Patents by Inventor Jayant D. Patel
Jayant D. Patel 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: 10647074Abstract: An aerospace vessel including a fuselage, a means for causing the fuselage to fly coupled to the fuselage, and an environmental control system within the fuselage. The environmental control system includes a duct made of closed cell thermoplastic foam, such as polyvinylidene fluoride foam.Type: GrantFiled: December 6, 2016Date of Patent: May 12, 2020Assignee: The Boeing CompanyInventors: Walter Forrest Frantz, Jayant D. Patel, Douglas Dean Maben, Bruce Whitman, Douglas E. Freeman
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Patent number: 9669593Abstract: An aerospace vessel including a fuselage, a means for causing the fuselage to fly coupled to the fuselage, and an environmental control system within the fuselage. The environmental control system includes a duct made of closed cell thermoplastic foam, such as polyvinylidene fluoride foam.Type: GrantFiled: June 14, 2007Date of Patent: June 6, 2017Assignee: THE BOEING COMPANYInventors: Walter Forrest Frantz, Jayant D. Patel, Douglas Dean Maben, Bruce Whitman, Douglas E. Freeman
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Publication number: 20170082314Abstract: An aerospace vessel including a fuselage, a means for causing the fuselage to fly coupled to the fuselage, and an environmental control system within the fuselage. The environmental control system includes a duct made of closed cell thermoplastic foam, such as polyvinylidene fluoride foam.Type: ApplicationFiled: December 6, 2016Publication date: March 23, 2017Inventors: Walter Forrest Frantz, Jayant D. Patel, Douglas Dean Maben, Bruce Whitman, Douglas E. Freeman
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Patent number: 9168708Abstract: A method of forming a closed cell thermoplastic foam duct and a method of forming a duct and attaching it to an aircraft environmental control system. The environmental control system includes a duct made of closed cell thermoplastic foam, such as polyvinylidene fluoride foam.Type: GrantFiled: June 20, 2013Date of Patent: October 27, 2015Assignee: THE BOEING COMPANYInventors: Walter Forrest Frantz, Jayant D. Patel, Douglas Dean Maben, Bruce Whitman, Douglas E. Freeman
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Publication number: 20130276959Abstract: An aerospace vessel including a fuselage, a means for causing the fuselage to fly coupled to the fuselage, and an environmental control system within the fuselage. The environmental control system includes a duct made of closed cell thermoplastic foam, such as polyvinylidene fluoride foam.Type: ApplicationFiled: June 20, 2013Publication date: October 24, 2013Inventors: Walter Forrest Frantz, Jayant D. Patel, Douglas Dean Maben, Bruce Whitman, Douglas E. Freeman
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Patent number: 8136845Abstract: A coupling apparatus for coupling free ends of a pair of tubular ducts in flow communication with one another, and where the free ends of the ducts are separated by an axial gap. The apparatus may have a sleeve having a length sufficient to span the gap and to overlap portions of the free ends of the ducts when the sleeve is secured to the free ends of the ducts. The sleeve may include a first stretchable ply of material, a non-stretchable ply of material, and a second stretchable ply of material sandwiched together. The non-stretchable ply of material may be disposed between the first and second stretchable plies of material to form a unitary assembly. The non-stretchable ply of material may have an axial length of no more than approximately a length of the axial gap to overlay the axial gap.Type: GrantFiled: December 21, 2007Date of Patent: March 20, 2012Assignee: The Boeing CompanyInventors: Jayant D. Patel, Clifford J. Petersen, Maggie E. Fuselier, Alfred R. Wiratunga, Annette D. Motherwell, Vitor M. Amorim
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Patent number: 7878550Abstract: An apparatus and a system for joining and sealing conduits are provided. The apparatus includes an edge trim positioned proximate to an end of a first conduit, and a sleeve positioned between the first conduit and a second conduit. The sleeve includes a flexible end positioned adjacent to the edge trim such that a portion of the flexible end of the sleeve overlies at least a portion of the edge trim, a semi-rigid end opposite the flexible end and positioned over at least a portion of the second conduit, and a flexible medial portion extending between the flexible end and the semi-rigid end. The apparatus also includes a retaining element configured to be secured over the flexible end of the sleeve such that a portion of the flexible end of the sleeve is sandwiched between the retaining element and the edge trim.Type: GrantFiled: June 30, 2006Date of Patent: February 1, 2011Assignee: The Boeing CompanyInventors: Jayant D. Patel, Alfred R. Wiratunga, Clifford J. Petersen
