Patents by Inventor Maxim De Jong
Maxim De Jong 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: 11724833Abstract: Systems for insulating a space vehicle or space borne container from an external environment as well as cryogens from heat sources. Such systems also protect the vehicle from the high dynamic pressures, the high heat loads encountered in atmospheric flight, and provide storage capability that strongly limits, or effectively eliminates, cryogenic boil-off losses once in space. Such systems include an expandable structure having a plurality of contiguously adjacent expandable layers. The layers are connected by a plurality of tension connectors between successive layers. For launch and flight the layers can be restrained in a collapsed position. Whereupon exiting a free stream environment, the layers are expanded where they can lock into place or otherwise remain in an expanded state. The expansion creates separation between the layers with minimal conduction paths providing near theoretically perfect multi-layer insulation and extremely effective debris protection.Type: GrantFiled: December 24, 2019Date of Patent: August 15, 2023Assignee: THIN RED LINE AEROSPACE LTDInventors: Maxim de Jong, Brian Aiken
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Patent number: 10934029Abstract: A joint assembly thermally isolates a warm structure, such as a payload, from a cold structure, such as a cryogenic fuel tank, in a space vehicle while maintaining structural interconnection within the joint assembly. The joint assembly includes a primary joint that is capable of separating, and a secondary joint connected to and adjacent to the primary joint. The secondary joint includes an inflatable annulus structure and one or more restraining members, where separation of the primary joint causes the inflatable annulus structure to be in compression and the one or more restraining members to be in tension.Type: GrantFiled: May 3, 2018Date of Patent: March 2, 2021Assignee: Paragon Space Development CorporationInventors: Chad E. Bower, Maxim de Jong, Brian Aiken, Jose Javier Lopez
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Publication number: 20200148399Abstract: Systems for insulating a space vehicle or space borne container from an external environment as well as cryogens from heat sources. Such systems also protect the vehicle from the high dynamic pressures, the high heat loads encountered in atmospheric flight, and provide storage capability that strongly limits, or effectively eliminates, cryogenic boil-off losses once in space. Such systems include an expandable structure having a plurality of contiguously adjacent expandable layers. The layers are connected by a plurality of tension connectors between successive layers. For launch and flight the layers can be restrained in a collapsed position. Whereupon exiting a free stream environment, the layers are expanded where they can lock into place or otherwise remain in an expanded state. The expansion creates separation between the layers with minimal conduction paths providing near theoretically perfect multi-layer insulation and extremely effective debris protection.Type: ApplicationFiled: December 24, 2019Publication date: May 14, 2020Applicant: THIN RED LINE AEROSPACE LTDInventors: Maxim de Jong, Brian Aiken
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Patent number: 10196123Abstract: A system for elevation control. The system comprises a substantially gastight envelope containing lifting gas wherein the envelope further comprises a plurality of envelope segments in fluid communication with one another. At least one tension cable connects at least two of the envelope segments. A control device including a motor adjusts the length of the tension cable to change the pressure within the envelope to thereby facilitate ascent and descent of the system. The control device causes the system to operate in ascent, descent, or vertically stationary modes.Type: GrantFiled: January 21, 2017Date of Patent: February 5, 2019Assignee: THIN RED LINE AEROSPACE LTDInventor: Maxim de Jong
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Publication number: 20180319516Abstract: This disclosure provides a joint assembly that thermally isolates a warm structure, such as a payload, from a cold structure, such as a cryogenic fuel tank, in a space vehicle while maintaining structural interconnection within the joint assembly. The joint assembly includes a primary joint that is capable of separating, and a secondary joint connected to and adjacent to the primary joint. The secondary joint includes an inflatable annulus structure and one or more restraining members, where separation of the primary joint causes the inflatable annulus structure to be in compression and the one or more restraining members to be in tension.Type: ApplicationFiled: May 3, 2018Publication date: November 8, 2018Inventors: Chad E. Bower, Maxim de Jong, Brian Aiken, Jose Javier Lopez
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Publication number: 20170129579Abstract: A system for elevation control. The system comprises a substantially gastight envelope containing lifting gas wherein the envelope further comprises a plurality of envelope segments in fluid communication with one another. At least one tension cable connects at least two of the envelope segments. A control device including a motor adjusts the length of the tension cable to change the pressure within the envelope to thereby facilitate ascent and descent of the system. The control device causes the system to operate in ascent, descent, or vertically stationary modes.Type: ApplicationFiled: January 21, 2017Publication date: May 11, 2017Applicant: THIN RED LINE AEROSPACE LTDInventor: Maxim de Jong
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Patent number: 8186625Abstract: A flexible vessel includes a restraint structure and a barrier structure. The restraint structure further includes a first portion, and a second substantially rounded end cap portion that is attached to the first portion. The restraint structure also includes an array of tendons. The barrier structure is positioned within the restraint structure. When the barrier contains a fluid, a portion of the load is carried by the restraint structure and another portion of the load is carried by the barrier structure. The flexible vessel is collapsible to occupy a first volume and distended to occupy a second volume. The flexible vessel is part of a system when used in various applications with respect to a craft.Type: GrantFiled: August 9, 2006Date of Patent: May 29, 2012Assignee: The Thin Red Line Aerospace Ltd.Inventor: Maxim De Jong
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Publication number: 20090002257Abstract: This document discloses, among other things, an inflatable apparatus having a plurality of attachment points. The apparatus can be collapsed, and when distended, the attachment points are dimensionally stable with varying applied pressure.Type: ApplicationFiled: May 20, 2008Publication date: January 1, 2009Applicant: Thin Red Line Aerospace Ltd.Inventors: Maxim de Jong, Brian Aiken
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Publication number: 20080078883Abstract: A flexible vessel includes a restraint structure and a barrier structure. The restraint structure further includes a first portion, and a second substantially rounded end cap portion that is attached to the first portion. The restraint structure also includes an array of tendons. The barrier structure is positioned within the restraint structure. When the barrier contains a fluid, a portion of the load is carried by the restraint structure and another portion of the load is carried by the barrier structure. The flexible vessel is collapsible to occupy a first volume and distended to occupy a second volume. The flexible vessel is part of a system when used in various applications with respect to a craft.Type: ApplicationFiled: August 9, 2006Publication date: April 3, 2008Inventor: Maxim de Jong