Sewn alternate inflate pneumatic de-icer

Patent metadata

Field	Value
Publication number	US-10780983-B2
Application number	US-201715845428-A
Country	US
Kind code	B2
Filing date	Dec 18, 2017
Priority date	Dec 18, 2017
Publication date	Sep 22, 2020
Grant date	Sep 22, 2020

Abstract

A de-icing assembly for a surface of an aircraft includes a carcass with a first layer and a second layer, a plurality of seams sewn into the carcass, and a bonded region. The plurality of seams join the first and second layers of the carcass together. Each of the plurality of seams comprises two or more stitchlines. The bonded region is disposed between the two or more stitchlines and seals a portion of the first layer of the carcass to a portion of the second layer of the carcass.

First claim

The invention claimed is:

1. A de-icing assembly for a surface of an aircraft, the de-icing assembly comprising:
a carcass with a first layer and a second layer;
a plurality of seams sewn into the carcass, wherein the plurality of seams joins the first and second layers of the carcass together, wherein each of the plurality of seams comprises two or more stitchlines;
a bonded region disposed between the two or more stitchlines of the plurality of seams, wherein the bonded region seals a portion of the first layer of the carcass to a portion of the second layer of the carcass; and
first and second sets of inflatable pockets each defined by the plurality of seams and by the bonded region, wherein the first set of inflatable pockets and the second set of inflatable pockets are disposed between the first and second layers of the carcass.

2. The de-icing assembly of claim 1 , wherein the bonded region prevents communication of a fluid across the bonded region.

3. The de-icing assembly of claim 1 , wherein the first and second sets of inflatable pockets are separately inflatable from each other.

4. The de-icing assembly of claim 1 , further comprising:
a first manifold fluidly connected to the first set of inflatable pockets, wherein the first manifold provides fluid to inflate the first set of inflatable pockets; and
a second manifold fluidly connected to the second set of passages, wherein the second manifold provides fluid to inflate the second set of inflatable pockets.

5. The de-icing assembly of claim 1 , wherein the first layer includes a first rubber coating, wherein the second layer includes a second rubber coating, wherein the first rubber coating faces towards the second rubber coating, wherein the second rubber coating faces towards the first rubber coating, and wherein a portion of the first rubber coating is in contact with a portion of the second rubber coating at the bonded region.

6. The de-icing assembly of claim 5 , wherein the bonded region comprises a vulcanized cross-link between the first and second rubber coatings.

7. The de-icing assembly of claim 1 , wherein the de-icing assembly comprises a pneumatic de-icer.

8. The de-icing assembly of claim 1 , wherein the de-icing assembly is configured to mount to at least one of a horizontal stabilizer of a wing, an upper surface of the wing, and a tail section of the aircraft.

9. A pneumatic de-icing assembly for an aircraft, the pneumatic de-icing assembly the comprising:
an array of pneumatically inflatable pockets arranged in a side-by-side configuration; and
a seam between adjacent pockets, the seam including a set of parallel stitchlines and a bond extending parallel to and positioned between the stitchlines, wherein the pneumatically inflatable pockets are formed by the bond and by the parallel stitchlines, the seam separating and sealing between the adjacent pockets so that the adjacent pockets are separably inflatable and deflatable.

10. The pneumatic de-icing assembly of claim 9 , further comprising:
a carcass with a first layer and a second layer, wherein the array of pneumatically inflatable pockets is disposed between the first and second layer of the carcass.

11. The pneumatic de-icing assembly of claim 10 , wherein the array of pneumatically inflatable pockets comprises a first set of inflatable pockets and a second set of inflatable pockets, wherein the first and second sets of inflatable pockets are formed by the seam, wherein the first and second sets of inflatable pockets are separately inflatable from each other.

12. The pneumatic de-icing assembly of claim 10 , wherein the first layer includes a first rubber coating, wherein the second layer includes a second rubber coating, wherein the first rubber coating faces towards the second rubber coating, wherein the second rubber coating faces towards the first rubber coating, wherein a portion of the first rubber coating is in contact with a portion of the second rubber coating at the bond, and wherein the bond comprises a vulcanized cross-link between the first and second rubber coatings.

13. A method of making a de-icer, the method comprising:
bringing together a first layer of a carcass and a second layer of the carcass such that a first rubber coating on the first layer faces a second rubber coating on the second layer;
sewing a plurality of seams into the carcass, wherein each of the plurality of seams comprises two or more stitchlines, wherein sewing a plurality of seams into the carcass comprises forming a first set of inflatable pockets and a second set of inflatable pockets, wherein the first set of inflatable pockets and the second set of inflatable pockets are disposed between the first and second layers of the carcass; and
bonding the first layer to the second layer, wherein a bond is formed between the stitchlines, wherein the inflatable pockets are formed by the bond and by the stitchlines.

14. The method of claim 13 , wherein bonding the first and second layers of the carcass together comprises creating a fluidic seal between the first and second layers of the carcass.

15. The method of claim 13 , wherein bonding the first and second layers of the carcass together comprises vulcanizing the first rubber coating of the first layer to the second rubber coating of the second layer.

16. The method of claim 13 , further comprising inserting a piece of fabric between the first and second layers before the first and second layers are bonded, wherein the piece of fabric prevents the first and second layers from bonding at a location where the piece of fabric is located relative to the first and second layers.

17. The method of claim 13 , further comprising applying at least one of a non-reactive chemical powder and a non-reactive chemical slurry to at least one of the first and second layers before the first and second layers are bonded, wherein the at least one of the non-reactive chemical powder and the non-reactive chemical slurry prevents the first and second layers from bonding at a location where the at least one of the non-reactive chemical powder and the non-reactive chemical slurry is located relative to the first and second layers.

18. The method of claim 13 , further comprising imparting a surface pattern onto at least one of the first and second layers with a tool before the first and second layers are bonded, wherein the surface pattern prevents the first and second layers from bonding at a location where the surface pattern is located relative to the first and second layers.

Assignees

• Goodrich Corp

Inventors

• Hunter James R
• Botura Galdemir Cezar
• Schomer Samual Steven Riczo
• Fahrner Alan J
• Tauscher Kurt M

Classifications

• B64D15/166 Primary

  using pneumatic boots · CPC title

• B32B7/08

  by mechanical means · CPC title

• B32B2605/18

  Aircraft · CPC title

• B32B2250/02

  2 layers · CPC title