IP Library Granted Patent US 12,654,847
Granted Patent B2
US 12,654,847 · App. 19/170,659 · Granted Jun 16, 2026

Pneumo-mechanical landing gear deployment system and method

Inventors: Donald Edward Hill (Wichita, KS); Michael R. DePinto (Wichita, KS); Matthew J. Allmond (Wichita, KS); Michael Troy Heeren (Wichita, KS); Dennis Scarberry (Wichita, KS)
Assignee: Textron Aviation Inc.
B64C25/20B64C25/26B64C25/30
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12,654,847
App. No.
19/170,659
Granted
Jun 16, 2026
Kind
B2
Abstract

A pneumo-mechanical landing gear deployment system includes a dual-stage handle operatively connected to a pressurized tank, a nose landing gear pneumatically connected to the pressurized tank, and a main landing gear pneumatically connected to the pressurized tank. Actuation of the dual-stage handle to a first position opens the pressurized tank thereby deploying the nose landing gear. Actuation of the dual-stage handle to a second position causes further opening of the pressurized tank thereby deploying the main landing gear. The system may be employed as a backup landing gear deployment system in the case of a primary landing gear system failure.

Claims (27)

1 . A method of servicing a pneumo-mechanical landing gear deployment system in which a nose landing gear and a main landing gear have been deployed, the method comprising:

partially retracting the nose landing gear and the main landing gear;

relieving pressure from the nose landing gear and the main landing gear via a relief valve;

extending the nose landing gear and the main landing gear;

closing a shutoff valve disposed pneumatically downstream of a pressurized tank;

closing a release valve disposed at the pressurized tank; and

repressurizing the pressurized tank.

2 . The method of claim 1 , wherein a secondary extension component may be unlocked for unlocking either the nose landing gear or the main landing gear prior to partially retracting.

3 . The method of claim 1 , wherein relieving pressure further comprises relieving any residual pressurized gas stored within a pressurized tank.

4 . The method of claim 1 , wherein extending the nose landing gear and the main landing gear comprises moving each of the nose landing gear and the main landing gear from an unlocked position to a locked position.

5 . The method of claim 1 , wherein closing the shutoff valve comprises actuating a dual-stage handle from a second position to a first position.

6 . The method of claim 5 , wherein closing the release valve comprises actuating the dual-stage handle from the first position to an initial starting position.

7 . The method of claim 1 , wherein repressurizing the pressurized tank comprises delivering pressurized gas to the pressurized tank via the relief valve.

8 . A method of servicing a pneumo-mechanical landing gear deployment system, wherein the pneumo-mechanical landing gear deployment system comprises a dual-stage handle operatively connected to a pressurized tank, a nose landing gear pneumatically connected to the pressurized tank, and a main landing gear pneumatically connected to the pressurized tank, the method comprising:

unlocking the nose landing gear and the main landing gear;

partially retracting the nose landing gear and the main landing gear;

relieving any pressure from the nose landing gear and the main landing gear by releasing a pressurized gas via a relief valve;

extending the nose landing gear and the main landing gear;

closing a shutoff valve disposed pneumatically downstream of the pressurized tank;

closing a release valve operatively coupled to the pressurized tank; and

repressurizing the pressurized tank.

9 . The method of claim 8 , wherein unlocking at least one of the nose landing gear or the main landing gear comprises unlocking a secondary extension component.

10 . The method of claim 8 , wherein relieving pressure further comprises relieving a pressurized gas stored within the pressurized tank.

11 . The method of claim 8 , wherein extending the nose landing gear and the main landing gear comprises returning each of the nose landing gear and the main landing gear from an unlocked position to a locked position.

12 . The method of claim 8 , wherein closing the shutoff valve comprises actuating the dual-stage handle from a second position to a first position.

13 . The method of claim 8 , wherein closing the release valve comprises actuating the dual-stage handle from a first position to an initial starting position.

14 . The method of claim 8 , wherein repressurizing the pressurized tank comprises delivering pressurized gas to the pressurized tank via the relief valve.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 15, 2026
From: TEXTRON AVIATION INC.
To: TEXTRON AVIATION RHODE ISLAND INC.
Reel/Frame 075281/0872 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 15, 2026
From: TEXTRON AVIATION RHODE ISLAND INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 075281/0933 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 4, 2025
From: HILL, DONALD EDWARD; DEPINTO, MICHAEL R.; ALLMOND, MATTHEW J.; HEEREN, MICHAEL TROY; SCARBERRY, DENNIS
To: TEXTRON AVIATION INC.
Reel/Frame 070742/0141 →
Continuity (3)
Continuation 18345749 · Jun 30, 2023
Provisional Application 63357895 · Jul 1, 2022
Related Publication 20250256839A1 · Aug 14, 2025
References Cited (7)
US 8191827B2 · Reynes · 2012 [cited by examiner]
US 10301846B2 · Macaraeg · 2019 [cited by applicant]
US 10364022B2 · Bond et al. · 2019 [cited by applicant]
US 10689098B2 · Waltner · 2020 [cited by examiner]
US 10894597B2 · Persico · 2021 [cited by examiner]
US 11192640B2 · Pierra et al. · 2021 [cited by applicant]
US 11299261B2 · Kerr · 2022 [cited by examiner]