Co-location of high-maintenance air data system components into one LRU

1. An air data sensing line-replaceable unit (LRU) comprising:

at least one pressure sensor, wherein the at least one pressure sensor includes a calibration memory that contains information related to calibration of the at least one pressure sensor; and

more than one probe or port coupled to the at least one pressure sensor, wherein the air data sensing LRU is configured to be coupled to an aircraft,

wherein the more than one probe or port conduits air located outside the air data sensing LRU and outside the aircraft to the at least one pressure sensor, and

wherein the more than one probe or port and the at least one pressure sensor are connected to each other by a permanent connection, wherein the permanent connection is non-disconnectable;

wherein the at least one pressure sensor is configured to generate an analog electrical signal, wherein the at least one pressure sensor is coupled to an electronic system LRU that is separate from the air data sensing LRU and positioned within the aircraft, wherein the at least one pressure sensor is configured to communicate the analog electrical signal to the electronic system LRU, wherein the electronic system LRU is configured to convert the analog electrical signal to a digital signal.

2. The air data sensing LRU of claim 1 , wherein the more than one probe or port comprises at least one of the following: one or more static ports, one or more pitot tubes, one or more pitot-static tubes, or one or more angle-of-attack vanes.

3. The air data sensing LRU of claim 1 , wherein the permanent connection is a weld.

4. The air data sensing LRU of claim 1 , wherein the permanent connection is a bond.

5. The air data sensing LRU of claim 1 , wherein the permanent connection is a braze.

6. The air data sensing LRU of claim 1 , wherein the at least one electronic system LRU comprises an air data module, wherein the at least one pressure sensor is configured to be coupled to the air data module to convert the analog electrical signal into a digital signal.

7. The air data sensing LRU of claim 1 , wherein the at least one electronic system LRU comprises an air data computer, wherein the at least one pressure sensor is configured to be coupled to the air data computer, wherein the air data computer calculates at least one of the following from the analog electrical signal: an altitude of the air data sensing LRU, an airspeed of the air data sensing LRU, or an angle of attack of the air data sensing LRU.

8. A method for constructing an air data sensing line-replaceable unit (LRU) comprising:

providing more than one probe or port and at least one pressure sensor that includes a calibration memory;

permanently connecting the more than one probe or port to the at least one pressure sensor to form a single air data sensing LRU, wherein permanently connecting includes establishing a permanent connection that is non-disconnectable, wherein the air data sensing LRU is coupled to an aircraft such that the more than one probe or port conduits air located outside the probe or port to the at least one pressure sensor; and

coupling the at least one pressure sensor and the calibration memory to at least one electronic system LRU in the aircraft;

wherein the at least one pressure sensor generates an analog electrical signal, wherein the at least one pressure sensor communicates the analog electrical signal to the at least one electronic system LRU over a communication medium, wherein the at least one electronic system LRU converts the analog electrical signal to a digital signal, wherein the at least one electronic system LRU is separate from the air data sensing LRU and positioned within the aircraft.

9. The method of claim 8 , wherein the more than one probe or port comprises one or more static ports, one or more pitot tubes, one or more pitot-static tubes, or one or more angle-of-attack vanes.

10. The method of claim 8 , wherein permanently connecting the more than one probe or port to the at least one pressure sensor comprises welding the more than one probe or port and the at least one pressure sensor together.

11. The method of claim 8 , wherein permanently connecting the more than one probe or port to the at least one pressure sensor comprises bonding the more than one probe or port and the at least one pressure sensor together.

12. The method of claim 8 , wherein permanently connecting the more than one probe or port to the at least one pressure sensor comprises brazing the more than one probe or port and the at least one pressure sensor together.

13. A system comprising:

an air data sensing line-replaceable unit (LRU) coupled to an aircraft, the air data sensing LRU comprising:

more than one probe or port, and

at least one pressure sensor,

wherein the more than one probe or port conduits air outside the air data sensing LRU and outside the aircraft to the at least one pressure sensor,

wherein the at least one pressure sensor converts the air into an analog electrical signal, and

wherein the more than one probe or port and the at least one pressure sensor are connected to each other by a permanent connection,

wherein the permanent connection is non-disconnectable;

an electronic system coupled to the air data sensing LRU, wherein the electronic system is separate from the air data sensing LRU and positioned within the aircraft,

wherein the electronic system is configured to receive the analog electrical signal from the at least one pressure sensor, and

wherein the electronic system is configured to convert the analog electrical signal into a digital signal; and

an air data inertial reference unit coupled to the electronic system, wherein the air data inertial reference unit converts the digital signal to at least one of the following: an altitude of the air data sensing LRU, an airspeed of the air data sensing LRU, or an angle of attack of the air data sensing LRU.

14. The system of claim 13 , wherein the permanent connection is a weld.

15. The system of claim 13 , wherein the permanent connection is a bond.

16. The system of claim 13 , wherein the permanent connection is a braze.

17. The system of claim 13 , wherein the electronic system is an air data module.

18. The system of claim 13 , wherein the electronic system is an air data computer.