A walker device ( ) includes a frame assembly ( ), which supports the user during operation and carries the other assemblies discussed below. Left and right front wheel assemblies ( ) include a pivoting fork supporting a wheel, thereby allowing directional control over the walker during use. Left and right rear wheel assemblies ( ) are fixed-direction. A brake assembly ( ) allows the user to apply a frictional brake element to the both rear wheels, and prevents unwanted movement by the walker. A support sling assembly ( ) carries some or all of the users weight. Left and right lift cylinder assemblies ( ), ( ) lift and lower the support sling assembly to the desired elevation during use. A compressed air assembly ( ) provides power to the lift cylinder assemblies. A valve assembly ( ) provides independent control over both lift cylinder assemblies, to provide extra help to one side, if needed.
A wheelchair access system includes a wheelchair having a frame, rear wheels, front wheels, a seat, and a backrest. An extension extending rearwardly of the wheelchair frame includes a bracket coupled to an adjacent rear wheel, which allows the rear wheel to be moved horizontally away from the side of the wheelchair seat. A platform, coupled to a slide bracket attached to the wheelchair, can be positioned to the side of the wheelchair to facilitate access into and out of the wheelchair. The wheelchair access system is designed so that the physically impaired can access the wheelchair without the assistance of another person.
An apparatus and method for defueling and aircraft. The apparatus includes a vacuum fuel tank comprising a first vacuum generator, a defueling hose in fluid communication with the vacuum fuel tank, a first defueling fitting attached to the first defueling hose, and a second vacuum generator operatively connected to the first defueling fitting. By providing both a first and a second vacuum generator, the defueling fitting can be attached and detached from an aircraft independent of the suction used to withdraw fuel from an aircraft. According to some embodiments, there may be multiple defueling hoses and additional vacuum generators. Further, some embodiments include a telescoping funnel that can be selectively isolated from the vacuum fuel tank so that the tank can be held at vacuum pressure.
A method and apparatus for defueling an aircraft. The apparatus includes a defueling fitting comprising one or more structural connectors, which may include one or more suction cups. The one or more structural members are attached to a mount. The mount may be of any shape, including generally straight, angled, polygonal, or circular. An actuator assembly is attached to the mount for opening an aircraft defueling valve. The first and second suction cups are operatively connected to a vacuum source to connect the defueling fitting to an aircraft body, with the actuator assembly positioned at the aircraft defueling valve. The defueling fitting facilitates safe and convenient defueling of certain aircraft that have recessed or covered fuel drain valves. For example, the Boeing C-17 has fuel drain valves that are recessed behind doors, heretofore presenting a great obstacle to appropriate defueling. The defueling fitting described herein may be used in small and tight spaces, even when other conventional defueling fittings are not helpful.
A method and apparatus for defueling an aircraft. The apparatus includes a defueling fitting comprising one or more structural connectors, which may include one or more suction cups. The suction cups are disposed in a mount. The suction cups may be raised from a surface in the mount and arranged in a non-circular pattern to facilitate connection to contoured surfaces. An actuator assembly may be attached to the mount for opening an aircraft defueling valve. The suction cups may be operatively connected to a vacuum source to connect the defueling fitting to an aircraft body, with the actuator assembly positioned at the aircraft defueling valve. The defueling fitting facilitates safe and convenient defueling of aircraft, even aircraft with significantly contoured surfaces.
The present invention provides methods and apparatus for containing aircraft fuel. According to some embodiments the apparatus includes a structural connector comprising an open shape, a first surface and a second surface, a seal defining a suction area disposed in the first surface, and a boot extending from the structural connector. The boot may comprise a lateral opening. The boot includes first and second ends, such that the first end of the boot may be attached to the structural connector and the second end may be spaced from the structural member. According to some embodiments the second end comprises a center offset laterally from the center of the structural connector.
A portable bath apparatus includes an enclosure formed by a bottom wall, first upstanding wall portions, and second upstanding wall portions. The first upstanding wall portions are stationary relative to the portable bath apparatus, and the second upstanding wall portions are movable relative to the stationary first upstanding wall portions. The movable wall portions define a bottom edge adjacent the bottom wall such that when the movable wall portions open relative to the stationary wall portions, a portion of the bottom wall can be positioned under a piece of furniture, such as a bed, to assist a physically challenged person into and out of the portable bath apparatus. The portable bath apparatus may further include hydrotherapy jets and a shower device which provide a person utilizing the portable bath apparatus with numerous options for personal hygiene.
The present invention involves an aircraft fueling apparatus and associated methods of fueling with features that reduce the risk of fuel spills and other accidents. The present invention more specifically contemplates aircraft fueling methods and apparatus that immobilize a fueler when a fueling nozzle is removed from its holster. Moreover, the apparatus described herein may be easily transported from one place to another and operate safely and effectively without external electrical power.
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James Kuntz
Work:
Accurate Technologies - Sr Software Engineer
James Kuntz
Tagline:
James is a young entrepreneur with huge goals of building a successful business. He loves adding value to people's lives and has a huge heart for making a big impact on families. He strives to become a leader and a builder of other leaders.
12544 High Bluff Dr. #440 San Diego, CA 92130Managing Director at Pacific Wealth Management LLC Jim Kuntz began his investment-advisory career in 1982 with a major global financial services firm. In addition to specializing in financial and retirement... Jim Kuntz began his investment-advisory career in 1982 with a major global financial services firm. In addition to specializing in financial and retirement strategies for affluent investors, he leads Pacific Wealth Management's investment research and due diligence efforts. An acknowledged expert...