Differential pressure flow probe

• US 4,703,661 A
• Filed: 03/11/1986
• Issued: 11/03/1987
• Est. Priority Date: 04/11/1985
• Status: Expired due to Term

• Current Assignee: Intra-Automation GmbH Mess-Und Regelinstrumente Von-Werth-Str 11C D-4053 Juchen 2
• Original Assignee: INTRA-AUTOMATION GmbH Meß- und Regelinstrumente
• Inventors: Evers, Ernst
• Primary Examiner(s): Goldstein, Herbert
• Application Number:
  US06/838,609
• Time in Patent Office: 602 Days
• Field of Search: 73/861.65, 73/861.66
• US Class Current: 73/861.66
• CPC Class Codes: G01F 1/46 Pitot tubes

Abstract

A differential pressure flow sensor to measure the differential pressure in fluid flow in a pipe including an elongated pressure tube designed as an elongated hollow tube which is provided at its leading edge with at least one dynamic-pressure aperture and a sensor for the static pressure with at least one sensor aperture formed in the rear edge thereof. The sensor aperture being located in the wake of a body, either a separate body or a part of the hollow elongated tube, with front surfaces swept back from a forward tip and which are provided with detachment edges for the lateral detachment of the incident fluid flow without there being subsequent reattachment. In order to obtain the best test results from this differential pressure flow sensor, arcuate recesses are formed in the front surfaces at a distance from the outer limits for forming detachment edges for deflecting fluid from the planes of the front surfaces.

Claims

1. A differential pressure flow probe for measuring the difference in the fluid flow in a pipe system, comprising:

(a) a hollow elongated stagnation tube,

(b) said stagnation tube including leading and trailing faces,

(c) said leading face having at least one dynamic-pressure aperture formed therein,

(d) a probe for sensing static pressure,

(e) said probe being secured to said hollow stagnation tube adjacent said trailing face,

(f) said probe including front and rear faces,

(g) said probe having an aperture formed in said rear face, said probe including front surfaces extending angularly from opposing ends of said front face such that said front surfaces intersect the line of flow of fluid in the pipe,

(h) said front surfaces of said probe including a concave recess formed therein for directing fluid from the planes of said front surfaces, and

(i) said front surfaces of said probe further include a substantially planar surface extending from one end of said concave recess, whereby the intersection of said substantially planar surface and said concave recess forms a detachment edge for providing lateral detachment of the incident fluid flow without there being subsequent reattachment.

2. A differential pressure flow probe as in claim 1, wherein:

(a) tangents to inner edges of said concave recesses subtend an angle of at most 40°

.

3. A differential pressure flow probe as in claim 2, wherein:

(a) tangents to inner edges of said concave recesses subtend an angle of at least 20°

.

4. A differential pressure flow probe as in claim 1, wherein:

(a) the angle between tangents to outer edges of said concave recesses and said substantially planar surfaces extending therefrom is at least 20°

.

5. A differential pressure flow probe as in claim 1, wherein:

(a) said concave recesses each extend across approximately 60 to 80% of said front surfaces.

6. A differential pressure flow probe as in claim 1, wherein:

(a) said hollow elongated stagnation tube includes a punched or drawn segment.

7. A differential pressure flow probe as in claim 1, wherein:

(a) said front surfaces subtend a sweep back angle of approximately 90°

.

8. A differential pressure flow probe as in claim 1, wherein:

(a) the tangents to inner edges of said concave recesses subtend an angle from zero to 60°

.

9. A differential pressure flow probe as in claim 1, wherein:

(a) tangents to outer edges of said concave recesses subtend an anle from 100°

to 180°

.

10. A differential pressure flow probe as in claim 9, wherein:

(a) tangents to outer edges of said concave recesses subtend angle of at least 130°

.

11. A differential pressure flow probe as in claim 9, wherein:

(a) tangents to outer edges of said concave recesses subtend an angle of at most 160°

.

12. A differential pressure flow probe for measuring the difference in fluid flow in a pipe system, comprising:

(a) a hollow elongated stagnation tube,

(b) said stagnation tube including leading and trailing faces,

(c) said leading face having at least one dynamic-pressure aperture formed therein,

(d) a probe for securing static pressure,

(e) said trailing face having a probe aperture formed therein,

(f) said probe being disposed in said hollow stagnation tube for communicating with said probe aperture,

(g) said stagnation tube including front surfaces extending angularly from opposing ends of said leading face such that said front surfaces intersect the line of flow of fluid in the pipe,

(h) said front surfaces include a concave recess formed therein for directing the fluid from the planes of said front surfaces, and

(i) said front surfaces include a substantially planar surface extending from one end of said concave recess whereby the intersection of said substantially planar suface and said concave recess forms a detachment edge for providing lateral detachment of the incident fluid flow without there being subsequent reattachment.

13. A differential pressure flow probe as in claim 12, wherein:

(a) said probe includes a punched or drawn segment.

14. A differential pressure flow probe as in claim 12, wherein:

(a) said front surfaces subtend a sweep back angle of approximately 90°

.

15. A differential pressure flow probe as in claim 12, wherein:

(a) tangents to inner edges of said concave recesses subtend an angle from zero to 60°

.

16. A differential pressure flow probe as in claim 12, wherein:

(a) tangents to outer edges of said concave recesses subtend an angle from 100°

to 180°

.

17. A differential pressure flow probe as in claim 12, wherein:

(a) tangents to outer edges of said concave recesses and said substantially planar surfaces extending therefrom is at least 20°

.

18. A differential pressure flow probe as in claim 12, wherein:

(a) said concave recesses each extend across approximately 60 to 80% of said front surfaces.