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公开(公告)号：US11603197B2
公开(公告)日：2023-03-14
申请号：US16331736
申请日：2017-09-11
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Ron Bublitsky
Abstract: A modular vehicle system includes at least one body module having at least one body connection interface, and a kit. The kit includes a plurality of utility modules including at least one first utility module (in the form of a fixed-wing utility module) and at least one second utility module (in the form of a rotor-wing utility module). Each first utility module includes at least one utility module connection interface in the form of a first utility module connection interface for coupling with the body connection interface. Each second utility module includes at least one utility module connection interface in the form of a second utility module connection interface, distinct from the first utility module connection interface, for coupling with the body connection interface. Each body connection interface is configured for selective reversible coupling at least with respect to any one of the utility module connection interfaces while concurrently excluding coupling of another utility module connection interface thereto, to provide an air vehicle.
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公开(公告)号：US11912435B2
公开(公告)日：2024-02-27
申请号：US17623492
申请日：2020-07-06
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Danny Abramov , Artem Korobkov , Ron Bublitsky
CPC classification number: B64D5/00 , B64C37/02 , B64C39/024 , B64C39/08 , B64C39/12 , B64D3/00 , B64C2211/00 , B64U10/25 , B64U30/10
Abstract: There is provided a composite air vehicle system including: a first air vehicle capable of independent aerodynamic flight; a second air vehicle capable of independent aerodynamic flight; and at least one connector element configured for reversibly interconnecting the first air vehicle and the second air vehicle in tandem arrangement to provide a composite air vehicle capable of aerodynamic flight. The composite air vehicle system is configured for enabling at least in-flight separation of composite air vehicle into the first air vehicle and second air vehicle, and for enabling each one of the first air vehicle and said second air vehicle to operate independently of one another.
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Patent Agency Ranking
公开(公告)号：USD947748S1
公开(公告)日：2022-04-05
申请号：US29692400
申请日：2019-05-24
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Designer： Sharon Levy , Ron Bublitsky , Ehud Baharav
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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
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.
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公开(公告)号：US20220355932A1
公开(公告)日：2022-11-10
申请号：US17623492
申请日：2020-07-06
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Danny Abramov , Artem Korobkov , Ron Bublitsky
Abstract: There is provided a composite air vehicle system including: a first air vehicle capable of independent aerodynamic flight; a second air vehicle capable of independent aerodynamic flight; and at least one connector element configured for reversibly interconnecting the first air vehicle and the second air vehicle in tandem arrangement to provide a composite air vehicle capable of aerodynamic flight. The composite air vehicle system is configured for enabling at least in-flight separation of composite air vehicle into the first air vehicle and second air vehicle, and for enabling each one of the first air vehicle and said second air vehicle to operate independently of one another.
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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
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.
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公开(公告)号：US20190210724A1
公开(公告)日：2019-07-11
申请号：US16331736
申请日：2017-09-11
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Ron Bublitsky
CPC classification number: B64C39/024 , B64C3/00 , B64C3/10 , B64C27/08 , B64C37/00 , B64C2201/027 , B64C2201/104 , B64C2201/165 , B64C2211/00 , B64D27/24
Abstract: A modular vehicle system includes at least one body module having at least one body connection interface, and a kit. The kit includes a plurality of utility modules including at least one first utility module (in the form of a fixed-wing utility module) and at least one second utility module (in the form of a rotor-wing utility module). Each first utility module includes at least one utility module connection interface in the form of a first utility module connection interface for coupling with the body connection interface. Each second utility module includes at least one utility module connection interface in the form of a second utility module connection interface, distinct from the first utility module connection interface, for coupling with the body connection interface. Each body connection interface is configured for selective reversible coupling at least with respect to any one of the utility module connection interfaces while concurrently excluding coupling of another utility module connection interface thereto, to provide an air vehicle.
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