Patent Application
20210179277
The present disclosure relates generally to air data probes, and in particular, to flush static plates.
Flush static plates measure pressure at the outer mold line of an aircraft to generate air data parameters. Flush static plates have faceplates with external surfaces in line with the aircraft outer mold line in order to minimize flow disruption. Thus, flush static plates are exposed to the environmental conditions exterior to the aircraft, which are often cold. As such, heaters are utilized within flush static plates to remove and prevent ice accumulation during flight operation and ensure the flush static plates function properly in liquid water, ice crystal, and mixed phase icing conditions. It can be difficult to heat flush static plates using power levels as are typically provided by the aircraft.
A static plate heating arrangement includes a faceplate including a port extending from an exterior surface of the faceplate to an interior surface of the faceplate, a fixed resistance heater in thermal communication with the interior surface and surrounding the port, and a self-regulating heater in thermal communication with the interior surface and surrounding the fixed resistance heater. The fixed resistance heater and the self-regulating heater are electrically connected in series.
A method of heating a static plate includes positioning a fixed resistance heater to be in thermal communication with an interior surface of a faceplate of the static plate and surround a port in the faceplate, positioning a self-regulating heater to be in thermal communication with the interior surface of the faceplate and surround the fixed resistance heater, and causing current to flow through the fixed resistance heater and the self-regulating heater in series.
In general, the present disclosure describes a heating arrangement for a flush static plate that has an outer self-regulating annular heater surrounding an inner fixed resistance heater, which are electrically connected in series; low thermal conductivity mounts; and annular gaps to increase power efficiency and reliability and reduce system complexity while removing entrapped moisture and maintaining an ice-free area.
Flush static plate 10 has faceplate 12 connected to housing 14. Housing 14 is connected to a central portion of faceplate 12. Internal components of flush static plate 10 are located within housing 14, such as a transducer. Faceplate 12 has exterior surface 16 at an outer surface of faceplate 12 and an interior surface 18 at an inner surface of faceplate 12. Housing 14 is connected to interior surface 18 of faceplate 12 via mounts (shown in
Flush static plate 10 is configured to be installed on an aircraft. Flush static plate 10 may be mounted to a fuselage of an aircraft via mounting holes 22 on faceplate 12 and fasteners, such as screws or bolts. Exterior surface 16 of faceplate 12 is in line with, or flush with, the outer mold line of the aircraft to minimize flow disruption. Housing 14 extends within aircraft. Flush static plate 10 measures static pressure at exterior surface 16 via ports 20 and communicates air pressures pneumatically through internal components of flush static plate 10. Pressure measurements are communicated to a flight computer and can be used to generate air data parameters related to the aircraft flight condition.
Flush static plate 10 has the same structure and function as described with respect to
As seen in
Faceplate 12 has inner annular gap 30, which is a space extending into faceplate 12 from interior surface 18 of faceplate 12 between fixed resistance heater 24 and self-regulating heater 26. Thus, faceplate 12 has a decreased thickness at inner annular gap 30. Inner annular gap 30 surrounds fixed resistance heater 24. Inner annular gap 30 extends into faceplate beyond fixed resistance heater 24 such that inner annular gap 30 is closer to exterior surface 16 of faceplate than fixed resistance heater 24. Inner annular gap 30 may have a uniform width. Outer annular gap 32 is a space that extends into faceplate 12 from interior surface 18 of faceplate 12 such that outer annular gap 32 surrounds self-regulating heater 26. Thus, faceplate 12 has a decreased thickness at outer annular gap 32, and self-regulating heater 26 is positioned between inner annular gap 30 and outer annular gap 32. Outer annular gap 22 may have a uniform width.
Flush static plate 10 is installed on an aircraft and exposed to external airflow, which may contain water and/or ice particles. Fixed resistance heater 24 and self-regulating heater 26 provide heat to flush static plate 10 to prevent and remove ice accumulation. Fixed resistance heater 24 also removes moisture that enters ports 20 during flight or when grounded. Upon start-up, heat from fixed resistance heater 24 is provided to ports 20 to bake out (or burn off or boil out) water that is ingested when the aircraft is grounded (or in flight) that would otherwise remain in ports 20 and block the pressure path within flush static plate 10.
