Abstract: Systems and methods for providing variable geometry winglets to an aircraft are disclosed. In one embodiment, a winglet includes a base portion configured to attach to a wing. The winglet further includes a body portion. In turn, the body portion includes at least one of a deflectable control surface, a shape memory alloy (SMA) bending plate, and a SMA torque tube. The base portion is configured to attach to the wing such that the body portion projects at an upward angle from the wing.

Abstract: Aircraft that have fuselages including a series of frames spaced apart according to a frame pitch. The series of frames are covered by an aircraft skin to define an interior volume of the aircraft. The interior volume contains a series of rows of seats separated according to a seat pitch. The seat pitch may be indexed to the frame pitch such that seats are located between adjacent ones of the series of frames to permit a reduced-perimeter aircraft fuselage with substantially equal passenger comfort metrics. In some embodiments, in addition, a series of windows are located adjacent outboard seats of the series of rows of seats to permit ergonomically appropriate viewing through the series of windows by passengers seated in the outboard seats.

Abstract: The invention provides an environmentally friendly renewable energy harvesting system for harvesting wind energy on a frozen surface, as in cold weather climatic regions associated with higher latitudes or higher altitudes, with snow or ice surfaces. A plurality of ski, skate or runner supported wings or sails are connected together to form a wind energy harvesting system, and capture wind energy by appropriate setting of wing or sail angles of attack so as to drive a cyclic motion that in turn can drive energy capture means such as electric generator means. The invention thus provides a wind energy harvesting system which is supported by a frozen surface, which includes fluid-foil means for interfacing with an air current such as a wind and which includes energy harvesting means utilizing periodic motion of the fluid-foil means for capturing wind energy and converting it into usable energy in a desired form such as electricity.

Abstract: An aircraft fuselage includes a tubular shell having a centerline axis, opposite ends, and a cross-section having a radius R(?), where ? is the angular coordinate of a cylindrical coordinate system, a curvature Curv(?), where Curv(?) is the inverse of a local radius of curvature of a surface of the shell, and a circumferential shape that varies radially by no more than ±7% from that of an elliptical cross-section at substantially every station along the centerline axis between the nose and tail ends thereof. The weight of the shell is minimized by “tailoring,” i.e., optimizing, at least one structural attribute, expressed as a function of ?, associated with every element of the shell, such that the weight of the shell required to react a design load incident thereon is less than that required to react the same design load, but wherein the same structural attribute has not been so tailored.

Abstract: The invention provides an environmentally friendly renewable energy harvesting system for harvesting wind energy on a frozen surface, as in cold weather climatic regions associated with higher latitudes or higher altitudes, with snow or ice surfaces. A plurality of ski, skate or runner supported wings or sails are connected together to form a wind energy harvesting system, and capture wind energy by appropriate setting of wing or sail angles of attack so as to drive a cyclic motion that in turn can drive energy capture means such as electric generator means. The invention thus provides a wind energy harvesting system which is supported by a frozen surface, which includes fluid-foil means for interfacing with an air current such as a wind and which includes energy harvesting means utilizing periodic motion of the fluid-foil means for capturing wind energy and converting it into usable energy in a desired form such as electricity.

Abstract: The invention provides a fluid-dynamic renewable energy harvesting system which includes fluid-foil means for interfacing with a fluid current such as a water current or wind or both, and which includes energy harvesting means utilizing fluid current driven periodic motion of the fluid-foil means for capturing fluid-dynamic renewable energy and converting it into usable energy in a desired form such as electricity. The invention provides devices, methods and systems for harvesting renewable energy for small-scale, medium-scale and large-scale applications, to provide real and substantial benefits towards efficiently fulfilling energy needs while also more broadly serving humanity and our global environment. The various embodiments of the invention provide energy with zero consumption of fossil fuels and zero emissions of greenhouse gases, and some selectively sited embodiments can beneficially counter global warming induced ice melting.

Abstract: Embodiments of the invention provide an aircraft configuration that provides for increased engine noise shielding for community noise reduction, while still providing desirable aerodynamic attributes such as good spanwise lift distributions and good structural integration without excessive wing surface area. Specifically, the aircraft is configured to have a longer-chord inboard wing portion and a shorter-chord outboard wing portion. The aircraft engines are positioned in major part over the longer-chord inboard wing portions such that communities below the wing are at least partially shielded by the inboard wing portion from the engine noise. Embodiments of the invention also strategically position fowler flaps or other chord-increasing devices in the region of the wing proximate the engine. Since the fowler motion increases the effective chord of the wing as the flaps are extended, the flaps may be deployed to increase the shielding characteristics of the wing.

Abstract: Systems and methods for providing variable geometry winglets to an aircraft are disclosed. In one embodiment, a winglet includes a base portion configured to attach to a wing. The winglet further includes a body portion. In turn, the body portion includes at least one of a deflectable control surface, a shape memory alloy (SMA) bending plate, and a SMA torque tube. The base portion is configured to attach to the wing such that the body portion projects at an upward angle from the wing.

Abstract: Aircraft that have fuselages including a series of frames spaced apart according to a frame pitch. The series of frames are covered by an aircraft skin to define an interior volume of the aircraft. The interior volume contains a series of rows of seats separated according to a seat pitch. The seat pitch may be indexed to the frame pitch such that seats are located between adjacent ones of the series of frames to permit a reduced-perimeter aircraft fuselage with substantially equal passenger comfort metrics. In some embodiments, in addition, a series of windows are located adjacent outboard seats of the series of rows of seats to permit ergonomically appropriate viewing through the series of windows by passengers seated in the outboard seats.

