Environmental condition sensing system

Patent metadata

Field	Value
Publication number	US-11713985-B2
Application number	US-202017070008-A
Country	US
Kind code	B2
Filing date	Oct 14, 2020
Priority date	Oct 16, 2019
Publication date	Aug 1, 2023
Grant date	Aug 1, 2023

Abstract

Fibre optics for distributed environmental condition and/or air quality sensing such as, but not limited to, sensing air quality in enclosed areas of an aircraft such as the passenger cabin. Fibre optics can be used for sensing and for communication and are therefore well suited to the distributed sensing of environmental conditions such as temperature, relative humidity, gas and particulate composition within spaces of the aircraft e.g. the cabin, cargo space, cockpit, electronics bay etc. and in related systems such as the environmental control system (ECS), the cabin recirculation system, bleed air system etc.

First claim

The invention claimed is:

1. A distributed environmental monitoring system comprising:
one or more optical fibres along a length of which light can be transmitted,
wherein each optical fibre comprises a tubular cladding along the interior of which runs a first core along which light is transmitted from a first end of the fibre to a second end of the fibre, the light exiting the second end into an environment to be sensed, and a second core along which light returned from the environment is transmitted from the second end to the first end;
wherein the one or more optical fibres define a plurality of nodes spaced along the length, each node configured to vary the properties of light returned back along the optical fibre(s) according to a condition of the environment detected at the node,
each node varying the properties of the returned light differently based on its configuration and its location along the length of the optical fibre; the system further comprising a light source for transmitting light into and along the optical fibre(s) and one or more detectors for receiving light returned along the optical fibre(s) from the environment via the nodes;
wherein one or more of the one or more nodes is located at or in a passenger seat of an aircraft;
wherein at least one of one or more nodes located at or in a passenger seat is provided in the seat and detects pressure due to presence of a passenger in the seat as the condition of the environment.

2. The system of claim 1 , wherein one or more of the one or more nodes is configured to detect a condition of the environment due to light scattering at the node.

3. The system of claim 1 , wherein one or more of the one or more nodes is configured to detect a condition of the environment due to deformation of fibres by deformation of a coating provided at the node in response to the coating being contacted by a specific substance.

4. The system of claim 1 , wherein the system is configured to detect a condition of the environment due to a metal organic framework (MOF) coating at the node being contacted by a specific substance.

5. A distributed environmental monitoring system comprising:
one or more optical fibres along a length of which light can be transmitted,
wherein each optical fibre comprises a tubular cladding along the interior of which runs a first core along which light is transmitted from a first end of the fibre to a second end of the fibre, the light exiting the second end into an environment to be sensed, and a second core along which light returned from the environment is transmitted from the second end to the first end;
wherein the one or more optical fibres define a plurality of nodes spaced along the length, each node configured to vary the properties of light returned back along the optical fibre(s) according to a condition of the environment detected at the node,
each node varying the properties of the returned light differently based on its configuration and its location along the length of the optical fibre;
the system further comprising a light source for transmitting light into and along the optical fibre(s) and one or more detectors for receiving light returned along the optical fibre(s) from the environment via the nodes;
wherein one or more of the one or more nodes is located at or in a passenger seat of an aircraft;
wherein at least one of one or more nodes located at or in a passenger seat detects pressure due to presence of an object in proximity to the seat as the condition of the environment.

6. The system of claim 5 , wherein the object is a flotation device.

7. The system of claim 5 , wherein one or more of the one or more nodes is configured to detect a condition of the environment due to light scattering at the node.

8. The system of claim 5 , wherein one or more of the one or more nodes is configured to detect a condition of the environment due to deformation of fibres by deformation of a coating provided at the node in response to the coating being contacted by a specific substance.

9. The system of claim 5 , wherein the system is configured to detect a condition of the environment due to a metal organic framework (MOF) coating at the node being contacted by a specific substance.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Thibaud Catherine
• Dardas Zissis A
• Karra Jagadeswara Reddy
• Lincoln David L

Classifications

• G01D5/35367 Primary

  using reflected light other than backscattered to detect the measured quantity · CPC title

• B64D11/0602

  Seat modules, i.e. seat systems including furniture separate from the seat itself · CPC title

• B64D11/0633

  for devices other than life vests and intended for external use, e.g. parachutes or life rafts · CPC title

• G01L1/243

  using means for applying force perpendicular to the fibre axis · CPC title

• G02B6/06

  the relative position of the fibres being the same at both ends, e.g. for transporting images · CPC title