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Publication number: 20090162140Abstract: A coupling apparatus for coupling free ends of a pair of tubular ducts in flow communication with one another, the free ends of the ducts being separated by an axial gap. The apparatus includes a sleeve having a length sufficient to span the gap and to overlap portions of the free ends of the ducts when the sleeve is secured to the free ends of the ducts. The sleeve includes a first stretchable ply of material, a non-stretchable ply of material, and a second stretchable ply of material sandwiched together to form a unitary assembly. The non-stretchable ply of material has an axial length approximately equal to the axial gap to fill the axial gap. A pair of clamps may be used to secure opposing end portions of the clamp to the free ends of a pair of ducts. The apparatus enables the free ends to be couple together even if slightly misaligned, and the sleeve is highly resistant to ballooning, slippage and rupturing.Type: ApplicationFiled: December 21, 2007Publication date: June 25, 2009Inventors: Jayant D. Patel, Clifford J. Petersen, Maggie E. Fuselier, Alfred R. Wiratunga, Annette D. Motherwell
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Publication number: 20080308674Abstract: An aerospace vessel including a fuselage, a means for causing the fuselage to fly coupled to the fuselage, and an environmental control system within the fuselage. The environmental control system includes a duct made of closed cell thermoplastic foam, such as polyvinylidene fluoride foam.Type: ApplicationFiled: June 14, 2007Publication date: December 18, 2008Inventors: Walter Forrest Frantz, Jayant D. Patel, Douglas Dean Maben, Bruce Whitman, Douglas E. Freeman
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Patent number: 7448219Abstract: A device for controlling fluid flow for heating or cooling an associated system is provided. The present invention includes a housing having a flow control member that includes a bendable portion. The flow control member responds automatically to a pressure condition within the housing and opens or closes based on the direction and quantity of fluid flow and does not include any mechanical or electromechanical control components. The bendable portion may include, for example, a convoluted section. The flow control member is in an open position during a mode of operation of the associated system and is in a closed position in another mode of operation of the system.Type: GrantFiled: June 21, 2004Date of Patent: November 11, 2008Inventors: John L. Bowers, Sham S. Hariram, Jayant D. Patel, Sharanpal S. Sikand
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Publication number: 20080245929Abstract: Systems and methods for fabricating multi-material joining mechanisms are described. In one embodiment, a tool assembly includes a main body having an outer surface, first and second enclosed ends, and an internal chamber. A plurality of vent holes is disposed through the outer surface, wherein each vent hole fluidly communicates with the internal chamber. A circumferentially-disposed ridge is formed on and extends outwardly from the outer surface proximate the second enclosed end. A port is disposed through the first enclosed end and is configured to be coupled to at least one of a source of pressurized medium and a vacuum. A drive assembly is operatively coupled to the second enclosed end and is configured to rotate the main body during a portion of a fabrication process. During operation, the internal chamber may be evacuated during a cure cycle, or may be pressurized to release a component from the outer surface.Type: ApplicationFiled: September 25, 2007Publication date: October 9, 2008Applicant: THE BOEING COMPANYInventors: Jayant D. Patel, Nikhilesh A. Sheth
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Patent number: 7347456Abstract: An apparatus is provided for joining and sealing conduits, includes edge trim, a sleeve, and a retaining element. The edge trim is shaped to mount upon and engage an end of a conduit. The sleeve extends between the conduits and at least partially surrounds the edge trim. The sleeve may be made of compressible material, such that when the retaining element surrounds a portion of the sleeve and the edge trim, the retaining element generally compresses the portion of the sleeve portion underlying the retaining element and displaces the sleeve material to expand on either side of the retaining element and limit movement of the retaining element. The method of joining and sealing conduits includes mounting the edge trim and a retaining element upon an end of a conduit, extending a sleeve between the conduits, and sliding the retaining element over the sleeve toward the end of the conduit.Type: GrantFiled: September 7, 2005Date of Patent: March 25, 2008Assignee: The Boeing CompanyInventors: Jayant D. Patel, Alfred R. Wiratunga
