公开(公告)号：US11952114B2

公开(公告)日：2024-04-09

申请号：US17708532

申请日：2022-03-30

Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

Inventor： Rami Skladman ,  Ron Bublitsky ,  Haim Korach ,  Ben Keshales

IPC: B64C39/02 ,  B64C25/24 ,  B64D3/00 ,  B64D5/00 ,  B64D17/80 ,  B64U70/20 ,  B64U80/82 ,  B64U101/00

CPC classification number: B64C39/022 ,  B64C25/24 ,  B64C39/024 ,  B64D3/00 ,  B64D5/00 ,  B64D17/80 ,  B64U70/20 ,  B64U80/82 ,  B64U2101/00

Abstract: A deployable device mountable on a carrier vehicle and configured to collect situation awareness data. The deployable device includes at least one recorder device configured to collect situation awareness data. The deployable device is capable of being ejected from the carrier vehicle and can be configured to operate as a vehicle and/or be towed by the carrier vehicle. The deployable device can continue collection of situation awareness data after being ejected.

公开(公告)号：US11312489B2

公开(公告)日：2022-04-26

申请号：US16313684

申请日：2017-06-28

Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

Inventor： Rami Skladman ,  Ron Bublitsky ,  Haim Korach ,  Ben Keshales

IPC: B64C39/02 ,  B64C25/24 ,  B64D3/00 ,  B64D5/00 ,  B64D17/80

Abstract: A deployable device mountable on a carrier vehicle and configured to collect situation awareness data. The deployable device includes at least one recorder device configured to collect situation awareness data. The deployable device is capable of being ejected from the carrier vehicle and can be configured to operate as a vehicle and/or be towed by the carrier vehicle. The deployable device can continue collection of situation awareness data after being ejected.

公开(公告)号：US12097970B2

公开(公告)日：2024-09-24

申请号：US18017741

申请日：2021-07-25

Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

Inventor： Rami Skladman ,  Ilan Darmon

IPC: B64D39/04

CPC classification number: B64D39/04

Abstract: Refueling devices for use in in-flight refueling operation are provided, including a body configured for being towed by a tanker aircraft and having a boom member that has a fuel delivery nozzle, a spatial control system and a longitudinal control system. The longitudinal displacement control system includes at least one panel element defining a front panel projected area orthogonal to a body longitudinal axis, each panel element being controllably and reversibly deployable incrementally to each one of a plurality of successive deployed positions between a fully retracted position and a fully deployed position, to provide a respective reversible incrementally increasing aft force to the refueling device at least during the in-flight refueling operation.

公开(公告)号：US11932375B2

公开(公告)日：2024-03-19

申请号：US18004947

申请日：2021-06-30

Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

Inventor： Uri Pinhasi ,  Rami Skladman ,  Gali Oz ,  Igor Golodriga ,  Meital Milo ,  Shay Arzi ,  Rami Zaphir ,  Michele Esther Hasid

IPC: B64C1/22 ,  A62C3/08 ,  B64C5/06 ,  B64D9/00

CPC classification number: B64C1/22 ,  A62C3/08 ,  B64C5/06 ,  B64D9/003 ,  B64D2009/006

Abstract: There are provided examples of an enhanced cargo capacity aircraft, converted from a datum aircraft. The enhanced cargo capacity aircraft includes the datum aircraft and a cargo module. The datum aircraft includes at least a fuselage having a dorsal fuselage part. The cargo module is affixed to the datum aircraft, thereby converting the datum aircraft to the enhanced cargo capacity aircraft. The datum aircraft is designed for aerodynamic flight capability absent the cargo module. The enhanced cargo capacity aircraft is capable of aerodynamic flight. The cargo module provides enhanced cargo capacity to the datum aircraft. The cargo module includes an external aerodynamic fairing defining an internal cargo volume, and is configured for being conformally affixed in overlying relationship with respect to the dorsal fuselage part. The cargo module includes a cargo handling floor and at least one access door, and a cargo handling system configured for transporting and securing at least one cargo unit within the cargo volume. The cargo unit includes a standard unit load device (ULD).

公开(公告)号：US20230339595A1

公开(公告)日：2023-10-26

申请号：US18004947

申请日：2021-06-30

Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

Inventor： Uri Pinhasi ,  Rami Skladman ,  Gali Oz ,  Igor Golodriga ,  Meital Milo ,  Shay Arzi ,  Rami Zaphir ,  Michele Esther Hasid

IPC: B64C5/06 ,  B64C1/22 ,  B64D9/00 ,  A62C3/08

CPC classification number: B64C1/22 ,  A62C3/08 ,  B64C5/06 ,  B64D9/003 ,  B64D2009/006

Abstract: There are provided examples of an enhanced cargo capacity aircraft, converted from a datum aircraft. The enhanced cargo capacity aircraft includes the datum aircraft and a cargo module. The datum aircraft includes at least a fuselage having a dorsal fuselage part. The cargo module is affixed to the datum aircraft, thereby converting the datum aircraft to the enhanced cargo capacity aircraft. The datum aircraft is designed for aerodynamic flight capability absent the cargo module. The enhanced cargo capacity aircraft is capable of aerodynamic flight. The cargo module provides enhanced cargo capacity to the datum aircraft. The cargo module includes an external aerodynamic fairing defining an internal cargo volume, and is configured for being conformally affixed in overlying relationship with respect to the dorsal fuselage part. The cargo module includes a cargo handling floor and at least one access door, and a cargo handling system configured for transporting and securing at least one cargo unit within the cargo volume. The cargo unit includes a standard unit load device (ULD).