Patents by Inventor Michael E. Rorabaugh
Michael E. Rorabaugh 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: 10112724Abstract: A hydraulic joint is disclosed. The hydraulic joint includes a tube, a hydraulic fitting, and a tip seal. The hydraulic fitting may be positioned around the tube. The hydraulic fitting may include a first open end for receiving the tube. The tip seal may be configured to define an opening that allows for the passage of leaks. The tip seal may be positioned on the hydraulic fitting adjacent the open end and forming a mechanical barrier between the fitting and the tube.Type: GrantFiled: August 18, 2014Date of Patent: October 30, 2018Assignee: The Boeing CompanyInventors: Michael E. Rorabaugh, James P. Irwin, Benjamin A. Johnson, Erik W. Dowell
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Patent number: 9511536Abstract: Disclosed is an adhesive system that allows for a strong adhesion of a member to a surface, while also allowing for easy removal of the member after a prolonged period of attachment. A releasing agent can be included in an adhesive layer of the adhesive system. A heating system, such as an induction heating system, can be used to heat the releasing agent to activate it to assist in removing the adhesive system.Type: GrantFiled: January 18, 2006Date of Patent: December 6, 2016Assignee: The Boeing CompanyInventors: Donald K. Dabelstein, Michael E. Rorabaugh, Stacey A. Sullivan, Glenn A. Hopper
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Patent number: 9033373Abstract: An axially swaged fitting for use in permanently coupling tubes together. The swaged fitting may be useful in coupling metal hydraulic lines to one another in an airplane. According to one embodiment, the swaged fitting includes a sleeve with a hard metal surface and a swaging ring with a soft metal surface, such that during the swaging process the soft metal surface of the swaging ring is deformed.Type: GrantFiled: May 4, 2011Date of Patent: May 19, 2015Assignee: The Boeing CompanyInventors: James P. Irwin, Michael E. Rorabaugh, Benjamin A. Johnson
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Publication number: 20150091293Abstract: A hydraulic joint is disclosed. The hydraulic joint includes a tube, a hydraulic fitting, and a tip seal. The hydraulic fitting may be positioned around the tube. The hydraulic fitting may include a first open end for receiving the tube. The tip seal may be configured to define an opening that allows for the passage of leaks. The tip seal may be positioned on the hydraulic fitting adjacent the open end and forming a mechanical barrier between the fitting and the tube.Type: ApplicationFiled: August 18, 2014Publication date: April 2, 2015Inventors: Michael E. Rorabaugh, James P. Irwin, III, Benjamin A. Johnson, Erik W. Dowell
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Patent number: 8840740Abstract: Described herein is a novel method and apparatus for preventing spark propagation from a hydraulic joint to a surrounding medium, such as a fuel source. The hydraulic joint includes a fitting and a tube. A tip seal may be placed about the edge of the hydraulic fitting or a sleeve may be placed about the joint, each resulting in an independent mechanical barrier between the joint and surrounding medium, thereby preventing spark propagation to the surrounding medium.Type: GrantFiled: June 24, 2011Date of Patent: September 23, 2014Assignee: The Boeing CompanyInventors: Michael E. Rorabaugh, James P. Irwin, Benjamin A. Johnson, Erik W. Dowell
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Patent number: 8783735Abstract: A method for improving conductance on hydraulic fittings by incorporating a soft metal interlayer between the fitting and a hydraulic tube, wherein the soft metal interlayer is located in an area where the fitting engages the hydraulic tube upon swaging or installation under pressure.Type: GrantFiled: October 24, 2011Date of Patent: July 22, 2014Assignee: The Boeing CompanyInventors: Eddie Kwon, Michael E. Rorabaugh, Benjamin A. Johnson, James P. Irwin, Robert E. Fisher
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Publication number: 20130099490Abstract: A method for improving conductance on hydraulic fittings by incorporating a soft metal interlayer between the fitting and a hydraulic tube, wherein the soft metal interlayer is located in an area where the fitting engages the hydraulic tube upon swaging or installation under pressure.Type: ApplicationFiled: October 24, 2011Publication date: April 25, 2013Applicant: THE BOEING COMPANYInventors: Eddie Kwon, Michael E. Rorabaugh, Benjamin A. Johnson, James P. Irwin, Robert E. Fisher
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Publication number: 20120326433Abstract: Described herein is a novel method and apparatus for preventing spark propagation from a hydraulic joint to a surrounding medium, such as a fuel source. The hydraulic joint includes a fitting and a tube. A tip seal may be placed about the edge of the hydraulic fitting or a sleeve may be placed about the joint, each resulting in an independent mechanical barrier between the joint and surrounding medium, thereby preventing spark propagation to the surrounding medium.Type: ApplicationFiled: June 24, 2011Publication date: December 27, 2012Applicant: THE BOEING COMPANYInventors: Michael E. Rorabaugh, James P. Irwin, Benjamin A. Johnson, Erik W. Dowell
