Electric signal to pressure signal transducer

Claim 2

An electric signal to pneumatic signal transducer having an electric input signal and a gas supply comprising: nozzle means connected to the gas supply for expelling a gas stream, receiver means spaced from the nozzle means positioned for recovering at least a portion of the expelled gas stream, the recovered portion constituting a pneumatic output signal; and deflector means, the position of which relative to the gas stream is controlled by the electric input signal for aerodynamically deflecting the gas stream expelled from the nozzle means to thereby affect the magnitude of the potion of the gas stream recovered by the receiver means and for providing an aerodynamic force to urge the deflector means further into the gas stream.

Claim 3

An electric signal to pneumatic signal transducer as claimed in claim 1 wherein a portion of the deflector means aerodynamically affects the gas stream, which portion comprises at least an arc of a circle in cross section.

Claim 4

An electrical signal to pneumatic signal transducer as claimed in claim 2 wherein the deflector means is made to respond to the electric input signal by means of magnetic actuation.

Claim 5

An electric signal to pneumatic signal transducer coupled to an input pneumatic supply of gas under pressure and having a pneumatic output port and electrically connected to a source of electric input signals, the transducer comprising, nozzle means having a first end coupled to the input pneumatic supply of gas and a second end coupled to the first end and having an opening for expelling the gas in a stream at a velocity; receiver means spaced apart from the nozzle means and having a first end having an opening for recovering a portion of expelled gas stream directed from the second end of the nozzle means and a second end coupled to the first end and coupled to the pneumatic output port for supplying the portion of the received gas stream thereto; actuator means connected to the source of electric input signals for converting such signals to motion in a plane; deflector means coupled to the actuator means such that the deflector means are moved responsive to the input electrical signals, said deflector means being located with respect to the gas stream whereby the deflector means is urged into the gas stream by aerodynamic lift, and located with respect to the nozzle means and receiver means whereby motion commanded by the actuator means causes the deflector means to move to affect the expelled gas stream between the nozzle means and receiver means, the deflector means producing a resultant gas local velocity direction that is deflected from the direction of the expelled gas stream velocity, which deflection affects the portion of the expelled gas stream recovered by the receiver means, the portion recovered bearing a predetermined relationship to the electric input signal to the actuator means.

Claim 6

An electric signal to pneumatic signal transducer coupled to an input pneumatic supply of gas under pressure and having a pneumatic output port and electrically connected to a source of electric input signals, the transducer comprising, nozzle means having a first end coupled to the input pneumatic supply of gas and a second end coupled to the first end and having an opening for expelling the gas in a stream at a velocity; receiver means spaced apart from the nozzle means and having a first end having an opening for recovering a portion of expelled gas stream directed from the second end of the nozzle means and a second end coupled to the first end and coupled to the pneumatic output port for supplying the portion of the received gas stream thereto; actuator means connected to the source of electric input signals for converting such signals to motion in a plane; deflector means coupled to the actuator means such that the deflector means are moved responsive to the input electrical signals, said deflector means being located with respect to the gas stream whereby the deflector means is urged into the gas stream by aerodynamic lift, and located with respect to the nozzle means and receiver means whereby motion commanded by the actuator means causes the deflector means to move to affect the expelled gas stream between the nozzle means and receiver means, the deflector means producing a resultant gas local velocity direction that is deflected from the direction of the expelled gas stream velocity, which deflection affects the portion of the expelled gas stream recovered by the receiver means, the portion recovered bearing a predetermined relationship to the electric input signal to the actuator means.

Claim 7

A transducer as claimed in claim 4 wherein the deflector means has a circular cross section.

Claim 8

A transducer as claimed in claim 4 wherein the deflector means has a triangular cross section.

Claim 9

A transducer as claimed in claim 4 wherein the deflector means has a semicircular cross section.

Claim 10

A transducer as claimed in claim 5 wherein the opening in the second end of the nozzle means is circular, the diameter of the deflector means being between one and two times the diameter of the opening in the second end of the nozzle means.

Claim 11

A transducer as claimed in claim 8 wherein the distance between the nozzle means and the receiving means is eight to twelve times the diameter of the opening in the second end of the nozzle means.

Claim 12

A transducer as claimed in claim 4 wherein the deflector means is positioned in the gas stream to produce a negative force per distance of deflection required of the actuation means to the deflector means to increasing affect the expelled gas stream, and the actuator means having a spring modulus greater in magnitude and opposite in sign to the spring modulus of the deflector means.

Claim 13

A transducer as claimed in claim 4 wherein the nozzle means has a longitudinal axis and the deflector means moves along a line intersecting the longitudinal axis at an angle θ between 75 degrees and 150 degrees.

Claim 14

A transducer as claimed in claim 8 wherein the diameter of the opening in the second end of the nozzle means is between 0.025 and 0.05 centimeters.

Claim 15

A transducer as claimed in claim 8 wherein the diameter of the opening in the second end of the nozzle is 0.0375 centimeters.

Claim 16

A transducer as claimed in claim 4 wherein the input electric signal is variable between 0 and 2 millamperes.

Claim 17

An electrical signal to pneumatic signal transducer having an electric input signal and a gas supply having: nozzle means connected to the gas supply for expelling a gas stream, receiver means spaced from the nozzle means positioned for recovering at least a portion of the expelled gas stream, the recovered portion constituting a pneumatic output signal; deflector means, the position of which relative to the gas stream is controlled by the electric input signal for deflecting the gas stream expelled from the nozzle means to thereby affect the magnitude of the portion of the gas stream recovered by the receiver means; and wherein the deflector means is shaped as an airfoil and located with respect to the nozzle means to affect the position of deflector means by aerodynamic lift.

Claim 18

An electrical signal to pneumatic signal transducer having an electric input signal and a gas supply having: nozzle means connected to the gas supply for expelling a gas stream, receiver means spaced from the nozzle means positioned for recovering at least a portion of the expelled gas stream, the recovered portion constituting a pneumatic output signal; deflector means, the position of which relative to the gas stream is controlled by the electric input signal for deflecting the gas stream expelled from the nozzle means to thereby affect the magnitude of the portion of the gas stream recovered by the receiver means; and wherein the deflector means is shaped as an airfoil and located with respect to the nozzle means to affect the position of deflector means by aerodynamic lift.

Claim 19

An electric signal to pneumatic signal transducer as claimed in claim 15 wherein the aerodynamic lift urges the deflector means further into the gas stream.

Claim 20

An electric signal to pneumatic signal transducer as claimed in claim 15 wherein the deflector means is drawn into the gas stream by aerodynamic lift.

Claim 21

An electric signal to pneumatic signal transducer as claimed in claim 15 wherein the deflector means interacts with only a portion of the gas stream.

Claim 22

An electric signal to pneumatic signal transducer as claimed in claim 15 wherein the electric input signal drives the deflector means away from the gas stream.

Claim 23

An electric signal to pneumatic signal transducer as claimed in claim 4 further comprising a 4 to 20 milliampere two-wire electric circuit wherein the 4 to 20 milliampere two-wire electric circuit energizes the actuation means.

Claim 24

An electric signal to pneumatic signal transducer as claimed in claim 20 wherein the actuator means is a magnetic force actuator.