Evacuation slide systems

• US 8,215,586 B2
• Filed: 04/08/2009
• Issued: 07/10/2012
• Est. Priority Date: 04/08/2009
• Status: Active Grant

• Current Assignee: Air Cruisers Company LLC (Safran SA)
• Original Assignee: Air Cruisers Company LLC (Safran SA)
• Inventors: O'Donnell, John, Brown, Frank, Luethi, Andreas
• Primary Examiner(s): Brown, Peter R.
• Application Number:
  US12/384,703
• Publication Number:
  US 20100258677A1
• Time in Patent Office: 1,189 Days
• Field of Search: 244/137.1, 244/137.2, 244/905, 182/48
• US Class Current: 244/137.2
• CPC Class Codes: B64D 25/14 Inflatable escape chutes

Abstract

Evacuation slide systems having extendable portions are detailed. The extendable portions of slides may be inflated separately from the main portions and actuated manually if desired. Consequently, attitude changes of, for example, an aircraft subsequent to inflation of the main portion of a slide would not necessarily defeat its use, as inflation of the extendable portion could still occur.

Claims

1. An evacuation slide system comprising:

a. an inflatable slide comprising;

i. a main portion having a length;

ii. an extension portion integrally formed with the main portion so as to extend the length thereof when inflated without creating an external seam at a boundary of the main and extension portions; and

iii. at least one internal bulkhead generally precluding fluid communication between the main portion and the extension portion; and

b. means for inflating the extension portion separately from the main portion.

2. An evacuation slide system according to claim 1 in which the inflating means comprises (a) an automatic actuator for inflating the main portion and (b) a manual actuator for inflating the extension portion after inflation of the main portion.

3. An evacuation slide system according to claim 1 in which the main portion comprises a first upper tube and the extension portion comprises an integral continuation of the first upper tube.

4. An evacuation slide system according to claim 3 in which the bulkhead is positioned within the first upper tube so as to define the boundary.

5. An evacuation slide system according to claim 4 in which the extension portion, when uninflated, folds adjacent the main portion.

6. An evacuation slide system according to claim 5 in which the main portion has a head end configured for attachment to an aircraft and a foot end adjacent the extension portion and further comprises:

a. a second upper tube;

b. a first transverse tube between the first and second upper tubes; and

c. a second transverse tube between the first and second upper tubes and adjacent the foot end.

7. An evacuation slide system according to claim 6 in which the main portion further comprises first and second lower tubes supporting and extending generally parallel to the first and second upper tubes, respectively.

8. An evacuation slide system according to claim 7 in which the extension portion further comprises first and second lower extension tubes.

9. An evacuation slide system according to claim 8 in which the extension portion (a) defines an extended foot end and (b) further comprises a third transverse tube.

10. An evacuation slide system according to claim 9 further comprising a containment wrapper attached to the main portion, the containment wrapper functioning to assist in retaining the extension portion in a predetermined position relative to the main portion prior to deployment of the extension portion.

11. An evacuation slide system according to claim 10 in which the containment wrapper comprises first and second ends, at least one of which is removably attached to the main portion.

12. An evacuation slide system according to claim 11 further comprising a passenger-sliding surface, comprising at least one panel, extending between the first and second upper tubes.

13. An evacuation slide system according to claim 12 in which the first end of the containment wrapper is removably attached to the panel.

14. An evacuation slide system according to claim 13 in which the inflation means further comprises an aspirator and an inflation tube communicating therewith.

15. An evacuation slide system according to claim 14 in which the inflation tube also communicates with the extension portion so as to convey inflation fluid thereto.

16. An evacuation slide system according to claim 12 in which at least portions of both the containment wrapper and the passenger-sliding surface are coated with the same friction-increasing agent so as to decelerate sliding passengers in approximately the same manner.