As the temperature of self-regulating heater 26 increases, the resistance of self-regulating heater 26 increases after a certain temperature has been reached, or set-point temperature (as defined by the self-regulating design), which reduces the amount of power consumed by both self-regulating heater 26 and fixed resistance heater 24. As the temperature of self-regulating heater 26 decreases below the set-point temperature, the resistance of self-regulating heater 26 decreases, which increases the amount of power consumed by both self-regulating heater 26 and fixed resistance heater 24. Self-regulating heater 26 utilizes an automatic shut-off. When self-regulating heater 26 reaches a certain temperature, or certain set-point, self-regulating heater 26 increases its resistance to choke the power draw of self-regulating heater 26 and fixed resistance heater 24 of flush static plate 10. The set-point may be in a range of about 80 degrees Celsius to about 130 degrees Celsius.
Because faceplate 12 is made from thermally conductive material, faceplate 12 is thermally conductive. Mounts 28, inner annular gap 30, and outer annular gap 32 keep heat at a center portion of aluminum faceplate 12. Mounts 28 are made of low thermal conductivity material to minimize heat loss through mounts 28. Inner annular gap 30 and outer annular gap 32 minimize heat loss to faceplate 12 via conduction. Inner annular gap 30 prevents heat from fixed resistance heater 24 from moving beyond inner annular gap 30, or keeps heat in the center of faceplate 12. Inner annular gap 30 extends closer to exterior surface 16 of faceplate than fixed resistance heater 24 to better prevent heat loss to faceplate 12. Outer annular gap 32 prevents heat from fixed resistance heater 24 and self-regulating heater 26 from moving beyond outer annular gap 32, or keeps heat in the center of faceplate 12. As such, inner annular gap 30 and outer annular gap 32 are features that decrease heat transfer radially across inner annular gap 30 and outer annular gap 32, respectively, providing thermal separation for fixed resistance heater 24 and self-regulating heater 26. Inner annular gap 30 and outer annular gap 32 define decreased thickness of faceplate 12 to prevent heat loss beyond inner annular gap 30 and outer annular gap 32.
Fixed resistance heater 24 and self-regulating heater 26 provide anti-icing and moisture management of flush static plate 10 to ensure flush static plate 10 functions properly. Self-regulating heater 26 is spaced from fixed resistance heater 24 so that self-regulating heater 26 effectively chokes the power draw at the desired temperature.
Mounts 28, inner annular gap 30, and outer annular gap 32 keep heat at a center portion of aluminum faceplate 12, such as at ports 20, to minimize heat loss from fixed resistance heater 24 and self-regulating heater 26 to faceplate 12, housing 14, and other areas of flush static plate 10. Thus, heat is maintained only where required, resulting in more efficient use of power.
R1 is the resistor of fixed resistance heater 24. R2 is the resistor of self-regulating heater 26. Resistor R1 and resistor R2 are connected in series. As such, fixed resistance heater 24 and self-regulating heater 26 are electrically connected in series. Circuitry 34 of flush static plate 10 does not include a switch between resistor R1 of fixed resistance heater 24 and resistor R2 of self-regulating heater 26.
Fixed resistance heater 24 receives power via input voltage VIN provided to resistor R1 as current. As such, current flows through resistor R1 of fixed resistance heater 24 and then to resistor R2 of self-regulating heater 26. Due to self-regulating heater 26, the combination of fixed resistance heater 24 and self-regulating heater 26 connected in series is also self-regulating. As such, circuitry 34 of flush static plate 10 is self-regulating. When flush static plate 10 increases in temperature, the total resistance of fixed resistance heater 24 and self-regulating heater 26 increases, decreasing the current, which decreases power consumption. When flush static plate 10 decreases in temperature, the total resistance of fixed resistance heater 24 and self-regulating heater 26 decreases to increase the current, which increases power and provides heat needed to maintain deicing and anti-icing capabilities in cold environments. Output voltage VOUT is a voltage that allows for monitoring of self-regulating heater 26 if desired.
Maximum power consumption of fixed resistance heater 24 and self-regulating heater 26 is limited by self-regulating heater 26, which utilizes the automatic shut-off, as described above with respect to
Fixed resistance heater 24 receives the most heat and draws the most power, upon power-up, allowing for bake out of ports 20, as discussed above with respect to
Because circuitry 34 passively controls the amount of power consumed by fixed resistance heater 24 and self-regulating heater 26, circuitry 34 does not include a switch, such as a mechanical or thermal switch, which would require additional circuitry and could result in increased development lead times and reduced reliability. Additionally, designs with active control may get too hot when the aircraft is grounded if the heaters are not turned off. Thus, flush static plate 10 is less complex, less prone to failure, more reliable, and has reduced associated lead time and technical risk.
