Evacuation system with an extendable head end

Patent metadata

Field	Value
Publication number	US-10611489-B2
Application number	US-201715603897-A
Country	US
Kind code	B2
Filing date	May 24, 2017
Priority date	May 24, 2017
Publication date	Apr 7, 2020
Grant date	Apr 7, 2020

Abstract

An evacuation slide assembly for an aircraft may comprise a main body configured to extend from a sill of the aircraft toward a surface within a range of angles relative to vertical when deployed so as to allow persons to safely slide down the main body to the surface. The main body may include a head end configured to attached to the sill of the aircraft, and a toe end opposite the head end. A first extendable portion may be coupled to the head end of the main body and may be in operable communication with a height sensor. The first extendable portion may be configured to deploy to adjust for a variation in a positional relationship between the surface and the sill to maintain the main body within the range of angles.

First claim

What is claimed is:

1. An evacuation slide assembly for an aircraft, comprising:
a main body including a head end configured to attached to a sill of the aircraft, and a toe end opposite the head end, the main body being configured to extend from the sill of the aircraft toward a surface within a range of angles relative to vertical when deployed so as to allow persons to safely slide down the main body to the surface;
a first extendable portion coupled to the head end of the main body;
a height sensor in operable communication with the first extendable portion, the height sensor being configured to determine at least one of a roll angle of the aircraft, a pitch angle of the aircraft, or an angle of the main body relative to vertical, wherein the height sensor is configured to determine a distance between the sill of the aircraft and the surface based on the at least one of the roll angle of the aircraft, the pitch angle of the aircraft, or the angle of the main body relative to vertical, and wherein the first extendable portion is configured to deploy to adjust for a variation in a positional relationship between the surface and the sill to maintain the main body within the range of angles.

2. The evacuation slide assembly of claim 1 , further comprising a first cutter configured to actuate and release the first extendable portion in response to the height sensor determining at least one of the distance between the sill and the surface, the roll angle of the aircraft, the pitch angle of the aircraft, or the angle of the main body relative to vertical exceeds a first threshold.

3. The evacuation slide assembly of claim 2 , wherein the first cutter comprises a first knife edge and a second knife edge, the first knife edge configured to be driven towards the second knife edge in response to actuation of the first cutter.

4. The evacuation slide assembly of claim 2 , wherein the first cutter comprises a pyrotechnic package.

5. The evacuation slide assembly of claim 2 , further including:
a second extendable portion coupled to the main body; and
a second cutter configured to actuate and release the second extendable portion in response to the height sensor determining the at least one of the distance between the sill and the surface, the roll angle of the aircraft, the pitch angle of the aircraft, or the angle of the main body relative to vertical exceeds a second threshold different from the first threshold.

6. The evacuation slide assembly of claim 2 , further comprising:
at least one thread configured to lace a first segment and a second segment of the first extendable portion together; and
a pin coupled to the first cutter, wherein the pin is coupled to the at least one thread and configured to loosen the at least one thread to allow the first extendable portion to extend.

7. The evacuation slide assembly of claim 6 , wherein the first extendable portion includes an extendable tube in fluid communication with the main body and configured to receive pressurized air from the main body and inflate in response to the at least one thread being loosened.

8. The evacuation slide assembly of claim 7 , wherein:
the first segment of the first extendable portion comprises a first distal end and a first proximal end opposite the first distal end;
the second segment of the first extendable portion comprises a second distal end and a second proximal end opposite the second distal end; and
the first distal end is configured to be adjacent the second distal end when the first extendable portion is in a packed state and to be distal the second distal end when the first extendable portion is in an extended state.

9. The evacuation slide assembly of claim 8 , wherein:
the first distal end and the second distal end each define a plurality of openings;
the at least one thread is configured to extend through each of the plurality of openings and form corresponding loops in a first direction;
each loop is configured to be threaded through an adjacent loop; and
a last loop is configured to be coupled to the pin such that the pin releases the last loop in response to actuation of the first cutter.

10. An evacuation system for an aircraft, comprising:
an evacuation slide assembly comprising:
a main body including a head end configured to attached to a sill of the aircraft, and a toe end configured to extend toward a surface when the main body is deployed, and
an extendable portion coupled to the main body,

a height sensor configured to determine a sill height based on at least one of a roll angle of the aircraft, a pitch angle of the aircraft, or an angle of the main body relative to vertical, and wherein the height sensor is configured output an electrical signal in response to the height sensor determining at least one of the sill height, the roll angle of the aircraft, the pitch angle of the aircraft, or the angle of the main body relative to vertical exceeds a predetermined threshold; and
a release mechanism electrically coupled to the height sensor and configured to actuate in response to receiving the electrical signal output from the height sensor.

11. The evacuation system of claim 10 , wherein the extendable portion comprises an extendable tube in fluid communication with the main body and configured to receive pressurized air from the main body.

12. The evacuation system of claim 11 , wherein the extendable portion further comprises:
a first segment having a first distal end and a first proximal end opposite the first distal end; and
a second segment having a second distal end and a second proximal end opposite the second distal end, wherein the first distal end is configured to be adjacent the second distal end when the extendable portion is in a packed state and to be distal the second distal end when the extendable portion is in an extended state.

13. The evacuation system of claim 12 , wherein:
the first distal end and the second distal end each define a plurality of openings;
at least one thread is configured to extend through each of the plurality of openings and form corresponding loops in a first direction;
each loop is configured to be threaded through an adjacent loop; and
a last loop is coupled to a pin.

14. The evacuation system of claim 13 , wherein the pin is coupled to the release mechanism.

15. The evacuation system of claim 10 , wherein the release mechanism comprises a cutter including a first knife edge and a second knife edge, the first knife edge configured to be driven towards the second knife edge in response to actuation of the cutter.

16. The evacuation system of claim 10 , wherein the release mechanism comprises a pyrotechnic package.

17. An evacuation system for an aircraft, comprising:
an evacuation slide assembly comprising:
a main body having a head end and a toe end, the head end being configured to be nearer the aircraft than the toe end when the evacuation slide assembly is deployed, wherein the toe end is configured to extend toward a surface when the main body is deployed;
an extendable portion in operable communication with the main body and configured to alter an angle of the main body relative to vertical when the evacuation slide assembly is deployed such that the angle is maintained within a selected range; and
a height sensor configured to determine a distance between the head end and the surface based on at least one of a roll angle of the aircraft, a pitch angle of the aircraft, or the angle of the main body relative to vertical, wherein the height sensor is configured output an electrical signal in response to the

Assignees

• Goodrich Corp

Inventors

• Bahena Daniel
• Haynes Timothy C

Classifications

• B64D25/14 Primary

  Inflatable escape chutes · CPC title

• B64D25/18

  Flotation gear · CPC title