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Publication number: 20080001406Abstract: An apparatus, a system and a method for joining and sealing conduits are provided. According to one embodiment of the present invention, the apparatus includes an edge trim positioned proximate to an end of a first conduit, and a sleeve positioned between the first conduit and a second conduit. The sleeve includes a flexible end positioned adjacent to the edge trim such that a portion of the flexible end of the sleeve overlies at least a portion of the edge trim, a semi-rigid end opposite the flexible end and positioned over at least a portion of the second conduit, and a flexible medial portion extending between the flexible end and the semi-rigid end. The apparatus also includes a retaining element configured to be secured over the flexible end of the sleeve such that a portion of flexible end of the sleeve is sandwiched between the retaining element and the edge trim.Type: ApplicationFiled: June 30, 2006Publication date: January 3, 2008Inventors: Jayant D. Patel, Alfred R. Wiratunga, Clifford J. Petersen
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Patent number: 7028383Abstract: The apparatus for joining and sealing conduits, includes edge trim, a sleeve, and a retaining element. The edge trim is shaped to mount upon and engage an end of a conduit. The sleeve extends between the conduits and at least partially surrounds the edge trim. The sleeve may be made of compressible material, such that when the retaining element surrounds a portion of the sleeve and the edge trim, the retaining element generally compresses the portion of the sleeve portion underlying the retaining element and displaces the sleeve material to expand on either side of the retaining element and limit movement of the retaining element. The method of joining and sealing conduits includes mounting the edge trim and a retaining element upon an end of a conduit, extending a sleeve between the conduits, and sliding the retaining element over the sleeve toward the end of the conduit.Type: GrantFiled: October 30, 2003Date of Patent: April 18, 2006Assignee: The Boeing CompanyInventors: Jayant D. Patel, Alfred R. Wiratunga
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Patent number: 6994378Abstract: The apparatus for joining and sealing conduits, includes edge trim, a sleeve, and a retaining element. The edge trim is shaped to mount upon and engage an end of a conduit. The sleeve extends between the conduits and at least partially surrounds the edge trim. The sleeve may be made of compressible material, such that when the retaining element surrounds a portion of the sleeve and the edge trim, the retaining element generally compresses the portion of the sleeve portion underlying the retaining element and displaces the sleeve material to expand on either side of the retaining element and limit movement of the retaining element. The method of joining and sealing conduits includes mounting the edge trim and a retaining element upon an end of a conduit, extending a sleeve between the conduits, and sliding the retaining element over the sleeve toward the end of the conduit.Type: GrantFiled: October 30, 2003Date of Patent: February 7, 2006Assignee: The Boeing CompanyInventors: Jayant D. Patel, Alfred R. Wiratunga
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Patent number: 6949163Abstract: The apparatus for joining and sealing conduits, includes edge trim, a sleeve, and a retaining element. The edge trim is shaped to mount upon and engage an end of a conduit. The sleeve extends between the conduits and at least partially surrounds the edge trim. The sleeve may be made of compressible material, such that when the retaining element surrounds a portion of the sleeve and the edge trim, the retaining element generally compresses the portion of the sleeve portion underlying the retaining element and displaces the sleeve material to expand on either side of the retaining element and limit movement of the retaining element. The method of joining and sealing conduits includes mounting the edge trim and a retaining element upon an end of a conduit, extending a sleeve between the conduits, and sliding the retaining element over the sleeve toward the end of the conduit.Type: GrantFiled: October 30, 2003Date of Patent: September 27, 2005Assignee: The Boeing CompanyInventors: Jayant D. Patel, Alfred R. Wiratunga
