IP Library Granted Patent US 12,357,517
Granted Patent B2
US 12,357,517 · App. 17/752,123 · Granted Jul 15, 2025

Gyroscope assisted helicopter rescue lift systems and methods

Inventors: Biplav Bijoy Goswami (Bangalore, IN); Girish Channakeshavrao Hirekerur (Bengaluru, IN)
Assignee: HORNET ACQUISITIONCO, LLC
A61G1/06B64D1/22A61G2203/36A61G2203/38A61G2220/10
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Quick Facts
Patent No.
US 12,357,517
App. No.
17/752,123
Granted
Jul 15, 2025
Kind
B2
Abstract

A patient litter basket spin control assembly includes a first gyroscope and a motion sensor for sensing an angular acceleration of a patient litter basket. The first gyroscope generates a counter torque to the litter basket to slow the angular acceleration of the litter basket to provide stabilization. The first gyroscope and a second gyroscope may be configured as a pair and located at opposite ends of the litter basket.

Claims (34)

1. A patient litter basket spin control assembly comprising:

a base of the litter basket;

a plurality of sidewalls extending perpendicular from the base of the litter basket to form a patient space for containing a patient;

a first gyroscope disposed at least partially within a first sidewall of the litter basket and comprising a first flywheel rotatably mounted to a second gimbal, which is rotatably mounted to a first gimbal, which is rotatably mounted to a first frame such that the first flywheel is rotatable in three dimensions;

a second gyroscope disposed at least partially within a second sidewall of the litter basket and comprising a second flywheel rotatably mounted to a fourth gimbal, which is rotatably mounted to a third gimbal, which is rotatably mounted to a second frame such that the second flywheel is rotatable in three dimensions; and

a motion sensor for sensing an angular acceleration of the patient litter basket, the first gyroscope configured to rotate the first flywheel about a first flywheel rotation axis and the second gyroscope to rotate the second flywheel about a second flywheel rotation axis to generate a gyroscopic torque as a counter torque in a rotational direction to slow the angular acceleration of the patient litter basket.

2. The patient litter basket spin control assembly of claim 1 , further comprising a controller associated with the first gyroscope and associated with an onboard computer of an aircraft.

3. The patient litter basket spin control assembly of claim 1 , wherein the first gyroscope and the second gyroscope form a first gyroscope pair configured to be simultaneously activated to generate the counter torque.

4. The patient litter basket spin control assembly of claim 3 , wherein the first gyroscope and the second gyroscope are configured to be coupled opposite each other with respect to the patient litter basket.

5. The patient litter basket spin control assembly of claim 4 , further comprising a second gyroscope pair comprising a third gyroscope and a fourth gyroscope, wherein the first gyroscope and the second gyroscope are configured to be disposed at opposite ends of the patient litter basket and the third gyroscope and the fourth gyroscope are configured to be disposed at opposite sides of the patient litter basket.

6. The patient litter basket spin control assembly of claim 5 , wherein the second gyroscope pair is configured to be located substantially midway between a first end and a second end of the patient litter basket.

7. The patient litter basket spin control assembly of claim 1 , further comprising a power source associated with the first gyroscope.

8. The patient litter basket spin control assembly of claim 1 , wherein the first frame is a circular frame surrounding the first gimbal in a first plane, the first gimbal is a first circular gimbal surrounding the second gimbal in a second plane, and the second gimbal is a second circular gimbal surrounding the first flywheel in a third plane, and wherein the first flywheel is rotatable in three dimensions with respect to the first frame.

9. A patient litter basket assembly comprising:

a litter basket having a base and a plurality of sidewalls extending perpendicular to the base, the litter basket configured to be raised and lowered by a helicopter using a cable;

a first gyroscope pair disposed at least partially within the sidewalls of the litter basket comprising a first gyroscope with a first flywheel rotatable in three dimensions and a second gyroscope with a second flywheel rotatable in three dimensions; and

a motion sensor for sensing an angular acceleration of the litter basket, the first gyroscope pair configured to rotate the first flywheel about a first flywheel rotation axis and the second gyroscope to rotate the second flywheel about a second flywheel rotation axis to generate a gyroscopic torque as a counter torque in a rotational direction to slow the angular acceleration of the litter basket.

10. The patient litter basket spin control assembly of claim 9 , further comprising a second gyroscope pair comprising a third gyroscope and a fourth gyroscope.

11. The patient litter basket spin control assembly of claim 10 , wherein the third gyroscope and the fourth gyroscope are configured to be disposed at opposite sides of the litter basket.

