the airfoil. The system may further include a control unit to change or maintain a suitable angle of attack of the airfoil for lift or thrust as well as to facilitate the cyclic control of the flying vehicle driven by the reciprocating system. The lift and thrust system may be deployed in a module that includes at least two reciprocating airfoils (RAs) and is configured to substantially cancel out the inertia forces and moments associated with the individual airfoils. The reciprocating driver maybe, but not limited to, a mechanical, electromagnetic, electrical, or hydraulic driver. The embodiments of the subject invention provide novel and advantageous RA-driven aircraft, RA-driven flying motor vehicles, and RA-driven watercraft.

The disclosure relates to a biomimetic insect. The biomimetic insect includes a trunk and at least two wings connected to the trunk. The wing includes a carbon nanotube layer and a vanadium dioxide layer (VO.sub.2) layer stacked with each other. Because the drastic, reversible phase transition of vanadium dioxide, the wing has giant deformation amplitude and fast response.

The disclosure relates to a biomimetic insect. The biomimetic insect includes a trunk and at least two wings connected to the trunk. The wing includes a carbon nanotube layer and a vanadium dioxide layer (VO.sub.2) layer stacked with each other. Because the drastic, reversible phase transition of vanadium dioxide, the wing has giant deformation amplitude and fast response.

A flapping-wing aircraft includes a support frame, a motor coupled to the support frame, a pair of wings coupled to the support frame, and a linkage assembly coupled to the support frame and configured to translate an output torque of the motor into flapping motion of the wings, wherein the linkage assembly includes a first link coupled to a rotational output of the motor, a second link pivotably coupled to the first link at a first pivot joint, a third link pivotably coupled to the second link at a second pivot joint, and a fourth link pivotably coupled to the support frame and slidably coupled to the third link, and wherein the fourth link is coupled to a first wing of the pair of wings.

A flapping-wing aircraft includes a support frame, a motor coupled to the support frame, a pair of wings coupled to the support frame, and a linkage assembly coupled to the support frame and configured to translate an output torque of the motor into flapping motion of the wings, wherein the linkage assembly includes a first link coupled to a rotational output of the motor, a second link pivotably coupled to the first link at a first pivot joint, a third link pivotably coupled to the second link at a second pivot joint, and a fourth link pivotably coupled to the support frame and slidably coupled to the third link, and wherein the fourth link is coupled to a first wing of the pair of wings.

The present disclosure provides a flying water-ski device which enables a person to float in the air and fly in addition to gliding on the water in waterskiing. The flying water-ski device may be equipped with an airfoil having an outer form of a simplified triangle whose top faces toward the front. A flap section which has right and left flap axes may be placed at the back-end of said airfoil and right and left flaps, each of which can rotate around said right and left flap axes. A suspension support section may be suspended from said airfoil, and a harness section fixed to the suspension support section. A first tow rope may be coupled to the airfoil, and a second tow rope coupled to the harness section.

The present disclosure provides a flying water-ski device which enables a person to float in the air and fly in addition to gliding on the water in waterskiing. The flying water-ski device may be equipped with an airfoil having an outer form of a simplified triangle whose top faces toward the front. A flap section which has right and left flap axes may be placed at the back-end of said airfoil and right and left flaps, each of which can rotate around said right and left flap axes. A suspension support section may be suspended from said airfoil, and a harness section fixed to the suspension support section. A first tow rope may be coupled to the airfoil, and a second tow rope coupled to the harness section.