Patents by Inventor Aram Aris Krikorian
Aram Aris Krikorian 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: 11084590Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.Type: GrantFiled: July 15, 2019Date of Patent: August 10, 2021Assignee: Safran Cabin Inc.Inventors: Gary Tien Le, Aram Aris Krikorian
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Publication number: 20210147082Abstract: An overhead stowage bin assembly having a bin structure with a lower panel and an open side that defines a front of the stowage bin assembly. The lower panel has a leading edge that is arranged at the front of the stowage bin assembly. A cover is formed by base plates and a central plate and is secured to the lower panel to form a passage. The central plate has protruding ribs that are aligned to increase the stiffness of the cover and the rigidity of the lower panel. A threshold has walls that are connected to each other and define a channel. The leading edge of the lower panel is received within the channel such that the threshold walls mate with opposite surfaces of the lower panel so as to grip the leading edge of the panel and further enhance the stiffness of the lower panel.Type: ApplicationFiled: November 13, 2020Publication date: May 20, 2021Inventors: Stephen Michael KING, Gary Tien LE, Aram Aris KRIKORIAN, Joseph Wesley MORAN, Louis Edward MAMMOLITO
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Publication number: 20190337625Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.Type: ApplicationFiled: July 15, 2019Publication date: November 7, 2019Applicant: C&D Zodiac, Inc.Inventors: Gary Tien Le, Aram Aris Krikorian
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Patent number: 10392114Abstract: Components and systems of an aircraft seating assembly are disclosed. The aircraft seating assembly can include a seat pan, a connection frame, and one or more mounts for removably coupling the seat pan to the connection frame. The aircraft seating assembly can include a back support having a removably coupled cushioning member. The aircraft seating assembly can include a tilt system which can allow the back support to articulate relative to the connection frame. The aircraft seating assembly can include a retention system coupled to the back support, the retention system can retain an object in place when in a closed configuration.Type: GrantFiled: August 31, 2017Date of Patent: August 27, 2019Assignee: ENCORE SEATS, INC.Inventors: Gary Tien Le, Wade Franklin DeLaney, Elijah Dobrusin, Aram Aris Krikorian, Thomas Zachary Lloyd, Luke Neil Pearson, Nicholas Stanley Borg Carpenter, Matthew Vu Hoang, Thomas Rodolph Eaton
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Patent number: 10392115Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.Type: GrantFiled: August 10, 2018Date of Patent: August 27, 2019Assignee: C&D Zodiac, Inc.Inventors: Gary Tien Le, Aram Aris Krikorian
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Publication number: 20180346127Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.Type: ApplicationFiled: August 10, 2018Publication date: December 6, 2018Applicant: C&D Zodiac, Inc.Inventors: Gary Tien Le, Aram Aris Krikorian
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Patent number: 10144515Abstract: Components and systems of an aircraft seating assembly are disclosed. The aircraft seating assembly can include an adjustable headrest that allows the headrest to be translated and/or rotated relative to a seat, a storage sleeve, and/or a spreader. The aircraft seating assembly can include an energy absorption system. The energy absorption system can include bracket which can control pivoting of a seat back relative to the bracket when subject to forces exceeding a threshold force. The energy absorption system can include a movable wall coupled to the seat.Type: GrantFiled: March 31, 2017Date of Patent: December 4, 2018Assignee: ENCORE SEATS, INC.Inventors: Gary Tien Le, Wade Franklin DeLaney, Elijah Dobrusin, Aram Aris Krikorian, Thomas Rodolph Eaton, Christopher Michael Gumbleton
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Patent number: 10059456Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.Type: GrantFiled: March 2, 2016Date of Patent: August 28, 2018Assignee: C&D Zodiac, Inc.Inventors: Gary Tien Le, Aram Aris Krikorian
