Fiber optic position sensing and indicating apparatus for electrical interference sensitive environments

Claim 2

Apparatus for passively sensing the physical condition of a remotely located object in an electrical interference sensitive environment comprising: an optical switch including a pressure sensitive member mechanically operable by said object alternately according to different positions of said object; said pressure sensitive member being provided with a pair of spaced reflective surfaces, each surface having a different degree of reflectivity; a light source; a single optical simultaneous light transmitting and receiving conductor having one end capable of receiving light from said light source for transmission through the other end to illuminate said optical switch; said optical conductor having a portion divided into at least two branch sections arranged so that one of said sections provides a light path from the light source to the optical switch, and one of said sections provides a return path for any reflected light from said optical switch to a processing means; means provided for testing and indicating the light transmitting continuity of said light source and said conductor; whereby the physical condition of said object can be determined passively at all times at a remote station without the need for the transmission of electrical energy that may be affected by electrical interference.

Claim 3

Apparatus for remotely sensing the mechanical position of an aircraft component comprising: an optical switch including a pressure movable piston mechanically operable by said component alternately between two positions; said piston having a reflecting surface for each of said positions; a pair of spaced dichroic filters mounted on the reflecting surfaces on said piston, each filter having a different wavelength, corresponding to said two positions of the piston; an enclosure containing a light source; means in the container for indicating the energization of the light source; a single optical simultaneous light transmitting and receiving conductor for said optical switch, one conductor end capable of receiving light from said source for transmission through the other end to illuminate alternately one of said dichroic filters; said optical conductor in said enclosure having a portion thereof divided into three branch cables so arranged that one of said branch cables provides a light path from the light source to the filters and the other two cables provide a return path for the reflected light from said filters to a respective detector; visual indicating means mounted on the face of said enclosure and connected to said filters; whereby the position of said component can be determined by the wavelength of the reflected light received at the respective detector, and the absence of any reflected light indicates a discontinuity in the light transmitting properties of said conductor.

Claim 4

Apparatus for remotely sensing the mechanical position of an aircraft component comprising: an optical switch including a pressure movable piston mechanically operable by said component alternately between two positions; said piston having a reflecting surface for each of said positions; a pair of spaced dichroic filters mounted on the reflecting surfaces on said piston, each filter having a different wavelength, corresponding to said two positions of the piston; an enclosure containing a light source; means in the container for indicating the energization of the light source; a single optical simultaneous light transmitting and receiving conductor for said optical switch, one conductor end capable of receiving light from said source for transmission through the other end to illuminate alternately one of said dichroic filters; said optical conductor in said enclosure having a portion thereof divided into three branch cables so arranged that one of said branch cables provides a light path from the light source to the filters and the other two cables provide a return path for the reflected light from said filters to a respective detector; visual indicating means mounted on the face of said enclosure and connected to said filters; whereby the position of said component can be determined by the wavelength of the reflected light received at the respective detector, and the absence of any reflected light indicates a discontinuity in the light transmitting properties of said conductor.