Environmental condition sensing system
AssigneeHamilton Sundstrand Corporation
InventorsCatherine Thibaud, Zissis A. Dardas, Jagadeswara Reddy Karra, David L. Lincoln
Life of this patent
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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.
Claims9
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.
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.
Dependencies are inferred from the claim text.