1. An apparatus comprising:
a first strut having a first end and a second end opposite the first end, the first end of the first strut operatively coupled to a fuselage of an aircraft and the second end of the first strut operatively coupled to a wing of the aircraft; and
a first actuator operatively coupled to the first strut to change an effective length of the first strut.
2. The apparatus of claim 1, wherein the first actuator is operatively coupled between the first end of the first strut and the fuselage of the aircraft.
3. The apparatus of claim 2 further comprising a second strut having a first end and a second end opposite the first end, the first end of the second strut operatively coupled to the fuselage of the aircraft and the second end of the second strut operatively coupled to the wing of the aircraft.
4. The apparatus of claim 3 further comprising a second actuator operatively coupled between the first end of the second strut and the fuselage to change an effective length of the second strut.
5. The apparatus of claim 4, wherein the second end of the first strut is operatively coupled to the wing proximate a forward spar in the wing and the second end of the second strut is operatively coupled to the wing proximate an aft spar in the wing.
6. The apparatus of claim 1 further comprising a controller to operate the actuator to change the effective length of the first strut based on at least one of an altitude of the aircraft, a speed of the aircraft, a weight of the wing of the aircraft, or a change in shape of the wing during flight.
7. The apparatus of claim 6 further comprising a sensor operatively coupled to the wing to detect the change in shape of the wing during flight.
8. The apparatus of claim 1, wherein the first actuator comprises a shape memory alloy wire.
9. An apparatus comprising:
a first strut operatively coupled between a fuselage of an aircraft and a wing of the aircraft to support the wing during flight; and
a first actuator to adjust a tension in the first strut during flight.
10. The apparatus of claim 9 further comprising a sensor to detect twist in the wing, wherein the first actuator is to adjust the tension in the first strut during flight based on the twist.
11. The apparatus of claim 9, wherein the first strut is operatively coupled to a forward spar in the wing.
12. The apparatus of claim 11 further comprising a second strut operatively coupled between the fuselage and the wing to support the wing during flight, the second strut operatively coupled to an aft spar in the wing.
13. The apparatus of claim 12 further comprising a second actuator to adjust a tension in the second strut during flight.
14. A method comprising:
measuring a deflection of a wing of an aircraft during flight, the aircraft having a first strut coupled between the wing and a fuselage of the aircraft; and
adjusting an effective length of the first strut between the wing and the fuselage based on the measured deflection of the wing to change the deflection of the wing.
15. The method of claim 14, wherein the aircraft includes a second strut coupled between the wing and the fuselage.
16. The method of claim 15 further comprising adjusting an effective length of the second strut between the wing and the fuselage based on the measured deflection of the wing to change the deflection of the wing.
17. The method of claim 16, wherein the first strut is coupled to a forward spar in the wing and the second strut is coupled to an aft spar in the wing.
18. The method of claim 16, wherein adjusting the effective length of the first strut comprises extending the first strut to increase the effective length of the first strut and adjusting the effective length of the second strut comprises shortening the second strut to decrease the effective length of the second strut.
19. The method of claim 14, wherein the deflection of the wing is measured via a sensor operatively coupled to the wing.
20. The method of claim 19 further comprising:
determining at least one of an altitude of the aircraft, a speed of the aircraft, or a volume of fuel in the wing; and
adjusting the effective length of the first strut based on the least one of the determined altitude, speed, or volume.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.
1. An ozone generation system comprising:
an ozone generator adapted to deliver a given amount of ozone in a space in order to obtain a target concentration therein;
a variable direct current power supply connected to the ozone generator and having a first input for receiving an alternating current power signal and a second input for an external control signal;
a control unit connected to the second input of the power supply for generating the external control signal, the external control signal being generated in accordance with an amount of ozone required in order to reach the target concentration; and
an ozone sensor connected to the control unit and adapted to measure a residual amount of ozone in the space and provide the control unit with a measurement signal of the residual amount for determining the amount of ozone required.
2. The ozone generation system of claim 1, wherein the power supply is controllable from substantially 0% to substantially 100% of an available output voltage.
3. The ozone generation system of claim 1, wherein the power supply comprises a solid-state relay connected to an input of a rectifier, for metering an amount of the alternating current power signal presented to the rectifier, and a filter connected to an output of the rectifier for smoothing out a rectified signal and presenting the rectified signal to the ozone generator.
4. The ozone generation system of claim 1, wherein the filter is one of an inductor-capacitor filter and a capacitor-inductor-capacitor filter.