12. The patient litter basket spin control assembly of claim 10 , wherein the third gyroscope comprises a third flywheel configured to rotate about a third flywheel rotation axis;

the fourth gyroscope comprises a fourth flywheel configured to rotate about a fourth flywheel rotation axis in a rotational direction opposite the third flywheel; and

the third flywheel rotation axis is parallel to the fourth flywheel rotation axis.

13. The patient litter basket spin control assembly of claim 9 , wherein the first gyroscope and the second gyroscope are configured to be disposed at opposite ends of the litter basket.

14. The patient litter basket spin control assembly of claim 9 , wherein the second flywheel is configured to rotate in a rotational direction opposite the first flywheel; and

the first flywheel rotation axis is parallel to the second flywheel rotation axis.

15. The patient litter basket spin control assembly of claim 9 , further comprising a power source for powering the first gyroscope and the motion sensor.

16. The patient litter basket spin control assembly of claim 9 , wherein at least one of the first gyroscope and the second gyroscope is mounted to a sidewall of the litter basket.

17. The patient litter basket spin control assembly of claim 10 , wherein at least one of the third gyroscope and the fourth second gyroscope is mounted to a base of the litter basket.

18. A patient litter basket spin control assembly comprising:

a base of the litter basket;

a plurality of sidewalls extending perpendicular from the base of the litter basket to form a patient space for containing a patient;

a first gyroscope disposed at least partially within a first sidewall of the litter basket and comprising a first flywheel rotatably mounted to a second circular gimbal, which is rotatably mounted to a first circular gimbal, which is rotatably mounted to a first circular frame such that the first flywheel is rotatable in three dimensions with respect to the first circular frame, such that the first circular frame surrounds the first circular gimbal in a first plane, such that the first circular gimbal surrounds the second circular gimbal in a second plane, and such that the second circular gimbal surrounds the first flywheel in a third plane;

a second gyroscope disposed at least partially within a second sidewall of the litter basket and comprising a second flywheel rotatably mounted to a fourth gimbal, which is rotatably mounted to a third gimbal, which is rotatably mounted to a second frame such that the second flywheel is rotatable in three dimensions; and

a motion sensor for sensing an angular acceleration of the patient litter basket, the first gyroscope configured to rotate the first flywheel about a first flywheel rotation axis and the second gyroscope to rotate the second flywheel about a second flywheel rotation axis to generate a gyroscopic torque as a counter torque in a rotational direction to slow the angular acceleration of the patient litter basket.

Assignments (6)
RELEASE OF SECURITY INTEREST Recorded Dec 13, 2024
From: BARINGS FINANCE LLC, AS COLLATERAL AGENT
To: HORNET ACQUISITIONCO, LLC; INTERNATIONAL MEZZO TECHNOLOGIES, INC.
Reel/Frame 069645/0938 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 13, 2024
From: GOODRICH CORPORATION
To: HORNET ACQUISITIONCO, LLC
Reel/Frame 069648/0049 →
U.S. INTELLECTUAL PROPERTY SECURITY AGREEMENT Recorded Dec 12, 2024
From: INTERNATIONAL MEZZO TECHNOLOGIES, INC.; LIFESAVING SYSTEMS, LLC; HORNET ACQUISITIONCO, LLC; HARTZELL ENGINE TECHNOLOGIES LLC; AIR COMM CORPORATION LLC; ONBOARD SYSTEMS INTERNATIONAL, LLC; ENVIRO SYSTEMS, INC.; TAILWIND TECHNOLOGIES LLC; HARTZELL PROPELLER LLC; AMERITECH INDUSTRIES, INC.
To: JPMORGAN CHASE BANK, N.A.
Reel/Frame 069604/0015 →
SECURITY INTEREST Recorded Oct 31, 2024
From: HORNET ACQUISITIONCO, LLC; INTERNATIONAL MEZZO TECHNOLOGIES, INC.
To: BARINGS FINANCE LLC, AS COLLATERAL AGENT
Reel/Frame 069284/0088 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 24, 2022
From: GOSWAMI, BIPLAV BIJOY; HIREKERUR, GIRISH CHANNAKESHAVRAO
To: GOODRICH AEROSPACE SERVICES PRIVATE LIMITED
Reel/Frame 059999/0434 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 24, 2022
From: GOODRICH AEROSPACE SERVICES PRIVATE LIMITED
To: GOODRICH CORPORATION
Reel/Frame 059999/0539 →