IP Library › Granted Patent US 12,606,307
Granted Patent B2
US 12,606,307 · App. 17/967,489 · Granted Apr 21, 2026

Human and/or non-human cargo attachment device for use with a rotorcraft

Inventors: Dominik Vogel (Langweid, DE); Christoph Heider (Rain Am Lech, DE); Stefan Salzburger (Augsburg, DE); Alexandru Dinca (Donauworth, DE)
Assignee: AIRBUS HELICOPTERS DEUTSCHLAND GMBH
B64D1/22B33Y80/00B64C27/04B66C1/22B66C1/34
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Quick Facts
Patent No.
US 12,606,307
App. No.
17/967,489
Granted
Apr 21, 2026
Kind
B2
Abstract

A human and/or non-human cargo attachment device for a rotorcraft, comprising: a mounting interface with a mounting base carrier 11 d that is removably attachable to an associated attachment for attachment to a rotorcraft rope or cable; a connecting member that is spaced apart from the mounting base carrier; and a plurality of lateral attachments which are connected to the mounting base carrier and the connecting member; wherein each lateral attachment of the plurality of lateral attachments forms a main lashing point for attachment of human external cargo and comprises an associated inner web that is connected to the mounting base carrier and the connecting member; and wherein the associated inner webs of the plurality of lateral attachments are spaced apart from each other in peripheral direction of the mounting base carrier and form a tube-shaped inner region.

Claims (22)

1 . A human and/or non-human cargo attachment device for use with a rotorcraft, comprising:

a mounting interface with a mounting base carrier that is removably attachable to an associated attachment for attachment to a rotorcraft rope or cable;

a connecting member that is spaced apart from the mounting base carrier; and

a plurality of lateral attachments which are connected to the mounting base carrier and the connecting member;

wherein the plurality of lateral attachments, the mounting base carrier, and the connecting member form a device body with a height direction;

wherein the connecting member is spaced apart from the mounting base carrier in the height direction of the device body;

wherein each lateral attachment of the plurality of lateral attachments forms a main lashing point for attachment of human external cargo and comprises an associated inner web that is connected to the mounting base carrier and the connecting member; and

wherein the associated inner webs of the plurality of lateral attachments are spaced apart from each other in peripheral direction of the mounting base carrier and form a tube-shaped inner region extending in height direction of the device body.

2 . The human and/or non-human cargo attachment device of claim 1 , wherein each lateral attachment of the plurality of lateral attachments extends in an associated extension plane, and wherein the associated extension planes of the plurality of lateral attachments are spaced apart from each other in the peripheral direction of the mounting base carrier.

3 . The human and/or non-human cargo attachment device of claim 2 , wherein each lateral attachment of the plurality of lateral attachments comprises an upper web and a lower web which are interconnected in an angled arrangement at an associated interconnection region and which are further connected to the associated inner web of the lateral attachment.

4 . The human and/or non-human cargo attachment device of claim 3 , wherein the upper web, the lower web, and the associated inner web of each lateral attachment of the plurality of lateral attachments form a triangular structure in the associated extension plane of the lateral attachment.

5 . The human and/or non-human cargo attachment device of claim 3 , wherein the main lashing point of each lateral attachment of the plurality of lateral attachments is arranged in the associated interconnection region of the lateral attachment.

6 . The human and/or non-human cargo attachment device of claim 3 , wherein each lateral attachment of the plurality of lateral attachments forms a redundant lashing point for an additional attachment of the human external cargo.

7 . The human and/or non-human cargo attachment device of claim 6 , wherein the redundant lashing point of the lateral attachment is arranged in the associated interconnection region of the lateral attachment.

8 . The human and/or non-human cargo attachment device of claim 1 , wherein the mounting base carrier is further removably attachable inside the tube-shaped inner region to an additional attachment for attachment of non-human external cargo.

9 . The human and/or non-human cargo attachment device of claim 8 , wherein the mounting base carrier is at least equipped with two mounting lugs which are attachable by means of a mounting bolt to the additional attachment.

10 . The human and/or non-human cargo attachment device of claim 1 , wherein the mounting base carrier is plate-shaped, wherein the associated inner webs are connected to an outer circumference of the mounting base carrier, and wherein the mounting base carrier and the plurality of lateral attachments form a star-shaped arrangement in radial direction of the mounting base carrier.

11 . The human and/or non-human cargo attachment device of claim 1 , wherein the plurality of lateral attachments is further interconnected via associated stiffening ribs.

12 . The human and/or non-human cargo attachment device of claim 1 , wherein the mounting base carrier is at least equipped with three mounting lugs which are attachable by means of a mounting bolt to an associated attachment for attachment to a rotorcraft rope or cable.

13 . The human and/or non-human cargo attachment device of claim 1 , wherein the device body is 3D printed, preferably by means of a 3D titanium printing process.

14 . The human and/or non-human cargo attachment device of claim 1 , wherein the device body forms a confined space outside the tube-shaped inner region, and wherein the confined space is filled with foam.

15 . The human and/or non-human cargo attachment device of claim 1 , wherein a plurality of redundancy cables or ropes is routed inside the device body to guarantee secure functioning of the device body at least upon breakage of one or more of the plurality of lateral attachments.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 1, 2022
From: VOGEL, DOMINIK; HEIDER, CHRISTOPH; SALZBURGER, STEFAN; DINCA, ALEXANDRU
To: AIRBUS HELICOPTERS DEUTSCHLAND GMBH
Reel/Frame 061614/0474 →
Priority Claims (1)
EP 21400023 · Nov 23, 2021 · regional
Continuity (1)
Related Publication 20230159168A1 · May 25, 2023
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