Abstract: The invention provides an innovative and practical new class of crossover motor vehicles for carrying passengers and for carrying cargo in a cargo or pickup bed, while still being of sufficiently small dimensions as to be garage-able in many home garages. Representative embodiments can carry 6 or 7 or 9 persons in comfortable seats all with adjacent or facing seats for companions; plus substantial varied cargos, which can potentially include sporting or recreational equipment such as bicycles or a powered waterscooter or snowmobile or motorcycle; camping gear including a 9-person tent; furniture such as a Queen bed set; appliances such as a washer and dryer; utility equipment such as a snowblower or riding lawnmower; or substantial quantities of items such as lumber, bark or fertilizer.

Abstract: The invention provides an innovative and practical new class of crossover motor vehicles for carrying passengers and for carrying cargo in a cargo or pickup bed, while still being of sufficiently small dimensions as to be garage-able in many home garages. Representative embodiments can carry 6 or 7 or 9 persons in comfortable seats all with adjacent or facing seats for companions; plus substantial varied cargos, which can potentially include sporting or recreational equipment such as bicycles or a powered waterscooter or snowmobile or motorcycle; camping gear including a 9-person tent; furniture such as a Queen bed set; appliances such as a washer and dryer; utility equipment such as a snowblower or riding lawnmower; or substantial quantities of items such as lumber, bark or fertilizer.

Abstract: This invention relates to recreational equipment for use on a sliding surface, such as skis, snowboards, or other equipment for use by a person such as a skier, snowboarder or water-skier. This invention provides a pogo-ski comprising a ski and a post thereon which is fitted with foot supports and a handhold suitable for use by a standing user.

Abstract: A seating and treadmill exercise device for passengers to exercise on an aircraft, capable of being displaced between stowed and deployed positions. While passengers board the aircraft, the seating and treadmill exercise device may be placed in the stowed position to allow passengers to freely move about the aircraft cabin. A folding seat is attached to the underside of the treadmill track, providing a seat for an airline attendant when the aircraft is taxiing and taking off, or landing. While the aircraft is in route, on long distance flights, the seating and treadmill exercise device may be placed in the deployed position so that passengers are able to exercise and stretch their legs, thus enhancing passenger well-being and health and helping to prevent maladies associated with long periods of sitting such as Deep Vein Thrombosis.

Abstract: A seating and treadmill exercise device for passengers to exercise on an aircraft, capable of being displaced between stowed and deployed positions. While passengers board the aircraft, the seating and treadmill exercise device may be placed in the stowed position to allow passengers to freely move about the aircraft cabin. A folding seat is attached to the underside of the treadmill track, providing a seat for an airline attendant when the aircraft is taxiing and taking off, or landing. While the aircraft is in route, on long distance flights, the seating and treadmill exercise device may be placed in the deployed position so that passengers are able to exercise and stretch their legs, thus enhancing passenger well-being and health and helping to prevent maladies associated with long periods of sitting such as Deep Vein Thrombosis.

Abstract: A fuselage for an airplane comprising a first side of the fuselage having a first curvature; and a second side of the fuselage having a second curvature; wherein the first curvature is different from the second curvature at a substantially vertical cross section of the fuselage. The invention can also be characterized as a cross section of an airplane comprising a first side of a fuselage with a first curvature; a second side of the fuselage with a second curvature that is coupled to the first side of the fuselage; a storage compartment within the fuselage; a seat within the fuselage; and an aisle within the fuselage; wherein the first curvature is different from the second curvature. The invention can reduce or eliminate sonic boom when applied to a supersonic airplane such as a supersonic business jet with a long slender fuselage.

Abstract: An automatic guidance and control system for aircraft moving on the ground. On-ground taxi control is provided in response to steering commands for nosewheel positioning.

Abstract: This invention relates to Recreational Vehicles (RVs) such as motorhomes, travel trailers, and fifth-wheel type camper trailers. The invention provides for a Recreational Vehicle configured with an integrated open-top cargo bed or pickup bed for carrying a wide variety of external loads, located in a portion of the aft end of the RV.

Abstract: Aircraft, such as tri-body aircraft, and associated methods of manufacture. In one embodiment, a tri-body aircraft has a fuselage with a forward portion extending at least partially forward of an aft-mounted main wing and first and second aft portions extending at least partially aft of the main wing. The forward fuselage portion and the first and second aft fuselage portions can include passenger cabins that are connected, allowing passengers to travel between the cabins during flight. In another embodiment, the aircraft includes a propulsion system having a first engine nacelle positioned at least proximate to the first aft fuselage portion, a second engine nacelle positioned at least proximate to the second aft fuselage portion, and a third engine nacelle positioned atop an inverted V-tail extending upwardly from the first and second engine nacelles.

Abstract: A less-than-200-seat-class passenger airplane includes a passenger cabin with two longitudinal aisles, and at least six economy class seats abreast the cabin. The cross-section of the cabin perpendicular to a longitudinal axis of the airplane fuselage has a horizontal diameter value in excess of a vertical diameter value.

Abstract: Transport aircraft, such as a transonic transport aircraft, having fuselages with multipurpose lower decks. In one embodiment, the fuselage is an “area-ruled” fuselage having a first fuselage portion, a second fuselage portion positioned aft of the first fuselage portion and at least proximate to a wing, and a third fuselage portion positioned aft of the second fuselage portion. The first fuselage portion can have a first dimension, the second fuselage portion can have a second dimension less than the first dimension, and the third fuselage portion can have a third dimension greater than the second dimension. The fuselage can further include an upper deck extending at least within the first and second fuselage portions, and a lower deck extending within the first fuselage portion. The upper deck can include a first passenger portion and the lower deck can include a second passenger portion, a cargo portion, or a second passenger portion and a cargo portion.