5. (canceled)
6. The ozone generation system of claim 1, wherein the external control signal is one of an alternating current signal from about 4 ma to about 20 ma and a direct current signal from about 0 volts to about 10 volts.
7. (canceled)
8. The ozone generation system of claim 1, wherein the rectifier is a full-wave rectifier.
9. The ozone generation system of claim 1, wherein the control unit comprises a Proportional-Integral-Derivative (PID) controller.
10. The ozone generation system of claim 1, wherein the control unit comprises a control device to vary a corona frequency and a corona voltage, a control loop feedback mechanism, and an interface for setting control parameters.
11. The ozone generation system of claim 10, wherein the control unit is adapted for setting the control parameters remotely.
12. The ozone generation system of claim 1, wherein the ozone generator comprises at least one output valve for selectively outputting generated ozone into the space and at least one dump valve for disposing of ozone when the at least one output valve is closed.
13. The ozone generation system of claim 12, wherein the at least one output valve is a proportional control valve controlled by the control unit.
14. The ozone generation system of claim 12, wherein each one of the at least one output valve is associated with a given zone in the space, and is controlled in accordance with ozone to be delivered to the given zone.
15. The ozone generation system claim 12, wherein the ozone generator comprises a flow sensor for measuring a flow rate of clean air provided to an ozone generating tube inside the ozone generator, and the flow rate as measured is provided to the control unit.
16. The ozone generation system of claim 15, wherein the flow sensor is an electronic flow sensor provided upstream from the ozone generating tube, in an input path thereof.
17. A method for generating ozone in a space, the method comprising:
measuring a concentration of residual ozone in the space;
determining, from the concentration measured, an amount of ozone required for providing a target concentration of ozone in the space;
generating an external control signal for energizing a variable direct current power supply, the external control signal having a value selected in accordance with the amount of ozone required;
energizing the variable direct current power supply with the external control signal and supplying the direct current power supply with an alternating current power signal;
metering an amount of the alternating current power signal allowed to flow through the variable direct current power supply by varying a conduction angle thereof, thereby causing the variable direct current power supply to output a predetermined voltage level to an ozone generator; and
delivering the amount of ozone required for providing the target concentration in the space.
18. The method of claim 17, wherein metering an amount of the alternating current power signal comprises metering from substantially 0% to substantially 100% of the alternating current power signal.
19. The method of claim 17, wherein metering an amount of the alternating current power signal comprises chopping the alternating current power signal using a solid state relay, rectifying a chopped signal, and filtering a rectified signal to provide the predetermined voltage level to the ozone generator.
20. The method of claim 17, wherein energizing the variable direct current power supply comprises providing the variable direct current power supply with one of an alternating current control signal from about 4 ma to about 20 ma and a direct current control signal from about 0 volts to about 10 volts.
21. (canceled)
22. The method of claim 17, wherein energizing the variable direct current power supply comprises energizing upon a zero-crossing of the alternating current power signal.
23. The method of claim 17, wherein causing the variable direct current power supply to output a predetermined voltage level comprises outputting a predetermined voltage level that is substantially linear with respect to the external control signal.
24. (canceled)
25. (canceled)
26. The method of claim 17, wherein delivering the amount of ozone comprises selectively opening and closing at least one output valve, and selectively opening at least one dump valve when the at least one output valve is closed.
27. (canceled)
28. The method of claim 26, wherein delivering the amount of ozone comprises selectively delivering the ozone to at least two zones of the space, each one of the at least two zones having at least one of the at least one output valve assigned thereto.
29. The method of claim 26, further comprising measuring a flow rate of a clean air input, and using the flow rate as measured to dynamically open and close the at least one output valve and the at least one dump valve.
30. A fully variable direct current power supply having a first input for receiving an alternating current power signal and a second input for an external control signal, the power supply comprising a solid-state relay and a rectifier, the solid state relay, connected to an input of the rectifier, adapted for metering the alternating current power signal presented to the rectifier from substantially 0% to substantially 100%, and a filter connected to an output of the rectifier for smoothing out a rectified signal and outputting a direct current voltage signal.
31. A method for generating a direct current voltage signal, the method comprising energizing the variable direct current power supply with an external control signal and an alternating current power signal, metering from substantially 0% to substantially 100% an amount of the alternating current power signal allowed to flow through the variable direct current power supply as a function of the external control signal by varying a conduction angle thereof using a solid state relay, rectifying an output of the solid state relay, filtering a rectified signal, and outputting a direct current voltage signal.