Pressure relief latch

Patent metadata

Field	Value
Publication number	US-12448140-B2
Application number	US-202318141855-A
Country	US
Kind code	B2
Filing date	May 1, 2023
Priority date	May 1, 2023
Publication date	Oct 21, 2025
Grant date	Oct 21, 2025

Abstract

A pressure relief latch includes a housing, a bolt, a cam, and a spring assembly. The housing includes a door panel, a first lateral panel, and a second lateral panel. The first lateral panel and the second lateral panel extend outward from the door panel. The bolt includes a bolt body and a roller bearing. The bolt body is pivotably mounted to the first lateral panel and the second lateral panel at a bolt pivot axis. The bolt body is pivotable about the bolt pivot axis between a latched position and an unlatched position. The roller bearing is rotatably mounted to the bolt body. The cam is pivotably mounted to the first lateral panel and the second lateral panel. The spring assembly is pivotably mounted to the cam. The spring assembly is configured to bias the cam toward the bolt.

First claim

What is claimed is:

1. A pressure relief latch comprising:
a housing including a door panel, a first lateral panel, and a second lateral panel, the door panel forms a bolt slot, and the first lateral panel and the second lateral panel extend outward from the door panel;
a bolt including a bolt body and a roller bearing, the bolt body is pivotably mounted to the first lateral panel and the second lateral panel at a bolt pivot axis, the bolt body is pivotable about the bolt pivot axis between a latched position and an unlatched position, the bolt body is configured to pass through the bolt slot between the latched position and the unlatched position, the bolt body includes a first lateral side wall, a second lateral side wall, and a laterally-extending wall forming a cavity, the laterally-extending wall extends between and to the first lateral side wall and the second lateral side wall, the roller bearing is rotatably mounted to the first lateral side wall and the second lateral side wall about a rotational axis, and the roller bearing is disposed within the cavity;
a cam pivotably mounted to the first lateral panel and the second lateral panel at a first cam pivot axis, the cam includes a first surface portion, a second surface portion, and an actuation edge, and the first surface portion intersects the second surface portion at the actuation edge; and
a spring assembly pivotably mounted to the cam at a second cam pivot axis, the spring assembly is configured to bias the cam toward the bolt with the cam first surface portion positioned in contact with the roller bearing and the second surface portion positioned in contact with the laterally-extending wall in the latched position of the bolt body.

2. The pressure relief latch of claim 1 , wherein the first surface portion has a concave shape and the second surface portion has a convex shape.

3. The pressure relief latch of claim 1 , wherein the actuation edge has a substantially orthogonal shape.

4. The pressure relief latch of claim 1 , wherein the spring assembly includes a shaft, a trunnion, and a spring, the shaft is pivotably mounted to the cam about the second cam pivot axis, the trunnion is pivotably mounted to the first lateral panel and the second lateral panel at a trunnion pivot axis, the shaft is mounted to the trunnion, the spring extends circumferentially about the shaft and the trunnion.

5. The pressure relief latch of claim 4 , wherein the shaft is movably mounted to the trunnion such that the shaft is configured to translate relative to and within the trunnion.

6. The pressure relief latch of claim 4 , wherein the spring assembly further includes an adjustment nut, the adjustment nut is selectively positionable on the trunnion, the spring is compressed against the adjustment nut.

7. The pressure relief latch of claim 4 , wherein the roller bearing is configured to push the cam to compress the spring as the bolt body pivots from the latched position to the unlatched position.

8. A propulsion system for an aircraft, the propulsion system comprising:
a cowl forming a compartment;
a pressure relief door pivotably mounted to the cowl, the pressure relief door is pivotable between a closed position and an open position, and the pressure relief door further forms the compartment; and
a pressure relief latch including a housing, a bolt, a cam, and a spring assembly,
the housing includes a door panel, a first lateral panel, and a second lateral panel, the door panel is mounted to the pressure relief door, and the first lateral panel and the second lateral panel extend outward from the door panel;
the bolt includes a bolt body and a roller bearing, the bolt body is pivotably mounted to the first lateral panel and the second lateral panel at a bolt pivot axis, the bolt body is pivotable about the bolt pivot axis between a latched position and an unlatched position, in the latched position, the bolt body is configured to contact the cowl, the bolt body includes a first lateral side wall, a second lateral side wall, and a laterally-extending wall forming a cavity, the laterally-extending wall extends between and to the first lateral side wall and the second lateral side wall, the roller bearing is rotatably mounted to the first lateral side wall and the second lateral side wall about a rotational axis, and the roller bearing is disposed within the cavity;
the cam is pivotably mounted to the first lateral panel and the second lateral panel at a first cam pivot axis, the cam includes a first surface portion, a second surface portion, and an actuation edge, and the first surface portion intersects the second surface portion at the actuation edge; and
a spring assembly pivotably mounted to the cam at a second cam pivot axis, the spring assembly including a spring biasing the cam toward the bolt with the first surface portion positioned in contact with the roller bearing and the second surface portion positioned in contact with the laterally-extending wall in the latched position of the bolt body.

9. The propulsion system of claim 8 , wherein:
the bolt body extends between and to a first longitudinal side and a second longitudinal side, the bolt body includes a first engagement surface and a second engagement surface, the first engagement surface is disposed at the first longitudinal side, the second engagement surface is disposed at the second longitudinal side;
in the latched position of the bolt body, the first engagement surface is configured to contact the cowl and the second engagement surface is configured to be disposed at the pressure relief door.

10. The propulsion system of claim 8 , wherein the bolt body is configured to pass through the pressure relief door as the bolt body pivots from the latched positioned to the unlatched position.

11. The propulsion system of claim 8 , wherein the roller bearing is positioned to push the cam to compress the spring as the roller bearing rolls along the first surface portion to the actuation edge.

12. The propulsion system of claim 8 , wherein the actuation edge has a substantially orthogonal shape.

13. The propulsion system of claim 8 , wherein the first surface portion has a concave shape and the second surface portion has a convex shape.

14. The propulsion system of claim 8 , wherein the spring assembly includes a shaft and a trunnion, the shaft is pivotably mounted to the cam about the second cam pivot axis, the trunnion is pivotably mounted to the first lateral panel and the second lateral panel at a trunnion pivot axis, the shaft is mounted to the trunnion, the spring extends circumferentially about the shaft and the trunnion.

15. The propulsion system of claim 14 , wherein the shaft is movably mounted to the trunnion such that the shaft is configured to translate relative to and within the trunnion.

16. The propulsion system of claim 14 , wherein the spring assembly further includes an adjustment nut, the adjustment nut is selectively positionable on the trunnion, the spring is compressed against the adjustment nut.

17. The propulsion system of claim 8 , wherein the roller bearing is configured to push the cam to compress the spring as the bolt body pivots from the latched position to the unlatched position.

Assignees

• Rohr Inc

Inventors

• Mcmahan Paul F
• Phillips Braskel

Classifications

• E05C3/30

  in the form of a hook {(hook-like fastenings E05C19/10; locks for sliding wings with pivoting bolts E05B65/0811, E05B65/0835)} · CPC title

• E05C3/122

  flush · CPC title

• E05B51/023

  actuated in response to external pressure, blast or explosion (E05B65/102 takes precedence) · CPC title

• B64C2001/009

  comprising decompression panels or valves for pressure equalisation in fuselages or floors · CPC title

• B64D29/06 Primary

  Attaching of nacelles, fairings or cowlings · CPC title