公开(公告)号：US20230055331A1

公开(公告)日：2023-02-23

申请号：US17865274

申请日：2022-07-14

Applicant: Ilya Daniel Rosenberg

Inventor： Ilya Daniel Rosenberg

IPC: B64F1/22 ,  B64C25/08 ,  B64D45/08 ,  B64F1/10 ,  B64D47/02 ,  B64F1/02

Abstract: One variation of a tram system includes: a chassis; a latch configured to selectively engage a latch receiver mounted to an aircraft; an alignment feature adjacent the latch and configured to engage an alignment receiver mounted to the aircraft and to communicate acceleration and braking forces from the chassis into the aircraft; an optical sensor facing upwardly from the chassis; a drivetrain configured to accelerate and decelerate the chassis along a runway; and a controller configured to detect an optical fiducial arranged on the aircraft in optical images recorded by the optical sensor adjust a speed of the drivetrain to longitudinally align the alignment feature with the alignment receiver based on positions of the optical fiducial detected in the optical images, trigger the latch to engage the latch receiver once the aircraft has descended onto the chassis, and trigger the drivetrain to actively decelerate the chassis during a landing routine.

公开(公告)号：US20210269173A1

公开(公告)日：2021-09-02

申请号：US17039749

申请日：2020-09-30

Applicant: Ilya Daniel Rosenberg

Inventor： Ilya Daniel Rosenberg

IPC: B64F1/22 ,  B64C25/08 ,  B64D45/08 ,  B64F1/10 ,  B64D47/02 ,  B64F1/02

Abstract: One variation of a tram system includes: a chassis; a latch configured to selectively engage a latch receiver mounted to an aircraft; an alignment feature adjacent the latch and configured to engage an alignment receiver mounted to the aircraft and to communicate acceleration and braking forces from the chassis into the aircraft; an optical sensor facing upwardly from the chassis; a drivetrain configured to accelerate and decelerate the chassis along a runway; and a controller configured to detect an optical fiducial arranged on the aircraft in optical images recorded by the optical sensor adjust a speed of the drivetrain to longitudinally align the alignment feature with the alignment receiver based on positions of the optical fiducial detected in the optical images, trigger the latch to engage the latch receiver once the aircraft has descended onto the chassis, and trigger the drivetrain to actively decelerate the chassis during a landing routine.

公开(公告)号：US11667400B2

公开(公告)日：2023-06-06

申请号：US17865274

申请日：2022-07-14

Applicant: Ilya Daniel Rosenberg

Inventor： Ilya Daniel Rosenberg

IPC: B64F1/22 ,  B64C25/08 ,  B64D45/08 ,  B64F1/10 ,  B64D47/02 ,  B64F1/02 ,  G08G5/06

CPC classification number: B64F1/228 ,  B64C25/08 ,  B64D45/08 ,  B64D47/02 ,  B64F1/0297 ,  B64F1/0299 ,  B64F1/10 ,  B64D2205/00 ,  G08G5/065 ,  Y02T50/40

Abstract: One variation of a tram system includes: a chassis; a latch configured to selectively engage a latch receiver mounted to an aircraft; an alignment feature adjacent the latch and configured to engage an alignment receiver mounted to the aircraft and to communicate acceleration and braking forces from the chassis into the aircraft; an optical sensor facing upwardly from the chassis; a drivetrain configured to accelerate and decelerate the chassis along a runway; and a controller configured to detect an optical fiducial arranged on the aircraft in optical images recorded by the optical sensor adjust a speed of the drivetrain to longitudinally align the alignment feature with the alignment receiver based on positions of the optical fiducial detected in the optical images, trigger the latch to engage the latch receiver once the aircraft has descended onto the chassis, and trigger the drivetrain to actively decelerate the chassis during a landing routine.

公开(公告)号：US20250051035A1

公开(公告)日：2025-02-13

申请号：US18657688

申请日：2024-05-07

Applicant: Ilya Daniel Rosenberg

Inventor： Ilya Daniel Rosenberg

IPC: B64F1/228 ,  B64C25/08 ,  B64D45/08 ,  B64D47/02 ,  B64F1/02 ,  B64F1/10 ,  G08G5/06

Abstract: One variation of a tram system includes: a chassis; a latch configured to selectively engage a latch receiver mounted to an aircraft; an alignment feature adjacent the latch and configured to engage an alignment receiver mounted to the aircraft and to communicate acceleration and braking forces from the chassis into the aircraft; an optical sensor facing upwardly from the chassis; a drivetrain configured to accelerate and decelerate the chassis along a runway; and a controller configured to detect an optical fiducial arranged on the aircraft in optical images recorded by the optical sensor adjust a speed of the drivetrain to longitudinally align the alignment feature with the alignment receiver based on positions of the optical fiducial detected in the optical images, trigger the latch to engage the latch receiver once the aircraft has descended onto the chassis, and trigger the drivetrain to actively decelerate the chassis during a landing routine.