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Publication number: 20180079509Abstract: Components and systems of an aircraft seating assembly are disclosed. The aircraft seating assembly can include a seat pan, a connection frame, and one or more mounts for removably coupling the seat pan to the connection frame. The aircraft seating assembly can include a back support having a removably coupled cushioning member. The aircraft seating assembly can include a tilt system which can allow the back support to articulate relative to the connection frame. The aircraft seating assembly can include a retention system coupled to the back support, the retention system can retain an object in place when in a closed configuration.Type: ApplicationFiled: August 31, 2017Publication date: March 22, 2018Inventors: Gary Tien Le, Wade Franklin DeLaney, Elijah Dobrusin, Aram Aris Krikorian, Thomas Zachary Lloyd, Luke Neil Pearson, Nicholas Stanley Borg Carpenter, Matthew Vu Hoang, Thomas Randolph Eaton, Christopher Michael Gumbleton, Kyle Robert Bettenhausen
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Publication number: 20180050803Abstract: Components and systems of an aircraft seating assembly are disclosed. The aircraft seating assembly can include an adjustable headrest that allows the headrest to be translated and/or rotated relative to a seat, a storage sleeve, and/or a spreader. The aircraft seating assembly can include an energy absorption system. The energy absorption system can include bracket which can control pivoting of a seat back relative to the bracket when subject to forces exceeding a threshold force. The energy absorption system can include a movable wall coupled to the seat.Type: ApplicationFiled: March 31, 2017Publication date: February 22, 2018Inventors: Gary Tien Le, Wade Franklin DeLaney, Elijah Dobrusin, Aram Aris Krikorian, Thomas Randolph Eaton, Christopher Michael Gumbleton
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Patent number: 9764844Abstract: Components and systems of an aircraft seating assembly are disclosed. The aircraft seating assembly can include a seat pan, a connection frame, and one or more mounts for removably coupling the seat pan to the connection frame. The aircraft seating assembly can include a back support having a removably coupled cushioning member. The aircraft seating assembly can include a tilt system which can allow the back support to articulate relative to the connection frame. The aircraft seating assembly can include a retention system coupled to the back support, the retention system can retain an object in place when in a closed configuration.Type: GrantFiled: April 1, 2016Date of Patent: September 19, 2017Assignee: Encore Seats, Inc.Inventors: Gary Tien Le, Wade Franklin DeLaney, Elijah Dobrusin, Aram Aris Krikorian, Thomas Zachary Lloyd, Luke Neil Pearson, Nicholas Stanley Borg Carpenter, Matthew Vu Hoang, Thomas Randolph Eaton
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Publication number: 20160297533Abstract: Components and systems of an aircraft seating assembly are disclosed. The aircraft seating assembly can include a seat pan, a connection frame, and one or more mounts for removably coupling the seat pan to the connection frame. The aircraft seating assembly can include a back support having a removably coupled cushioning member. The aircraft seating assembly can include a tilt system which can allow the back support to articulate relative to the connection frame. The aircraft seating assembly can include a retention system coupled to the back support, the retention system can retain an object in place when in a closed configuration.Type: ApplicationFiled: April 1, 2016Publication date: October 13, 2016Inventors: Gary Tien Le, Wade Franklin DeLaney, Elijah Dobrusin, Aram Aris Krikorian, Thomas Zachary Lloyd, Luke Neil Pearson, Nicholas Stanley Borg Carpenter, Matthew Vu Hoang, Thomas Randolph Eaton, Christopher Michael Gumbleton, Kyle Robert Bettenhausen
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Publication number: 20160176527Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.Type: ApplicationFiled: March 2, 2016Publication date: June 23, 2016Inventors: Gary Tien Le, Aram Aris Krikorian
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Publication number: 20150145312Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.Type: ApplicationFiled: February 3, 2015Publication date: May 28, 2015Inventors: Gary Tien Le, Aram Aris Krikorian
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Patent number: 8974002Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.Type: GrantFiled: July 11, 2013Date of Patent: March 10, 2015Assignee: C&D Zodiac, Inc.Inventors: Gary Tien Le, Aram Aris Krikorian
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Patent number: 8506015Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.Type: GrantFiled: April 5, 2010Date of Patent: August 13, 2013Assignee: C&D Zodiac, Inc.Inventors: Gary Tien Le, Aram Aris Krikorian
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Publication number: 20100289318Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.Type: ApplicationFiled: April 5, 2010Publication date: November 18, 2010Inventors: Gary Tien Le, Aram Aris Krikorian