Patents by Inventor Jeffrey New
Jeffrey New has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 7422647Abstract: An aircraft part manufacturing device for automated composite lay up includes a mandrel tool having a an interior mandrel surface that conforms to an outside mold line (OML) of a part: to be manufactured. One or more circular rings surround the mandrel and are attached to the mandrel. The circular rings rotate supported by bearings in a bearing cradle so that the mandrel rotates concentrically with the circular rings about an axis of rotation passing through the center of the circular rings. Multiple composite material delivery heads simultaneously deliver material directly to the outside mold line on the interior mandrel surface while the mandrel is rotated. A cantilever supported gantry beam supports the material delivery heads inside the interior mandrel surface. A connecting mechanism connects the material delivery heads to the gantry beam and provides motion of the material delivery heads relative to the interior mandrel surface.Type: GrantFiled: December 9, 2005Date of Patent: September 9, 2008Assignee: The Boeing CompanyInventors: Randall R. Clark, Dwight L. Engwall, Mark G. Yonash, Jeffrey A. New
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Patent number: 7083698Abstract: An aircraft part manufacturing device for automated composite lay up includes a mandrel tool having a an interior mandrel surface that conforms to an outside mold line (OML) of a part: to be manufactured. One or more circular rings surround the mandrel and are attached to the mandrel. The circular rings rotate supported by bearings in a bearing cradle so that the mandrel rotates concentrically with the circular rings about an axis of rotation passing through the center of the circular rings. A composite material delivery head delivers material directly to the outside mold line on the interior mandrel surface while the mandrel is rotated. A cantilever supported gantry beam supports the material delivery head inside the interior mandrel surface. A connecting mechanism connects the material delivery head to the gantry beam and provides motion of the material delivery head relative to the interior mandrel surface.Type: GrantFiled: August 22, 2003Date of Patent: August 1, 2006Assignee: The Boeing CompanyInventors: Dwight L. Engwall, Mark G. Yonash, Randall R. Clark, Jeffrey A. New
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Patent number: 7048024Abstract: An aircraft part manufacturing device for automated composite lay up includes a mandrel tool having a an interior mandrel surface that conforms to an outside mold line (OML) of a part: to be manufactured. One or more circular rings surround the mandrel and are attached to the mandrel. The circular rings rotate supported by bearings in a bearing cradle so that the mandrel rotates concentrically with the circular rings about an axis of rotation passing through the center of the circular rings. Multiple composite material delivery heads simultaneously deliver material directly to the outside mold line on the interior mandrel surface while the mandrel is rotated. A cantilever supported gantry beam supports the material delivery heads inside the interior mandrel surface. A connecting mechanism connects the material delivery heads to the gantry beam and provides motion of the material delivery heads relative to the interior mandrel surface.Type: GrantFiled: August 22, 2003Date of Patent: May 23, 2006Assignee: The Boeing CompanyInventors: Randall R. Clark, Dwight L. Engwall, Mark G. Yonash, Jeffrey A. New
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Publication number: 20060096700Abstract: An aircraft part manufacturing device for automated composite lay up includes a mandrel tool having a an interior mandrel surface that conforms to an outside mold line (OML) of a part: to be manufactured. One or more circular rings surround the mandrel and are attached to the mandrel. The circular rings rotate supported by bearings in a bearing cradle so that the mandrel rotates concentrically with the circular rings about an axis of rotation passing through the center of the circular rings. Multiple composite material delivery heads simultaneously deliver material directly to the outside mold line on the interior mandrel surface while the mandrel is rotated. A cantilever supported gantry beam supports the material delivery heads inside the interior mandrel surface. A connecting mechanism connects the material delivery heads to the gantry beam and provides motion of the material delivery heads relative to the interior mandrel surface.Type: ApplicationFiled: December 9, 2005Publication date: May 11, 2006Inventors: Randall Clark, Dwight Engwall, Mark Yonash, Jeffrey New
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Publication number: 20050151436Abstract: A gear motor assembly comprises an electric motor, and one or more gear reducers comprising first and second spiral bevel gears. The gear motor assembly is configured to power one or more implements such as floor care brushes, burnish drives, polishers, rotary finishers, and the like.Type: ApplicationFiled: January 14, 2004Publication date: July 14, 2005Inventors: Scott Lantzy, Jeffrey New
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Publication number: 20050039842Abstract: An aircraft part manufacturing device for automated composite lay up includes a mandrel tool having a an interior mandrel surface that conforms to an outside mold line (OML) of a part: to be manufactured. One or more circular rings surround the mandrel and are attached to the mandrel. The circular rings rotate supported by bearings in a bearing cradle so that the mandrel rotates concentrically with the circular rings about an axis of rotation passing through the center of the circular rings. Multiple composite material delivery heads simultaneously deliver material directly to the outside mold line on the interior mandrel surface while the mandrel is rotated. A cantilever supported gantry beam supports the material delivery heads inside the interior mandrel surface. A connecting mechanism connects the material delivery heads to the gantry beam and provides motion of the material delivery heads relative to the interior mandrel surface.Type: ApplicationFiled: August 22, 2003Publication date: February 24, 2005Applicant: The Boeing CompanyInventors: Randall Clark, Dwight Engwall, Mark Yonash, Jeffrey New
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Publication number: 20050039844Abstract: An aircraft part manufacturing device for automated composite lay up includes a mandrel tool having a an interior mandrel surface that conforms to an outside mold line (OML) of a part: to be manufactured. One or more circular rings surround the mandrel and are attached to the mandrel. The circular rings rotate supported by bearings in a bearing cradle so that the mandrel rotates concentrically with the circular rings about an axis of rotation passing through the center of the circular rings. A composite material delivery head delivers material directly to the outside mold line on the interior mandrel surface while the mandrel is rotated. A cantilever supported gantry beam supports the material delivery head inside the interior mandrel surface. A connecting mechanism connects the material delivery head to the gantry beam and provides motion of the material delivery head relative to the interior mandrel surface.Type: ApplicationFiled: August 22, 2003Publication date: February 24, 2005Applicant: The Boeing CompanyInventors: Dwight Engwall, Mark Yonash, Randall Clark, Jeffrey New
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Patent number: 4931126Abstract: The present invention relates to a seaming apparatus a method for producing a continuous sheet of thermoplastic material having a predetermined width from a plurality of elongated thermoplastic tapes each having edges defining a transverse width less than the predetermined width and each tape being wound on a roll. The seaming apparatus comprising a frame having a seaming zone. A feed device is mounted on the frame for rotatably supporting a plurality of rolls in a predetermined relationship. An alignment mechanism is mounted on the frame for receiving the tapes from rolls thereof supported by the feed device and for guiding the tapes into the seaming zones along paths defining a predetermined transversely adjacent relationship when the edges of the tapes position adjacent one another form a contiguous area. Thermal heating elements are provided in the seaming zone for thermally joining the contiguous area of the tapes to form the contiguous sheet of thermoplastic material.Type: GrantFiled: April 14, 1989Date of Patent: June 5, 1990Assignee: The Boeing CompanyInventors: Douglas A. McCarville, Jeffrey A. New