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Patent number: 6830076Abstract: A hose assembly for coupling a plurality of components in fluid connection and a method for making same. According to a first aspect of the invention, the hose assembly includes at least one rigid portion and at least one flexible portion which cooperate to permit the shape and size of the hose assembly to be easily modified so that the components may be coupled to one another. A second aspect of the invention provides a method for reinforcing a flexible portion of the hose assembly to prevent the flexible portion from kinking when the flexible portion is bent. A third aspect of the invention provides a support collar for use in reinforcing an intersection between a pair of duct sections wherein at least one of the duct sections is moveable relative to the other duct section. The support collar reinforces the intersection and helps to render this section less susceptible to tearing.Type: GrantFiled: August 2, 2000Date of Patent: December 14, 2004Assignee: The Boeing CompanyInventor: Jayant D. Patel
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Patent number: 6811192Abstract: The apparatus for joining and sealing conduits, includes edge trim, a sleeve, and a retaining element. The edge trim is shaped to mount upon and engage an end of a conduit. The sleeve extends between the conduits and at least partially surrounds the edge trim. The sleeve may be made of compressible material, such that when the retaining element surrounds a portion of the sleeve and the edge trim, the retaining element generally compresses the portion of the sleeve portion underlying the retaining element and displaces the sleeve material to expand on either side of the retaining element and limit movement of the retaining element. The method of joining and sealing conduits includes mounting the edge trim and a retaining element upon an end of a conduit, extending a sleeve between the conduits, and sliding the retaining element over the sleeve toward the end of the conduit.Type: GrantFiled: April 11, 2002Date of Patent: November 2, 2004Assignee: The Boeing CompanyInventors: Jayant D. Patel, Alfred R. Wiratunga
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Publication number: 20040090012Abstract: The apparatus for joining and sealing conduits, includes edge trim, a sleeve, and a retaining element. The edge trim is shaped to mount upon and engage an end of a conduit. The sleeve extends between the conduits and at least partially surrounds the edge trim. The sleeve may be made of compressible material, such that when the retaining element surrounds a portion of the sleeve and the edge trim, the retaining element generally compresses the portion of the sleeve portion underlying the retaining element and displaces the sleeve material to expand on either side of the retaining element and limit movement of the retaining element. The method of joining and sealing conduits includes mounting the edge trim and a retaining element upon an end of a conduit, extending a sleeve between the conduits, and sliding the retaining element over the sleeve toward the end of the conduit.Type: ApplicationFiled: October 30, 2003Publication date: May 13, 2004Applicant: The Boeing CompanyInventors: Jayant D. Patel, Alfred R. Wiratunga
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Publication number: 20040089401Abstract: The apparatus for joining and sealing conduits, includes edge trim, a sleeve, and a retaining element. The edge trim is shaped to mount upon and engage an end of a conduit. The sleeve extends between the conduits and at least partially surrounds the edge trim. The sleeve may be made of compressible material, such that when the retaining element surrounds a portion of the sleeve and the edge trim, the retaining element generally compresses the portion of the sleeve portion underlying the retaining element and displaces the sleeve material to expand on either side of the retaining element and limit movement of the retaining element. The method of joining and sealing conduits includes mounting the edge trim and a retaining element upon an end of a conduit, extending a sleeve between the conduits, and sliding the retaining element over the sleeve toward the end of the conduit.Type: ApplicationFiled: October 30, 2003Publication date: May 13, 2004Applicant: The Boeing CompanyInventors: Jayant D. Patel, Alfred R. Wiratunga