Aircraft evacuation slide

• US 10,000,291 B2
• Filed: 09/24/2015
• Issued: 06/19/2018
• Est. Priority Date: 09/24/2015
• Status: Active Grant

• Current Assignee: Goodrich Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Goodrich Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Prevost, Craig Erwin, Evans, Steven
• Primary Examiner(s): Woldemaryam, Assres H
• Application Number:
  US14/864,688
• Publication Number:
  US 20170088273A1
• Time in Patent Office: 999 Days
• CPC Class Codes: B64D 25/14 Inflatable escape chutes

Abstract

According to various embodiments, disclosed is a slide configured to be supported on a ground surface at a slide angle, comprising a support structure, a sliding surface supported by the support structure, and a weakened support region in the support structure, wherein the weakened support region enables the slide to buckle and the slide angle to change in response to a bending load imposed on the slide. According to various embodiments, the slide is an aircraft evacuation slide.

Claims

1. An aircraft slide comprising:

a support structure comprising a first slide rail, a second slide rail, and a ground rail;

a sliding surface supported by the support structure; and

a bend region formed in the support structure and comprising a first diameter, the bend region defining an upper tube region of the support structure above the bend region and a lower tube region of the support structure below the bend region, wherein the upper tube region comprises a second diameter that is greater than the first diameter and is generally uniform throughout the upper tube region and the lower tube region comprises a third diameter that is greater than the first diameter and is generally uniform throughout the lower tube region, wherein the bend region is located between the ground rail and a midpoint of the aircraft slide, the midpoint of the aircraft slide being halfway between the ground rail and a top of the aircraft slide opposite the ground rail, and wherein

the aircraft slide is configured to be supported on a ground surface at a slide angle relative to the ground surface, the bend region enabling the support structure to bend and the slide angle of the lower tube region to change in response to a bending load imposed on the lower tube region.

2. The aircraft slide of claim 1, further comprising a lower support having a U-shape configuration and configured to extend from the support structure toward the ground surface, wherein the lower support is located between the bend region and the midpoint of the aircraft slide.

3. The aircraft slide of claim 1, wherein the aircraft slide is an inflatable slide used for emergency evacuation of an aircraft and configured to be packed within a compartment of the aircraft.

4. The aircraft slide of claim 1, wherein the support structure is in bordering engagement with the sliding surface, and wherein the support structure is inflatable.

5. The aircraft slide of claim 1,

wherein the first slide rail and the second slide rail boarder opposite sides of the sliding surface, and the ground rail boarders a bottom side of the sliding surface,

wherein the ground rail is coupled between the first slide rail and the second slide rail, and

wherein the first slide rail, the second slide rail, and the ground rail form a continuous air filled tube when the support structure is inflated.

6. The aircraft slide of claim 1, wherein, the bend region further comprises:

a first bend region on the first slide rail, and

a second bend region, corresponding to the first bend region, on the second slide rail opposite the first bend region.

7. The aircraft slide of claim 1, wherein the bend region of the support structure comprises:

a middle tapered region comprising the first diameter;

an upper tapering segment extending radially inwards from to the upper tube region of the support structure to the middle tapered region; and

a lower tapering segment extending radially inwards from the lower tube region of the support structure to the middle tapered region.

8. The aircraft slide of claim 1, wherein the bend region is located approximately halfway between the midpoint of the aircraft slide and the ground rail.

9. The aircraft slide of claim 1, further comprising a lower support located between the bend region and the midpoint of the aircraft slide, wherein the lower support contacts the ground surface when the slide angle is 36°

or less and is located off of the ground surface when the slide angle is greater than 36°

.

10. The aircraft slide of claim 9, wherein the lower support comprises a ground support bar and vertical posts, wherein the ground support bar is integrally coupled between the vertical posts, wherein the vertical posts are coupled to the support structure.

11. An aircraft slide comprising:

a support structure comprising a ground rail configured to support the aircraft slide on a ground surface;

a sliding surface supported by the support structure; and

a bend region in the support structure, the bend region comprising a first diameter, wherein

the bend region defines a lower region of the support structure and an upper region of the support structure above the bend region, the lower region of the support structure comprising a second diameter greater than the first diameter of the bend region and the upper region of the support structure comprising a third diameter greater than the first diameter, the bend region being located between the lower region and a midpoint of the aircraft slide along a length of the aircraft slide, and wherein

the support structure is configured to bend at the bend region and change an angle of the lower region of the support structure with respect the ground surface in response to a bending load being imposed on the lower region of the support structure, and wherein when the angle of the lower region of the support structure with respect the ground surface is less than 20°

the angle increases in response to the bending load being imposed on the lower region of the support structure, and wherein when the angle of the lower region of the support structure with respect the ground surface is greater than 36°

, the angle decreases in response to the bending load being imposed on the lower region of the support structure.

12. The aircraft slide of claim 11, wherein the bend region is located between the ground rail and the midpoint of the aircraft slide, the midpoint of the aircraft slide being halfway between the ground rail and a top of the aircraft slide opposite the ground rail.

13. The aircraft slide of claim 12, wherein the support structure further comprises a lower support rail located between the bend region and the midpoint of the aircraft slide.