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Publication number: 20120280498Abstract: Described is an improved axially swaged fitting for use in permanently coupling tubes together. The swaged fitting may be useful in coupling metal hydraulic lines to one another in an airplane or other applications, such as industrial hydraulic systems or other systems. According to one embodiment, the swaged fitting includes a sleeve with a hard metal surface and a swaging ring with a soft metal surface, such that during the swaging process the soft metal surface of the swaging ring is deformed.Type: ApplicationFiled: May 4, 2011Publication date: November 8, 2012Applicant: THE BOEING COMPANYInventors: James P. Irwin, Michael E. Rorabaugh, Benjamin A. Johnson
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Publication number: 20040076817Abstract: An adhesive system that allows for a strong adhesion of a member to a surface, while also allowing for easy removal of the member after a prolonged period of attachment. The member may include a structural component or a film or appliqué that is applied for other purposes. The member is affixed to a substrate with an adhesive having a releasing agent or constituent. The releasing agent allows a substantially complete removal of the member and adhesive from the substrate. Also, the adhesive may be easily removed at a desired time in the future due to the application of a particular catalyst. Thus the releasing agent permits a substantially complete removal of both the member and the adhesive which bonds the member or component to the surface.Type: ApplicationFiled: October 18, 2002Publication date: April 22, 2004Inventors: Michael E. Rorabaugh, Stacey A. Sullivan, Glenn A. Hopper
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Patent number: 6417125Abstract: A fibrous ceramic mat is molded from a slurry of ceramic fibers and/or ceramic micropartides and/or a metal. The mat is impregnated with a sol prior to drying. A catalyst for the sol is introduced into the mat to cause the sol to gel. The sol-gel binder forms bonds so that the mat is dimensionally stabilized. The mat is dried to produce the desired ceramic insulation that has preferably a consistent microstructure and a fully gelled sol-gel binder through its entire thickness. If we use a metal, it corrodes (i.e., oxidizes) or otherwise reacts to form a refractory binder that augments the sol and reduces the need to infuse sol incrementally to achieve strength. Using metal powder significantly reduces the cost of manufacture.Type: GrantFiled: June 5, 1995Date of Patent: July 9, 2002Assignee: The Boeing CompanyInventors: Michael E. Rorabaugh, Darryl F. Garrigus, Juris Verzemnieks
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Patent number: 6183852Abstract: A fibrous ceramic mat is molded from a slurry of ceramic fibers and/or ceramic microparticles and/or a metal. The mat is impregnated with a sol prior to drying. A catalyst for the sol is introduced into the mat to cause the sol to gel. The sol-gel binder forms bonds so that the mat is dimensionally stabilized. The mat is dried to produce the desired ceramic insulation that has preferably a consistent microstructure and a fully gelled sol-gel binder through its entire thickness. If we use a metal, it corrodes (i.e., oxidizes) or otherwise reacts to form a refractory binder that augments the sol and reduces the need to infuse sol incrementally to achieve strength. Using metal powder significantly reduces the cost of manufacture.Type: GrantFiled: March 11, 1994Date of Patent: February 6, 2001Assignee: The Boeing CompanyInventors: Michael E. Rorabaugh, Darryl F. Garrigus, Juris Verzemnieks
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Patent number: 5958583Abstract: A coated ceramic has alumina as an amorphous residue from an alumina sol containing alumina powder or and, optionally, a high emittance powder. The alumina powder alters the rheology and wetting characteristics of the sol to aid in forming the residue and increases the alumina concentration (% solids) in the residue. The high emittance powder radiates heat out of the residue and away from the ceramic when the coated ceramic is heated, such as during orbital reentry.Type: GrantFiled: December 20, 1996Date of Patent: September 28, 1999Assignee: The Boeing CompanyInventors: Michael E. Rorabaugh, Charles W. Newquist, Juris Verzemnieks
