Escape slide with support tube assembly

• US 5,820,773 A
• Filed: 03/13/1997
• Issued: 10/13/1998
• Est. Priority Date: 03/13/1997
• Status: Expired due to Term

• Current Assignee: Goodrich Corporation (Rtx Corporation)
• Original Assignee: Goodrich Corporation (Rtx Corporation)
• Inventors: Hintzman, Roland Dwight, Melander, Clarence Sigurd
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US08/816,905
• Time in Patent Office: 579 Days
• Field of Search: 244/137.2, 244/905, 182/48, 193/25 B
• US Class Current: 244/137.2
• CPC Class Codes: B64D 25/14 Inflatable escape chutes

Abstract

An aircraft slide assembly used for evacuating personnel from an aircraft or other elevated structure having a longitudinally extending inflatable escape slide and a stabilizing support tube assembly attached to the underneath portion thereof closely adjacent the head end or upper end of the escape slide. The support tube has a first chamber and a second chamber with an orifice therebetween that allows inflation of the second chamber from the first chamber and thence allows the end wall of the first chamber to retract.

Claims

1. An inflatable escape slide for a structure comprising an elongated inflated slide having an upper surface portion and a lower surface portion;

said upper surface portion providing a slideway surface having sufficient strength upon inflation of said slide to support the weight of a load carried on said slideway surface;

said slide having a head end and a toe end;

inflatable cross member means extending laterally across the width of said slide and attached to the under surface of said slide;

an inflatable support tube assembly connected to the under surface of said slide close to said head end of said slide;

said support tube assembly having a pair of chambers;

one of said chambers being a first chamber and having an end wall located closely adjacent to said head end of said slide;

communication holes interconnecting said inflatable slide to said first chamber;

the second one of said pair of chambers spaced from said head end and extends in the direction towards said toe end;

orifice means interconnecting said chambers to inflate said second chamber only from said first chamber;

pressurizing means mounted on said slide and operative upon actuation to inflate said first chamber and said inflatable escape slide; and

said first chamber being operative upon inflation to initially move said end wall into contact with said structure and support said head end of said slide and then retracts said end wall after inflation of said second chamber.

2. An inflatable escape slide as set forth in claim 1 wherein said first chamber having an end portion remote from said second chamber defining said end wall, said second chamber having an end portion remote from said first chamber, and the surface area of said end portion of said second chamber being greater than the surface area of said end portion of said first chamber to define a differential piston area that aids in the retraction of said end wall of said first chamber upon full inflation of said second chamber.

3. An inflatable escape slide as set forth in claim 2 wherein a tension member extends through said first and second chamber and has its respective ends connected to said remote end portions of said first and second chambers to exert a retraction force on said first chamber as said second chamber is inflated.

4. An inflatable escape slide as set forth in claim 3 wherein the overall length of said support tube assembly is greater then the length of said tension member.

5. An inflatable escape slide as set forth in claim 4 wherein said tension member is an elongated nylon cord that extends through a common wall located between said first chamber and said second chamber.

6. An inflatable escape slide as set forth in claim 5 wherein said tension member extends through said orifice means that interconnects said chambers.

7. An inflatable escape slide for an aircraft comprising an elongated inflatable slide member having an upper slide surface and a lower under surface;

said slide member having a head end and a toe end;

an inflatable support tube assembly connected to the under surface of said slide member and located at said head end of said slide member;

said support tube assembly being compartmentalized with a first compartment located at said head end and a second compartment spaced from said head end and extending in the direction towards said toe end;

said first compartment having one end wall;

pressurizing means mounted on said slide member and operative upon actuation to inflate said inflatable slide member and said one compartment through communication holes;

orifice means interconnecting said first compartment to said second compartment to provide pressurization from said one compartment to said second compartment; and

said secondary compartment configured to retract said one end wall of said first compartment when said second compartment is fully inflated.

8. An inflatable escape slide as set forth in claim 7 wherein a common wall is shared between said one compartment and said second compartment;

and the oppositely disposed end areas of said one compartment to said second compartment provides a greater piston surface area on the oppositely disposed end area of said second compartment to provide a greater force acting on said compartments in a direction away from said head end to facilitate the retraction of said end wall of said first compartment.

9. An inflatable escape slide as set forth in claim 8 wherein said oppositely disposed area of said one compartment defines a first piston area, said oppositely disposed area of said second compartment defines a second piston area;

and said piston areas are interconnected by a tension member whose length is less than the overall length of said inflatable support tube assembly to aid in the retraction of said first piston area of said first compartment away from said aircraft.

10. An aircraft escape slide comprising an inflatable slide member;

said slide member in the inflated condition having a head end and a toe end;

said head end releasably secured to said aircraft adjacent to an egress door upon deployment of said inflatable slide member;

said slide member having an upper surface portion and a lower surface portion;

said upper surface portion providing a slideway surface for the discharge of aircraft passengers and crew members;

said slide member including a plurality of longitudinally extending tube members and laterally extending tube members communicating with each other to permit inflation thereof;

an elongated positioning tube located on the lower surface portion of said slide member;

said positioning tube having a pair of longitudinally spaced chamber;

one of said chambers being closely adjacent to said head end defining a first chamber;

the remaining one of said pair of chambers being spaced from said head end defining a second chamber;

a common wall between said chambers;

said common wall having an orifice for directing the passage of pressurized gas from said first chamber to said second chamber;

said first chamber having an end wall that is adapted to engage a portion of said aircraft adjacent to said egress door;

said second chamber having an end wall spaced from said common wall and said head end;

said end wall of said second chamber having a greater surface area than said end wall of said first chamber to provide a differential piston area between said first and second chambers; and

said first chamber operative to inflate said second chamber and retract said end wall of said first chamber.

11. An aircraft life raft escape slide as set forth in claim 10 wherein a tension member interconnects said end walls of said first and second chambers;

and the overall length of said positioning tube is greater than the length of said tension member to thereby direct said tension member to aid in the retraction of said end wall of said first chamber.