Pneumatic deicer with sensors

Patent metadata

Field	Value
Publication number	US-2019016467-A1
Application number	US-201715650566-A
Country	US
Kind code	A1
Filing date	Jul 14, 2017
Priority date	Jul 14, 2017
Publication date	Jan 17, 2019
Grant date	—

Abstract

A pneumatic deicer includes a base layer, a forming layer, a first chamber, and a first sensor. The base layer has an inlet, a first side, and a second side. The forming layer is connected to the base layer along at least two seams and has inner side and an outer side with the outer side being distant from the base layer. The first chamber is formed between the base layer and the forming layer and configured to be inflated by air passing into the first chamber through the inlet in the base layer. The first sensor is situated within the first chamber.

First claim

1 . A pneumatic deicer comprising:
a base layer having an inlet, a first side, and a second side; a forming layer connected to the base layer along at least two seams, the forming layer having an inner side and an outer side with the outer side being distant from the base layer; a first chamber formed between the base layer and the forming layer and configured to be inflated by air passing into the first chamber through the inlet in the base layer; and a first sensor situated within the first chamber.

2 . The pneumatic deicer of claim 1 , wherein the first sensor is located on the first side of the base layer.

3 . The pneumatic deicer of claim 1 , wherein the first sensor is embedded in the first side of the base layer.

4 . The pneumatic deicer of claim 1 , wherein the first sensor is located on the inner side of the forming layer.

5 . The pneumatic deicer of claim 1 , wherein the first sensor is embedded in the inner side of the forming layer.

6 . The pneumatic deicer of claim 5 , further comprising:
a second sensor embedded in the first side of the base layer.

7 . The pneumatic deicer of claim 1 , further comprising:
an air line extending from an air source to the inlet in the base layer to provide air to inflate the forming layer to increase a volume of the first chamber; and a second sensor in the air line.

8 . The pneumatic deicer of claim 1 , wherein the first sensor measures a displacement of the forming layer relative to the base layer to determine at least one of an amount of inflation of the first chamber and a rate of inflation of the first chamber.

9 . The pneumatic deicer of claim 1 , wherein the first sensor measures at least one of a temperature of the air within the first chamber, a pressure of the air within the first chamber, and a humidity of the air within the first chamber.

10 . The pneumatic deicer of claim 1 , further comprising:
second chamber formed by the base layer and the forming layer and separated from the first chamber by a first seam of the at least two seams, the first seam including at least one passage to allow air to flow between the first chamber and the second chamber; and a second sensor within the second chamber.

11 . The pneumatic deicer of claim 10 , wherein air that is provided to the first chamber inflates the first chamber and the second chamber simultaneously.

12 . The pneumatic deicer of claim 1 , wherein the first sensor is at a first location and the pneumatic deicer further comprises:
a second sensor at a second location within the first chamber; a third sensor at a third location within the first chamber; and a fourth sensor at a fourth location within the first chamber.

13 . The pneumatic deicer of claim 1 , wherein the first sensor is a wireless sensor.

14 . The pneumatic deicer of claim 1 , wherein the first chamber formed by the base layer and the forming layer has an elongated shape.

15 . The pneumatic deicer of claim 1 , wherein a volume of the first chamber when the forming layer is deflated is less than a volume of the first chamber when the forming layer is inflated.

16 . A pneumatic deicer for an aircraft structure comprising:
a base layer adjacent to a structure prone to ice accumulation; a forming layer adjacent to the base layer; a first chamber between the base layer and the forming layer; a second chamber between the base layer and the forming layer; a first seam connecting the base layer to the forming layer and separating the first chamber from the second chamber; a first inlet in the base layer; a first air line extending from an air source to the first inlet, the first air line configured to provide air to inflate the first chamber to increase a volume of the first chamber; a first sensor situated within the first chamber; and a second sensor situated within the second chamber.

17 . The pneumatic deicer of claim 16 , wherein the first chamber is isolated from the second chamber and the pneumatic deicer further comprising:
a second inlet in the base layer adjacent the second chamber; and a second air line extending from an air source to the second inlet, the second air line configured to provide air to inflate the second chamber to increase a volume of the second chamber.

18 . The pneumatic deicer of claim 16 , further comprising:
at least one passage between the first chamber and the second chamber to allow air to flow from the first chamber into the second chamber to inflate the second chamber to increase a volume of the second chamber.

19 . The pneumatic deicer of claim 16 , further comprising:
a third chamber between the base layer and the forming layer; a second seam connecting the base layer to the forming layer and separating the first chamber from the third chamber; at least one passage between the first chamber and the third chamber to allow air to flow from the first chamber into the third chamber to inflate the forming layer to increase a volume of the third chamber; and a third sensor situated within the third chamber.

20 . The pneumatic deicer of claim 16 , wherein the first sensor is configured to measure at least one of a pressure of the air within the first chamber, a temperature of the air within the first chamber, a humidity of the air within the first chamber, a rate of inflation of the first chamber, and an amount of inflation of the first chamber.

Assignees

• Goodrich Corp

Inventors

• Botura Galdemir Cezar
• Brittingham David L
• Hu Jin
• Taylor Andrew

Classifications

• B64D15/166 Primary

  using pneumatic boots · CPC title

• F02C7/04

  Air intakes for gas-turbine plants or jet-propulsion plants · CPC title

• B64F5/60

  Testing or inspecting aircraft components or systems · CPC title

• F01D25/02

  De-icing means for engines having icing phenomena · CPC title