Multi-function air data probe having multi-hole ports used for determining angle of attack, total and static pressure values

Patent metadata

Field	Value
Publication number	US-11215631-B2
Application number	US-202016735366-A
Country	US
Kind code	B2
Filing date	Jan 6, 2020
Priority date	Oct 16, 2019
Publication date	Jan 4, 2022
Grant date	Jan 4, 2022

Abstract

A multi-function air data probe comprises a probe stem having an outer surface that extends between a first end and an opposite second end, with the probe stem having a first cross-sectional diameter; and a probe head having an outer surface that extends between a proximal end and a distal end, wherein the proximal end of the probe head is coupled to the first end of the probe stem. The probe head has a second cross-sectional diameter that is larger than the first cross-sectional diameter of the probe stem. A plurality of multi-hole ports is located in the probe head, with the multi-hole ports extending into and through the probe stem. The air data probe is operative to make measurements used to determine one or more of angle of attack values, total pressure values, and static pressure values.

First claim

What is claimed is:

1. A multi-function air data probe, comprising:
a probe stem having an outer surface that extends along an axial direction between a first end and an opposite second end, the probe stem having a first cross-sectional diameter;
a probe head having an outer surface that extends along the axial direction between a proximal end and a distal end, wherein the proximal end of the probe head is coupled to the first end of the probe stem, wherein the probe head has a second cross-sectional diameter that is larger than the first cross-sectional diameter of the probe stem; and
a plurality of multi-hole ports located in the probe head, the multi-hole ports extending into and through the probe stem along the axial direction, the multi-hole ports defined by respective sensor manifold tubes each having a plurality of openings;
wherein the outer surface of the probe head includes an array of sensor holes radially arranged in sensor hole rows along the axial direction;
wherein each of the sensor manifold tubes respectively communicates with one of the sensor hole rows along the axial direction through respective port tubes coupled between each of the sensor holes and the plurality of openings in the respective sensor manifold tubes;
wherein the air data probe is operative to make measurements used to determine one or more of angle of attack values, total pressure values, and static pressure values.

2. The multi-function air data probe of claim 1 , further comprising:
a base plate coupled to the probe stem at the opposite second end; and
one or more static pressure ports in the base plate.

3. The multi-function air data probe of claim 1 , further comprising a drain hole located at the distal end of the probe head.

4. The multi-function air data probe of claim 1 , wherein the probe stem and the probe head each have has a substantially cylindrical shape.

5. The multi-function air data probe of claim 1 , wherein the second cross-sectional diameter of the probe head is least about 10 percent larger than the first cross-sectional diameter of the probe stem.

6. The multi-function air data probe of claim 1 , further comprising:
a first set of flow stability structures extending along the outer surface of the probe stem; and
a second set of flow stability structures extending along the outer surface of the probe head.

7. The multi-function air data probe of claim 6 , wherein the first and second sets of flow stability structures encourage smooth air flow off a trailing edge of the structures to avoid vortex shedding.

8. The multi-function air data probe of claim 6 , wherein the first and second sets of flow stability structures are matching fins on left and right hand sides of a principle structure of the air data probe, with the fins having a substantially triangular cross section profile.

9. The multi-function air data probe of claim 1 , further comprising a drain port communicatively coupled to the sensor manifold tubes, the drain port configured to provide an outlet for excess air from the sensor manifold tubes.

10. The multi-function air data probe of claim 1 , wherein the air data probe is configured to be mounted on an aircraft.

11. An air data sensor, comprising:
a multi-function air data probe configured to protrude into an airflow to collect air data, the air data probe comprising:
a probe stem that extends along an axial direction between a first end and an opposite second end, the probe stem having a first cross-sectional diameter;
a probe head having an outer surface that extends along the axial direction between a proximal end and a distal end, wherein the proximal end is coupled to the first end of the probe stem, wherein the probe head has a second cross-sectional diameter that is larger than the first cross-sectional diameter of the probe stem;
a plurality of multi-hole ports located in the probe head, the multi-hole ports extending into and through the probe stem along the axial direction, the multi-hole ports defined by respective sensor manifold tubes each having a plurality of openings; and
a base flange coupled to the probe stem at the opposite second end;
wherein the outer surface of the probe head includes an array of sensor holes radially arranged in sensor hole rows along the axial direction;
wherein each of the sensor manifold tubes respectively communicates with one of the sensor hole rows along the axial direction through respective port tubes coupled between each of the sensor holes and the plurality of openings in the respective sensor manifold tubes;

a base plate coupled to the base flange of the air data probe; and
an electronics housing coupled to the base plate, the electronics housing containing at least one processor;
wherein the base plate includes one or more static pressure ports that extend into the electronics housing;
wherein the air data probe and the one or more static pressure ports are operative to make measurements used by the at least one processor to determine one or more of angle of attack values, total pressure values, and static pressure values.

12. The air data sensor of claim 11 , wherein:
the air data probe is positioned at a first location on the base plate that is offset from a center of the base plate; and
the one or more static pressure ports are positioned at a second location on the base plate that is offset from the center of the base plate.

13. The air data sensor of claim 11 , wherein the air data sensor is implemented in a digital line replaceable unit (LRU) for an aircraft.

Assignees

• Honeywell Int Inc

Inventors

• Anderson Morris G
• Gordon Grant A

Classifications

• B64D45/00

  Aircraft indicators or protectors not otherwise provided for · CPC title

• G01P13/025 Primary

  indicating air data, i.e. flight variables of an aircraft, e.g. angle of attack, side slip, shear, yaw · CPC title

• G01F1/46

  Pitot tubes · CPC title

• G01P21/025

  for measuring speed of fluids; for measuring speed of bodies relative to fluids (for measuring volume flow G01F25/10) · CPC title

• B64D43/02

  for indicating aircraft speed or stalling conditions · CPC title