IP Library › Granted Patent US 10,589,870
Granted Patent B2
US 10,589,870 · App. 16/298,569 · Granted Mar 17, 2020

Moisture resistant air data probes

Inventors: Timothy T. Golly (Lakeville, MN); Greg A. Seidel (Farmington, MN); Paul R. Johnson (Prior Lake, MN)
Assignee: Rosemount Aerospace Inc.
B64D43/02B65H54/103G01L19/0092G01L19/04G01P5/165G01P13/025B65H2701/341
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Quick Facts
Patent No.
US 10,589,870
App. No.
16/298,569
Granted
Mar 17, 2020
Kind
B2
Abstract

An air data probe includes a probe head defining a longitudinal axis between a forward tip and aft base. A port opening is defined in the forward tip. A first conduit is in fluid communication with the port opening to guide fluid flow from the port opening to a first chamber. The first chamber is downstream from the port opening. A second conduit, offset radially and circumferentially from the first conduit, is in fluid communication with the first chamber to guide fluid flow from the first chamber to a second chamber. The second chamber is downstream from the first chamber. The offset between the first and second conduits is configured to prevent particle ingestion from the port opening from entering the second conduit.

Claims (14)

1. An air data probe comprising:

a probe head defining a longitudinal axis between a forward tip and aft base;

a port opening defined in the forward tip;

a first conduit in fluid communication with the port opening to guide fluid flow from the port opening to a first chamber, wherein the first chamber is downstream from the port opening; and

a second conduit, offset radially and circumferentially from the first conduit, in fluid communication with the first chamber to guide fluid flow from the first chamber to a second chamber, wherein the second chamber is downstream from the first chamber, wherein the offset between the first and second conduits is configured to prevent particle ingestion from the port opening from entering the second conduit.

2. An air data probe as recited in claim 1 , further comprising a static conduit in fluid communication with a static chamber, wherein the static chamber is upstream from the first chamber.

3. An air data probe as recited in claim 2 , further comprising a respective capillary tube nested within at least one of the first conduit, the second conduit or the static conduit, and wherein the capillary tube abuts an inner surface at least one of the first conduit, the second conduit or the static conduit to gather moisture entering the port opening.

4. An air data probe as recited in claim 2 , wherein an inner surface of at least one of the first conduit, the second conduit or the static conduit includes raised features to gather moisture entering the port opening.

5. An air data probe as recited in claim 2 , wherein an inner surface of at least one of the first conduit, the second conduit or the static conduit includes at least one of recessed features or a porous material to gather moisture entering the port opening.

6. An air data probe as recited in claim 1 , wherein the static conduit directs flow from the static chamber through the first chamber, wherein the static conduit is sigmoidal shaped between an outlet of the first conduit and an inlet of the second conduit within the first chamber to block a direct pathway between the outlet of the first conduit and the inlet of the second conduit.

7. An air data probe as recited in claim 1 , further comprising a thermocouple having a sense end in the forward tip to measure the temperature in the forward tip.

8. An air data probe as recited in claim 7 , further comprising a bulkhead within the forward tip of the probe head for holding the sense end of the thermocouple.

9. An air data probe as recited in claim 7 , further comprising a strut extending from the aft base of the probe head, wherein the thermocouple extends from the forward tip of the probe head to a base of the strut and terminates in a thermocouple connector.

10. An air data probe as recited in claim 7 , further comprising a heater coil positioned within the probe head, wherein the thermocouple includes a thermocouple coil, wherein windings of the thermocouple coil are wound between windings of the heater coil.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 11, 2019
From: GOLLY, TIMOTHY T.; SEIDEL, GREG; JOHNSON, PAUL R.
To: ROSEMOUNT AEROSPACE INC.
Reel/Frame 048856/0191 →
Continuity (3)
Division 15067650 · Mar 11, 2016
Provisional Application 62137080 · Mar 23, 2015
Related Publication 20190202576A1 · Jul 4, 2019
Cited By (3)
US 12,455,295 US 12,535,499 US 12,681,036