Self-regulating heater 26 connected in series with fixed resistance heater 24 prevents excessive power consumption and burn-out of fixed resistance heater 24 and self-regulating heater 26 via the automatic shut-off. Further, flush static plate 10 uses power more efficiently and is more cost-effective.
Mounts 28, inner annular gap 30, and outer annular gap 32, together with fixed resistance heater 24 and self-regulating heater 26 connected in series, achieves improved management of heat for optimal de-icing, anti-icing, and moisture management while reducing system complexity and cost and increasing reliability.
Flush static plate 10A has generally the same structure and function as flush static plate 10 described with respect to
R1A and R1B are the resistors of fixed resistance heater 24A. R2A is the resistor of self-regulating heater 26A. Switch 36A is between resistors R1A and R1B and between resistors R1A and R2A. As such, switch 36A is between fixed resistance heater 24A and self-regulating heater 26A. Resistors R1A and R1B are connected in series when switch 36A is in a first position. Switch 36A is in a first position when circuitry 34A is unpowered. When switch 36A is in a first position, all of the current, and thus heat, is directed to fixed resistance heater 24A. As such, fixed resistance heater 24A responds rapidly at start-up and effectively achieves bake out more quickly. Resistors R1A and R2A are connected in series when switch 36A is in a second position. When switch 36A is in a second position, current is divided between fixed resistance heater 24A and self-regulating heater 26A, and fixed resistance heater 24A and self-regulating heater 26A function the same as fixed resistance heater 24 and self-regulating heater 26 described with respect to
While switch 36A may require active control of flush static plate 10A and introduce a decrease in reliability, switch 36A can offer some performance benefits, particularly at start-up. Additionally, when switch 36A is in the second position, flush static plate 10A can be passively controlled and achieve optimal de-icing and moisture management.
The following are non-exclusive descriptions of possible embodiments of the present invention.
A static plate heating arrangement includes a faceplate including a port extending from an exterior surface of the faceplate to an interior surface of the faceplate; a fixed resistance heater in thermal communication with the interior surface and surrounding the port; and a self-regulating heater in thermal communication with the interior surface and surrounding the fixed resistance heater; wherein the fixed resistance heater and the self-regulating heater are electrically connected in series.
The static plate heating arrangement of the preceding paragraph can optionally include, additionally and/or alternatively, any one or more of the following features, configurations and/or additional components:
Circuitry of the flush static plate does not include a switch between the fixed resistance heater and the self-regulating heater.
The faceplate is made of material having a thermal conductivity in the range of the thermal conductivity of titanium to the thermal conductivity of copper.
A feature positioned between the fixed resistance heater and the self-regulating heater configured to decrease heat transfer radially across the feature.
The feature is an inner annular gap that defines a decreased thickness of the faceplate where the annular gap exists.
A feature surrounding the self-regulating heater configured to decrease heat transfer radially across the feature.
The feature is an outer annular gap that defines a decreased thickness of the faceplate where the annular gap exists.
An inner annular gap extending into the faceplate from an interior surface of the faceplate; and an outer annular gap extending into the faceplate from an interior surface of the faceplate; wherein the self-regulating heater is positioned between the inner annular gap and the outer annular gap.
A mount positioned between the interior surface of the faceplate and a housing of the flush static plate, the mount being formed of a low thermal conductivity material.
The mount is formed of at least one of steel, titanium, composite, and plastic.
The mount is adjacent the self-regulating heater.
A plurality of mounts positioned between the interior surface of the faceplate and a housing, the plurality of mounts being formed of a low thermal conductivity material and being adjacent the self-regulating heater.
The port extends through a portion of the faceplate within the fixed resistance heater such that the fixed resistance heater surrounds an interior portion of the port.
A switch between the fixed resistance heater and the self-regulating heater.
The switch is one of a thermal switch and an electronically-controlled switch.
A method of heating a static plate includes positioning a fixed resistance heater to be in thermal communication with an interior surface of a faceplate of the static plate and surround a port in the faceplate; positioning a self-regulating heater to be in thermal communication with the interior surface of the faceplate and surround the fixed resistance heater; and causing current to flow through the fixed resistance heater and the self-regulating heater in series.
While the invention has been described with reference to an exemplary embodiment(s), it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment(s) disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.
