Insulating a protective cover for a seal to sensor associated with a spacesuit

• US 10,791,962 B2
• Filed: 01/26/2017
• Issued: 10/06/2020
• Est. Priority Date: 01/26/2017
• Status: Active Grant

• Current Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Murray, Sean K., Avalone, Robert G., Quinn, Gregory John
• Primary Examiner(s): Huls, Natalie
• Application Number:
  US15/415,993
• Publication Number:
  US 20180206765A1
• Time in Patent Office: 1,349 Days
• CPC Class Codes: A61B 5/082 Evaluation by breath analysis, e.g. determination of the chemical composition of exhaled breath A61B5/083, A61B5/091 take precedence
• CPC Class Codes: A61B 5/097 Devices for facilitating collection of breath or for directing breath into or through measuring devices
• CPC Class Codes: B64G 6/00 Space suits
• CPC Class Codes: G01N 21/3504 for analysing gases, e.g. multi-gas analysis
• CPC Class Codes: G01N 2201/021 Special mounting in general
• CPC Class Codes: G01N 2201/0231 Thermostating
• CPC Class Codes: G01N 33/004 for CO, CO2

Abstract

A carbon dioxide sensor has a conduit connecting to a source of breathing air and delivering a sample of breathing air into a test chamber. A radiation source applies radiation across the chamber. A sensor detects modification in the radiation as it passes through the air sample in the test chamber and communicates with electronics to identify a percentage of carbon dioxide in the sample. A rigid cover surrounds the radiation source, the test chamber, and the sensor. A spacesuit is also disclosed.

Claims

1. A carbon dioxide sensor comprising:

a conduit connecting to a source of breathing air and delivering a sample of breathing air into a test chamber;

a radiation source for applying radiation across said chamber and a sensor for detecting modification in the radiation as it passes through the air sample in the test chamber and communicating with electronics to identify a percentage of carbon dioxide in the sample; and

a rigid cover surrounding said radiation source, said test chamber, and said sensor; and

wherein said cover has a first portion surrounding said radiation source, said test chamber and said sensor, and a second portion that encloses a connection point for said conduit to be connected to the source of breathing air.

2. The carbon dioxide sensor as set forth in claim 1, wherein said radiation source is an infrared source.

3. The carbon dioxide sensor as set forth in claim 1, wherein an inner surface of said cover facing said sensor has greater reflectivity to infrared radiation than does an outer surface of said cover.

4. The carbon dioxide sensor as set forth in claim 3, wherein said outer surface of said cover is formed by a first material and said inner surface of said cover is formed by a second material.

5. The carbon dioxide sensor as set forth in claim 4, wherein said inner surface is provided by a polished metal.

6. The carbon dioxide sensor as set forth in claim 3, wherein said inner surface is one of nickel, aluminum, or gold.

7. The carbon dioxide sensor as set forth in claim 3, wherein said inner surface is provided by a polished metal.

8. A spacesuit comprising:

a suit;

a source of breathing air and a conduit delivering a sample of the breathing air into a test chamber of a CO₂ sensor;

said CO2 sensor being within said suit, said CO2 sensor also including a radiation source for applying radiation across said chamber and a sensor for detecting modification in the radiation as it passes through the air sample in the test chamber and communicating with electronics to identify a particular percentage of carbon dioxide in the sample;

a rigid cover surrounding said radiation source, said test chamber, and said sensor;

wherein there is a port adjacent to said carbon dioxide sensor for expelling fluid from within said spacesuit; and

wherein said port has a hydraulic diameter, and a distance between an outer edge of said port, and a closest portion of said carbon dioxide sensor is less than said hydraulic diameter.

9. The spacesuit as set forth in claim 8, wherein said radiation source is an infrared source.

10. The spacesuit as set forth in claim 9, wherein an inner surface of said cover facing said sensor has greater reflectivity to infrared radiation than does an outer surface of said cover.

11. The spacesuit as set forth in claim 10, wherein said inner surface is provided by a polished metal.

12. The spacesuit as set forth in claim 8, wherein an inner surface of said cover facing said sensor has greater reflectivity to infrared radiation than does an outer surface of said cover.

13. The spacesuit as set forth in claim 12, wherein said outer surface of said cover is formed by a first material and said inner surface of said cover is formed by a second material.

14. The spacesuit as set forth in claim 13, wherein said inner surface is provided by a polished metal.

15. The spacesuit as set forth in claim 12, wherein said inner surface is one of nickel, aluminum, or gold.

16. The spacesuit as set forth in claim 12, wherein said inner surface is provided by a polished metal.