公开(公告)号：US12012227B2

公开(公告)日：2024-06-18

申请号：US18205842

申请日：2023-06-05

Applicant: Ilya Daniel Rosenberg

Inventor： Ilya Daniel Rosenberg

IPC: B64F1/228 ,  B64C25/08 ,  B64D45/08 ,  B64D47/02 ,  B64F1/02 ,  B64F1/10 ,  G08G5/06

CPC classification number: B64F1/228 ,  B64C25/08 ,  B64D45/08 ,  B64D47/02 ,  B64F1/0297 ,  B64F1/0299 ,  B64F1/10 ,  B64D2205/00 ,  G08G5/065 ,  Y02T50/40

Abstract: One variation of a tram system includes: a chassis; a latch configured to selectively engage a latch receiver mounted to an aircraft; an alignment feature adjacent the latch and configured to engage an alignment receiver mounted to the aircraft and to communicate acceleration and braking forces from the chassis into the aircraft; an optical sensor facing upwardly from the chassis; a drivetrain configured to accelerate and decelerate the chassis along a runway; and a controller configured to detect an optical fiducial arranged on the aircraft in optical images recorded by the optical sensor adjust a speed of the drivetrain to longitudinally align the alignment feature with the alignment receiver based on positions of the optical fiducial detected in the optical images, trigger the latch to engage the latch receiver once the aircraft has descended onto the chassis, and trigger the drivetrain to actively decelerate the chassis during a landing routine.

公开(公告)号：US20230406539A1

公开(公告)日：2023-12-21

申请号：US18205842

申请日：2023-06-05

Applicant: Ilya Daniel Rosenberg

Inventor： Ilya Daniel Rosenberg

IPC: B64F1/22 ,  B64C25/08 ,  B64D45/08 ,  B64F1/10 ,  B64D47/02 ,  B64F1/02

CPC classification number: B64F1/228 ,  B64C25/08 ,  B64D45/08 ,  B64F1/10 ,  B64D47/02 ,  B64F1/0297 ,  B64F1/0299 ,  B64D2205/00 ,  G08G5/065

Abstract: One variation of a tram system includes: a chassis; a latch configured to selectively engage a latch receiver mounted to an aircraft; an alignment feature adjacent the latch and configured to engage an alignment receiver mounted to the aircraft and to communicate acceleration and braking forces from the chassis into the aircraft; an optical sensor facing upwardly from the chassis; a drivetrain configured to accelerate and decelerate the chassis along a runway; and a controller configured to detect an optical fiducial arranged on the aircraft in optical images recorded by the optical sensor adjust a speed of the drivetrain to longitudinally align the alignment feature with the alignment receiver based on positions of the optical fiducial detected in the optical images, trigger the latch to engage the latch receiver once the aircraft has descended onto the chassis, and trigger the drivetrain to actively decelerate the chassis during a landing routine.

公开(公告)号：US11420769B2

公开(公告)日：2022-08-23

申请号：US17039749

申请日：2020-09-30

Applicant: Ilya Daniel Rosenberg

Inventor： Ilya Daniel Rosenberg

IPC: B64F1/22 ,  B64C25/08 ,  B64D45/08 ,  B64F1/10 ,  B64D47/02 ,  B64F1/02 ,  G08G5/06

Abstract: One variation of a tram system includes: a chassis; a latch configured to selectively engage a latch receiver mounted to an aircraft; an alignment feature adjacent the latch and configured to engage an alignment receiver mounted to the aircraft and to communicate acceleration and braking forces from the chassis into the aircraft; an optical sensor facing upwardly from the chassis; a drivetrain configured to accelerate and decelerate the chassis along a runway; and a controller configured to detect an optical fiducial arranged on the aircraft in optical images recorded by the optical sensor adjust a speed of the drivetrain to longitudinally align the alignment feature with the alignment receiver based on positions of the optical fiducial detected in the optical images, trigger the latch to engage the latch receiver once the aircraft has descended onto the chassis, and trigger the drivetrain to actively decelerate the chassis during a landing routine.