Pressure distribution measurement system
View Patent ↗A pressure distribution measurement system for measuring a pressure distribution on a measurement object. A flexible sheet-form pressure detection member includes a plurality of pressure passages extending in parallel and a pressure detection hole opened in each of the pressure passages is affixed to a surface of an outer plate of a main wing W of an airplane. Each of the pressure passages is connected to a pressure measurement device via a pressure pipeline. Because the pressure detection hole is opened in the pressure detection member, that is, the pressure detection hole is not required to be opened in the outer plate of the main wing, the outer plate is not damaged. Further, because the flexible sheet-form pressure detection member conforms well to the three dimensionally curved surface of the outer plate and has a small thickness, the airflow is hardly disturbed at all, thereby enhancing pressure distribution measurement accuracy.
1. A pressure distribution measurement system for measuring a pressure distribution on a surface of a measurement object (W) that moves relative to a fluid, the system comprising:
a flexible sheet-form pressure detection member ( 11 ) fixed to the surface of the measurement object (W), the pressure detection member ( 11 ) having a plurality of pressure passages ( 11 a ) having lengths extending in parallel to a length of the pressure detection member ( 11 ), and a pressure detection hole ( 11 b ) opened in each of the pressure passages ( 11 a ); and
a pressure measurement device ( 20 ),
wherein each of the pressure passages ( 11 a ) is connected to the pressure measurement device ( 20 ) via a pressure pipeline ( 17 ).
2. The pressure distribution measurement system according to claim 1 , wherein the pressure detection member ( 11 ) is extrusion-molded from a synthetic resin.
3. The pressure distribution measurement system according to claim 1 , wherein the pressure distribution member is in a chord direction on an upper face on a main wing of an airplane.
4. The pressure distribution measurement system according to claim 1 , wherein the pressure detection member is a narrow long band-shaped sheet that is detachably mounted to the surface by adhesive.
5. The pressure distribution measurement system according to claim 4 , wherein the pressure detection member is a thin sheet having a thickness of approximately 1 mm.
6. The pressure distribution measurement system according to claim 5 , wherein the pressure detection member is extrusion-molded from a synthetic resin.
7. The pressure distribution measurement system according to claim 1 , wherein the plurality of pressure passages are arranged adjacent to each other in said flexible sheet-form pressure detection member and each pressure detection hole opened in each of the pressure passages is spaced along a length of said pressure detection member by a predetermined distance.
8. The pressure distribution measurement system according to claim 7 , wherein the measurement object is an upper face of a main wing of an airplane and a small interval is provided between adjacent pressure detection holes in a section of a front edge of the wing and larger interval is provided between adjacent pressure detection holes in a section of a rear edge of the wing.
9. The pressure distribution measurement system according to claim 1 , wherein openings at opposite ends of the pressure detection member are hermetically closed by heat welding and flattened for minimizing the influence on airflow.
10. The pressure distribution measurement system according to claim 1 , wherein the measurement object is an upper face of a main wing of an airplane and a maintenance opening is formed along the width thereof whereby the pressure detection member is secured to said maintenance opening for forming a cover therefore.
11. The pressure distribution measurement system according to claim 1 , wherein the pressure passages have lengths extending in parallel to a length of the pressure detection member.
12. The pressure distribution measurement system according to claim 1 , wherein the surface of the measurement object is three-dimensionally curved and the flexible sheet-form pressure detection member is thin enough to conform to the three-dimensionally curved surface of the measurement object.
13. The pressure distribution measurement system according to claim 1 , wherein the measurement object is a wing of an airplane and the flexible sheet-form pressure detection member is thins enough to be affixed to an upper face of the wing of the airplane along a chord line of the wing.
14. A pressure distribution measurement system for measuring a pressure distribution on a surface of a measurement object that moves relative to a fluid, the system comprising:
a flexible sheet-form pressure detection member fixed to the surface of the measurement object;
a plurality of pressure passages formed in the pressure detection member and extending therethrough;
a pressure detection hole opened in each of the pressure passages; and
a pressure measurement device;
wherein each of the pressure passages is connected to the pressure measurement device via a pressure conduit, and
wherein openings at opposite ends of the pressure detection member are hermetically closed by heat welding and flattened for minimizing the influence on airflow.
15. The pressure distribution measurement system according to claim 14 , wherein the pressure detection member is extrusion-molded from a synthetic resin.
16. The pressure distribution measurement system according to claim 14 , wherein the pressure detection member is a narrow long band-shaped sheet that is detachably mounted to the surface by adhesive.
17. The pressure distribution measurement system according to claim 16 , wherein the pressure detection member is a thin sheet having a thickness of approximately 1 mm.
18. The pressure distribution measurement system according to claim 17 , wherein the pressure detection member is extrusion-molded from a synthetic resin with the plurality of pressure passages being formed therein.
19. The pressure distribution measurement system according to claim 14 , wherein the plurality of pressure passages are arranged adjacent to each other in said pressure detection member and each pressure detection hole opened in each of the pressure passages is spaced along a length of said pressure detection member by a predetermined distance.
20. The pressure distribution measurement system according to claim 19 , wherein the measurement object is an upper face of a main wing of an airplane and a small interval is provided between adjacent pressure detection holes in a section of a front edge of the wing and larger interval is provided between adjacent pressure detection holes in a section of a rear edge of the wing.
21. The pressure distribution measurement system according to claim 14 , wherein the measurement object is an upper face of a main wing of an airplane and a maintenance opening is formed along the width thereof whereby the pressure detection member is secured to said maintenance opening for forming a cover therefore.
22. The pressure distribution measurement system according to claim 14 , wherein the surface of the measurement object is three-dimensionally curved and the flexible sheet-form pressure detection member is thin enough to conform to the three-dimensionally curved surface of the measurement object.
23. The pressure distribution measurement system according to claim 14 , wherein the measurement object is a wing of an airplane and the flexible sheet-form pressure detection member is thin enough to be affixed to an upper face of the wing of the airplane along a chord line of the wing.
24. A pressure distribution measurement system for measuring a pressure distribution on a surface of a measurement object that moves relative to a fluid, the system comprising:
a pressure detection member fixed to the surface of the measurement object;
a plurality of pressure passages formed in the pressure detection member and extending therethrough;
a pressure detection hole opened in each of the pressure passages; and
a pressure measurement device;
wherein each of the pressure passages is connected to the pressure measurement device via a pressure conduit, wherein the pressure distribution member is in a chord direction on an upper face on a main wing of an airplane.