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Patent number: 5876652Abstract: Improved pin-reinforced sandwich structure ties the face sheets (typically on opposite sides of a foam core) together with a plurality of Z-pins that extend into each face sheet (through the core). The pins are arranged in a tetrahedral or hat section configuration in 2-dimensional or 3-dimensional arrangements to provide enhanced reinforcement, particularly in shear. We are able to improve the pulloff strength additionally by dimpling the core surrounding the pins to produce adhesive fillets along the pins.Type: GrantFiled: June 13, 1997Date of Patent: March 2, 1999Assignee: The Boeing CompanyInventors: Michael E. Rorabaugh, Anthony Falcone
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Patent number: 5869165Abstract: Improved pin-reinforced sandwich structure ties the face sheets (typically on opposite sides of a foam core) together with a plurality of Z-pins that extend into each face sheet (through the core). The pins are arranged in a tetrahedral or hat section configuration in 2-dimensional or 3-dimensional arrangements to provide enhanced reinforcement, particularly in shear. We are able to improve the pulloff strength additionally by dimpling the core surrounding the pins to produce adhesive fillets along the pins.Type: GrantFiled: November 10, 1997Date of Patent: February 9, 1999Assignee: The Boeing CompanyInventors: Michael E. Rorabaugh, Anthony Falcone
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Patent number: 5863846Abstract: A slurry is molded from ceramic fibers and/or microparticles to form a soft felt mat which is impregnated with a sol prior to drying the mat. A catalyst for the sol is caused to diffuse into the mat by exposing the mat to the catalyst and subjecting the mat to a soak time during which the catalyst diffuses into the mat and causes the sol to gel. The sol-gel binder forms bonds so that the mat is dimensionally stabilized. The mat is dried to produce ceramic insulation.Ceramic insulation having a consistent microstructure and a fully gelled sol-gel binder through its entire thickness is also provided.Type: GrantFiled: June 5, 1995Date of Patent: January 26, 1999Assignee: The Boeing CompanyInventors: Michael E. Rorabaugh, Darryl F. Garrigus, Juris Verzemnieks
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Patent number: 5849650Abstract: A fibrous ceramic mat is molded from a slurry of ceramic fibers and/or ceramic microparticles and/or a metal. The mat is impregnated with a sol prior to drying. A catalyst for the sol is introduced into the mat to cause the sol to gel. The sol-gel binder forms bonds so that the mat is dimensionally stabilized. The mat is dried to produce the desired ceramic insulation that has preferably a consistent microstructure and a fully gelled sol-gel binder through its entire thickness. When a metal is used, it corrodes (i.e., oxidizes) or otherwise reacts to form a refractory binder that augments the sol and reduces the need to infuse sol incrementally to achieve strength. Using metal powder significantly reduces the cost of manufacture.Type: GrantFiled: June 5, 1995Date of Patent: December 15, 1998Assignee: The Boeing CompanyInventors: Michael E. Rorabaugh, Darryl F. Garrigus, Juris Verzemnieks
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Patent number: 5753573Abstract: A slurry is molded from ceramic fibers and/or microparticles to form a soft felt mat which is impregnated with a sol prior to drying the mat. A catalyst for the sol is caused to diffuse into the mat by exposing the mat to the catalyst and subjecting the mat to a soak time during which the catalyst diffuses into the mat and causes the sol to gel. The sol-gel binder forms bonds so that the mat is dimensionally stabilized. The mat is dried to produce ceramic insulation.Type: GrantFiled: June 5, 1995Date of Patent: May 19, 1998Assignee: The Boeing CompanyInventors: Michael E. Rorabaugh, Darryl F. Garrigus, Juris Verzemnieks
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Patent number: 5624613Abstract: A slurry is molded from ceramic fibers and/or microparticles to form a soft felt mat which is impregnated with a sol prior to drying the mat. A catalyst for the sol is caused to diffuse into the mat by exposing the mat to the catalyst and subjecting the mat to a soak time during which the catalyst diffuses into the mat and causes the sol to gel. The sol-gel binder forms bonds so that the mat is dimensionally stabilized. The mat is dried to produce ceramic insulation, ceramic insulation having a consistent microstructure and a fully gelled sol-gel binder through its entire thickness.Type: GrantFiled: May 12, 1995Date of Patent: April 29, 1997Assignee: The Boeing CompanyInventors: Michael E. Rorabaugh, Darryl F. Garrigus, Juris Verzemnieks
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Patent number: 5551904Abstract: Carbon-carbon grids for ion optics sets are thermomechanically stable under the extreme temperature changes that are experienced in ion thrusters. Screen, accelerator and decelerator grids are thermomechanically stable, lightweight, and resistant to erosion from ion sputtering and have extended lifetimes over conventional molybdenum grids.Type: GrantFiled: June 5, 1995Date of Patent: September 3, 1996Assignee: The Boeing CompanyInventors: Daniel E. Hedges, Jere S. Meserole, Jr., Michael E. Rorabaugh