IP Library › Granted Patent US 12,198,839
Granted Patent B2
US 12,198,839 · App. 17/578,653 · Granted Jan 14, 2025

Pitot tube heater assembly

Inventors: Robin Jacob (Karnataka, IN); Guru Prasad Mahapatra (Karnataka, IN); Paul Robert Johnson (Prior Lake, MN)
Assignee: ROSEMOUNT AEROSPACE INC.
H01C17/04F16L33/223G01F15/10G01L19/04G01P5/165
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Quick Facts
Patent No.
US 12,198,839
App. No.
17/578,653
Granted
Jan 14, 2025
Kind
B2
Abstract

A pitot tube includes an outer tube extending from a first tube end to second tube end. The second tube end defines a tip portion of the pitot tube. A tube sleeve is located inside of the outer tube and defines a tube passage extending from the first tube end to the second tube end. A heating element is located between the outer tube and the tube sleeve. The heating element is isolated from airflow into the tube passage. A method of forming a pitot tube includes installing a heating element to an outer surface of a tube sleeve, the tube sleeve defining a tube passage of the pitot tube. The tube sleeve is secured in an outer tube such that the heating element is between the tube sleeve and the outer tube and is isolated from airflow through the tube passage.

Claims (15)

1. A method of forming a pitot tube, comprising:

installing a heating element to an outer surface of a tube sleeve, the tube sleeve defining a tube passage of the pitot tube;

securing the tube sleeve in an outer tube such that the heating element is between the tube sleeve and the outer tube and is isolated from airflow through the tube passage;

plugging a tip portion of the pitot tube after securing the tube sleeve to the outer tube; and

forming a selected tip profile shape in the tip portion.

2. The method of claim 1 , wherein installing the heating element to the tube sleeve comprises:

forming one or more sleeve grooves in the outer surface of the tube sleeve; and

installing the heating element in the one or more grooves.

3. The method of claim 1 , wherein the heating element is a heater coil.

4. The method of claim 1 , further comprising forming the tube sleeve by additive manufacturing.

5. The method of claim 1 , further comprising:

applying a layer of braze paste to the tube sleeve prior to securing the tube sleeve into the outer tube; and

securing the tube sleeve to the outer tube via brazing.

6. The method of claim 1 , further comprising forming one or more drain openings in the pitot tube, extending from the tube passage through the tube sleeve and through the outer tube for egress of fluid from the tube passage.

7. The method of claim 1 , wherein the selected tip profile shape is formed by machining.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 19, 2022
From: JOHNSON, PAUL ROBERT
To: ROSEMOUNT AEROSPACE INC.
Reel/Frame 058693/0202 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 19, 2022
From: JACOB, ROBIN; MAHAPATRA, GURU PRASAD
To: GOODRICH AEROSPACE SERVICES PRIVATE LIMITED
Reel/Frame 058693/0217 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 19, 2022
From: GOODRICH AEROSPACE SERVICES PRIVATE LIMITED
To: ROSEMOUNT AEROSPACE INC.
Reel/Frame 058693/0234 →
Priority Claims (1)
IN 201811037757 · Oct 5, 2018 · national
Continuity (2)
Division 16578561 · Sep 23, 2019
Related Publication 20220136884A1 · May 5, 2022
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