公开(公告)号：USD1069646S1

公开(公告)日：2025-04-08

申请号：US29885958

申请日：2023-03-02

Applicant: Zipline International Inc.

Designer： Gregoire Vandenbussche ,  Zoltan Laszlo ,  Devin Williams ,  Brendan Doyle Wade ,  Tristan Semmelhack ,  Keenan Wyrobek ,  Elizabeth Trimble ,  Brian Boomgaard ,  Scott Johnston ,  Daniel Ingriselli ,  Rajan Gill

公开(公告)号：US20240182152A1

公开(公告)日：2024-06-06

申请号：US18285402

申请日：2022-04-28

Applicant: ZIPLINE INTERNATIONAL INC.

Inventor： Brendan Doyle Wade ,  Philip M. Green

IPC: B64C1/06 ,  B64C1/00 ,  H04R1/02 ,  H04R1/04 ,  H04R1/08 ,  H04R1/28

CPC classification number: B64C1/0683 ,  H04R1/028 ,  H04R1/04 ,  H04R1/086 ,  H04R1/2876 ,  B64C2001/0054 ,  B64C2220/00 ,  H04R2410/07 ,  H04R2499/13

Abstract: A nosecone of an aircraft sensor probe may include a first portion defining a tip of the nosecone that is formed from a first material. The nosecone further includes a second portion aft of the first portion and formed from a second material. The second portion may define an internal volume. The second material may have a greater porosity than the first material. The nosecone may further include a third portion aft of the second portion. The third portion may be configured to arrange a microphone assembly relative to the internal volume. The nosecone may a component or subassembly or a sensor probe for the aircraft. For example, the sensor probe may include the nosecone and the microphone assembly. The nosecone may be configured to block the audio signals at the tip and reduce turbulent noise of the audio signals associated with non-parallel local flow angles of the airflow.

公开(公告)号：USD1042225S1

公开(公告)日：2024-09-17

申请号：US29885957

申请日：2023-03-02

Applicant: Zipline International Inc.

Designer： Gregoire Vandenbussche ,  Zoltan Laszlo ,  Eric Chrisman ,  Brian Boomgaard ,  Brendan Doyle Wade ,  Tristan Semmelhack ,  Sven Blaser ,  Frederik Neilsen ,  Keenan Wyrobek ,  Scott Johnston ,  Daniel Ingriselli ,  Noah Allen

Abstract: FIG. 1 is a front isometric view of an aerial vehicle.
FIG. 2 is a bottom isometric view thereof.
FIG. 3 is a front elevation view thereof.
FIG. 4 is a rear elevation view thereof.
FIG. 5 is a right side elevation view thereof.
FIG. 6 is a left side elevation view thereof.
FIG. 7 is a top plan view thereof; and,
FIG. 8 is a bottom plan view thereof.
The broken lines depict portions of the aerial vehicle that form no part of the claimed design.