公开(公告)号：US20220011786A1

公开(公告)日：2022-01-13

申请号：US17138285

申请日：2020-12-30

Applicant: ZIPLINE INTERNATIONAL INC.

Inventor： Thomas O. Teisberg ,  Rohit H. Sant ,  Matthew O. Derry ,  Michael J. Demertzi ,  Gavin K. Ananda Krishnan ,  Keenan A. Wyrobek ,  Vasumathi Raman ,  Brendan J.D. Wade ,  Blair R. Hagen ,  Randall R. Patterson ,  Philip M. Green

IPC: G05D1/10 ,  G05D1/00 ,  H04R1/32 ,  H04R29/00 ,  G06N3/02

Abstract: An acoustic detection system of an aircraft receives a first signal, where the first signal is a multichannel audio signal. The multichannel audio signal is determined to be associated with at least one intruding aircraft based on the multichannel audio signal. An avoidance maneuver is commanded for the aircraft based on a track of the intruding aircraft generated based on the multichannel audio signal and a second signal providing additional information about the intruding aircraft.

公开(公告)号：US20220089293A1

公开(公告)日：2022-03-24

申请号：US17485050

申请日：2021-09-24

Applicant: ZIPLINE INTERNATIONAL INC.

Inventor： Keenan A. Wyrobek ,  Gavin K. Ananda Krishnan ,  Brendan J.D. Wade ,  Philip M. Green ,  Randall R. Patterson

IPC: B64D45/04

Abstract: Described herein is an aircraft. The aircraft includes a peripheral assembly, such as a sensor probe. The aircraft further includes a release assembly connecting the peripheral assembly to a portion of the aircraft. The release assembly is configured to separate the peripheral assembly and the portion upon receipt of a threshold force. The release assembly may be configured to allow for the quick release, such as via a snap-fit connection, between the peripheral assembly and the portion of the aircraft.