-
公开(公告)号：US11698282B2
公开(公告)日：2023-07-11
申请号：US16987623
申请日：2020-08-07
申请人： ABL Space Systems
IPC分类号： G01F23/284 , G01F23/24
CPC分类号： G01F23/24 , G01F23/284
摘要： A system for determining a fluid level includes a front end and a measurement probe. The measurement probe receives a pulse from the front end and returns a partially reflected pulse and a fully reflected pulse to the front end. The partially reflected pulse is evaluated to determine a liquid level within a tank that includes the measurement probe. The measurement probe includes a conductive trace configuration to provide a time delay to prevent pulse build up.
-
公开(公告)号：US11759837B1
公开(公告)日：2023-09-19
申请号：US16654577
申请日：2019-10-16
申请人： ABL Space Systems
发明人： Harrison O'Hanley , Daniel Piemont
CPC分类号： B21D5/008 , B60K15/03 , B64G1/402 , B60K2015/03032
摘要： A method for forming a dome used in a launch vehicle includes cutting a disk from a plate, the disk having a first disk diameter. The method also includes forming a bend in the disk, the bend applying a curvature to at least a portion of the disk, the disk having a second disk diameter after the forming. The method further includes performing a first heat-treating process to the disk. The method also includes performing a second heat-treating process to the disk. The method further includes machining the disk to remove at least a portion of a thickness of the disk.
-
公开(公告)号：US20230184196A1
公开(公告)日：2023-06-15
申请号：US17947883
申请日：2022-09-19
申请人： ABL Space Systems
发明人： Harrison O'Hanley , Ryan Kuhn , Jessica Pauley , Oleg Teplyuk
CPC分类号： F02K1/80 , F02K9/64 , F02K9/972 , B23K9/0026
摘要： A coupling system is utilized to form a multi-part rocket engine thrust compartment that maintains inner channels within walls of the thrust compartment for regenerative cooling. The coupling system includes an insert joint arranged between joint faces of a first segment and a second segment. The first segment and the second segment include inner edges that, when jointed together, form an inner wall. The joint insert is installed between the first segment and the second segment after the inner wall is formed and coupled to the first segment and the second segment. The joint faces of the first segment and the second segment include extending feature to form a flow passage along with cavities at least partially defined by the joint insert.
-
公开(公告)号：US11939935B2
公开(公告)日：2024-03-26
申请号：US17947883
申请日：2022-09-19
申请人： ABL Space Systems
发明人： Harrison O'Hanley , Ryan Kuhn , Jessica Pauley , Oleg Teplyuk
CPC分类号： F02K1/80 , F02K9/64 , F02K9/972 , B23K9/0026
摘要： A coupling system is utilized to form a multi-part rocket engine thrust compartment that maintains inner channels within walls of the thrust compartment for regenerative cooling. The coupling system includes an insert joint arranged between joint faces of a first segment and a second segment. The first segment and the second segment include inner edges that, when jointed together, form an inner wall. The joint insert is installed between the first segment and the second segment after the inner wall is formed and coupled to the first segment and the second segment. The joint faces of the first segment and the second segment include extending feature to form a flow passage along with cavities at least partially defined by the joint insert.
-
公开(公告)号：US20210116286A1
公开(公告)日：2021-04-22
申请号：US16987623
申请日：2020-08-07
申请人： ABL Space Systems
IPC分类号： G01F23/24
摘要： A system for determining a fluid level includes a front end and a measurement probe. The measurement probe receives a pulse from the front end and returns a partially reflected pulse and a fully reflected pulse to the front end. The partially reflected pulse is evaluated to determine a liquid level within a tank that includes the measurement probe. The measurement probe includes a conductive trace configuration to provide a time delay to prevent pulse build up.
-
公开(公告)号：US11448163B1
公开(公告)日：2022-09-20
申请号：US16529733
申请日：2019-08-01
申请人： ABL Space Systems
发明人： Harrison O'Hanley , Ryan Kuhn , Jessica Pauley , Oleg Teplyuk
摘要： A coupling system is utilized to form a multi-part rocket engine thrust compartment that maintains inner channels within walls of the thrust compartment for regenerative cooling. The coupling system includes an insert joint arranged between joint faces of a first segment and a second segment. The first segment and the second segment include inner edges that, when jointed together, form an inner wall. The joint insert is installed between the first segment and the second segment after the inner wall is formed and coupled to the first segment and the second segment. The joint faces of the first segment and the second segment include extending feature to form a flow passage along with cavities at least partially defined by the joint insert.
-
公开(公告)号：US20210229841A1
公开(公告)日：2021-07-29
申请号：US17156183
申请日：2021-01-22
申请人： ABL Space Systems
IPC分类号： B64G1/62
摘要： An orbital delivery system includes a exo-atmospheric system arranged along an orbital or sub-orbital trajectory. The exo-atmospheric system includes a propulsion system to adjust an orientation responsive to a signal to begin a reentry procedure. During the reentry procedure, a deployment system is activated to engage an atmospheric landing system to direct a payload toward a landing location.
-
-
-
-
-
-
搜索结果
7 条记录 (耗时 0.012 秒)
