In mask sensor system

Patent metadata

Field	Value
Publication number	US-12085507-B2
Application number	US-202117645026-A
Country	US
Kind code	B2
Filing date	Dec 17, 2021
Priority date	Dec 17, 2020
Publication date	Sep 10, 2024
Grant date	Sep 10, 2024

Abstract

An in-situ sensor system that is configured to be placed inside of an oxygen mask for a pilot. The sensor system is readily placed in a position over the exhalation valve such that it can capture data from the exhaled air of the pilot. The sensor system has an optical sensor element that can capture data real time and feed the data to a control module that can subsequently be use to generate output data for the pilot and/or ground elements.

First claim

What is claimed is:

1. An in-situ sensor system comprising
a main housing, wherein the main housing is configured to cooperatively engage with an exhalation valve of an oxygen mask configured with a voluminous breathing chamber and wherein the main housing has an opening disposed therein that corresponds with an opening in the exhalation valve of the mask, and is disposed within the voluminous breathing chamber,
an optical transmitter housing disposed on the main housing and configured to house an optical transmitter element,
an optical receiver housing disposed on the main housing and configured to house an optical receiver element, and
wherein the optical transmitter element is optically aligned with the optical receiver element such that a signal path between the optical transmitter element and the optical receiver element transects the opening in the main housing such that exhaled air from a user of the mask will pass through the signal path as it is pushed through the exhalation valve.

2. The in-situ sensor system of claim 1 , wherein the optical transmitter element is a laser.

3. The in-situ sensor system of claim 2 , wherein the laser is a tunable laser.

4. The in-situ sensor system of claim 3 , wherein the laser is tunable to a wavelength suitable for detecting CO2.

5. The in-situ sensor system of claim 3 , wherein the laser is tunable to a wavelength suitable for detecting H2O.

6. The in-situ sensor system of claim 1 , wherein the optical transmitter housing has a power reducing aperture disposed in a front face of the housing such that the power reducing aperture effectively reduces the power output of the optical transmitter into the volume of the mask by blocking a portion of the signal path limiting.

7. The in-situ sensor system of claim 1 , wherein the optical transmitter housing has a step-down profile producing a smaller opening at an exit end of the housing that effectively reduces the power output from the optical transmitter.

8. The in-situ sensor system of claim 6 , wherein the laser has a maximum power output of 9.5 mW and the power reducing aperture reduces the power to less than 500 μW.

9. The in-situ sensor system of claim 7 , wherein the laser has a maximum power output of 9.5 mW and the smaller opening reduces the power output to less than 500 μW.

10. The in-situ sensor system of claim 1 , further comprising a temperature sensor disposed on the main housing and configured to measure the temperature of the sensor system.

11. The in-situ sensor system of claim 1 , further comprising a plurality of electrical connections between the optical transmitter and the optical receiver, and an external control module, wherein the control module is configured to receive and analyze data from the sensor system.

12. The in-situ sensor system of claim 11 , wherein the control module is configured to analyze the relative content of CO2 and/or H2O in the exhaled air and wherein the control module further comprises one or more feedback elements to provide feedback to the user with respect to the relative content of CO2 and H2O.

13. The in-situ sensor system of claim 11 , wherein the plurality of electrical connections are configured to be disconnectable from the mask through a connection port disposed on an exterior surface of the mask.

14. The in-situ sensor system of claim 1 , wherein the optical transmitter and the optical receiver are a fiber coupled laser.

15. A pilot oxygen mask system comprising:
an in-situ sensor system, wherein the in-situ sensor system comprises, a main housing, wherein the main housing is configured to cooperatively engage with an exhalation valve of an oxygen mask configured with a voluminous breathing chamber and wherein the main housing has an opening disposed therein that corresponds with an opening in the exhalation valve of the mask, and is disposed within the voluminous breathing chamber,
an optical transmitter housing disposed on the main housing and configured to house an optical transmitter element,
an optical receiver housing disposed on the main housing and configured to house an optical receiver element, and
wherein the optical transmitter element is optically aligned with the optical receiver element such that a signal path between the optical transmitter element and the optical receiver element transects the opening in the main housing such that exhaled air from a user of the mask will pass through the signal path as it is pushed through the exhalation valve.

Assignees

• California Inst Of Techn

Inventors

• Christensen Lance E
• Mansour Kamjou

Classifications

• G01N33/004

  CO or CO2 · CPC title

• G01N2201/06113

  Coherent sources; lasers · CPC title

• A61M2202/0208

  Oxygen · CPC title

• A61M16/0003

  Accessories therefor, e.g. sensors, vibrators, negative pressure · CPC title

• A61B5/6803

  Head-worn items, e.g. helmets, masks, headphones or goggles · CPC title