A moving-vane angle of attack probe is provided. The moving-vane angle of attack probe comprises: a vane having opposed first and second vane surfaces that define a leading edge and a trailing edge, the first and second vane surfaces, each extending between the leading edge and the trailing edge; a
A moving-vane angle of attack probe is provided. The moving-vane angle of attack probe comprises: a vane having opposed first and second vane surfaces that define a leading edge and a trailing edge, the first and second vane surfaces, each extending between the leading edge and the trailing edge; a first vane opening located on the leading edge; at least one exhaust opening; a vane conduit extending between the first vane opening and the exhaust opening such that the first vane opening and the exhaust opening are in fluid communication, the vane conduit defining at least an interior chamber between the first and second vane surfaces; and a pitot-tube located within the interior chamber such that in use it receives air that enters the interior chamber via the first vane opening.
대표청구항▼
1. A moving-vane angle of attack probe comprising: a vane having opposed first and second vane surfaces that define a leading edge and a trailing edge, the first and second vane surfaces, each extending between the leading edge and the trailing edge;a first vane opening located on the leading edge;a
1. A moving-vane angle of attack probe comprising: a vane having opposed first and second vane surfaces that define a leading edge and a trailing edge, the first and second vane surfaces, each extending between the leading edge and the trailing edge;a first vane opening located on the leading edge;at least one exhaust opening;a vane conduit extending between the first vane opening and the exhaust opening such that the first vane opening and the exhaust opening are in fluid communication, the vane conduit defining at least an interior chamber between the first and second vane surfaces; anda pitot-tube located within the interior chamber such that in use it receives air that enters the interior chamber via the first vane opening. 2. A moving-vane angle of attack probe according to claim 1, wherein at least a portion of the vane conduit comprises an upper interior chamber wall, a lower interior chamber wall, a first interior chamber sidewall and a second interior chamber sidewall which together define the interior chamber. 3. A moving-vane angle of attack probe according to claim 2, wherein the exhaust opening is located on the trailing edge, and wherein at least one of the upper interior chamber wall, lower interior chamber wall, first interior chamber sidewall and second interior chamber sidewall extends to the trailing edge. 4. A moving-vane angle of attack probe according to claim 1, wherein the first vane opening is a slot opening configured to extend along the leading edge. 5. A moving-vane angle of attack probe according to claim 2, wherein the pitot-tube comprises: a first shielding wall extending substantially between the first and second sidewalls of the interior chamber;a second shielding wall extending substantially between the first and second sidewalls of the interior chamber, wherein the first shielding wall and the second shielding wall are spaced apart from each other to define a first sensor opening therebetween;a rear wall extending between the first shielding wall and the second shielding wall, and substantially between the first and second sidewalls of the interior chamber; anda first pressure conduit located between the first sensor opening and the rear wall, wherein the first pressure conduit is configured to transmit a pressure between the first and second shielding walls. 6. A moving-vane angle of attack probe according to claim 5, wherein the first sensor opening faces the first vane opening. 7. A moving-vane angle of attack probe according to claim 5, wherein first and second bypass channels are defined between the first shielding wall and the lower interior chamber wall, and the second shielding wall and the upper interior chamber wall respectively, and wherein the bypass channels are configured such that, in use, a portion of the air that enters the interior chamber is directed along the first and second bypass channels without entering the pitot-tube. 8. A moving-vane angle of attack probe according to claim 1, wherein the leading edge is at an angle to an axis of rotation of the vane. 9. A moving-vane angle of attack probe according to claim 1, wherein the vane conduit tapers inwardly as it extends from the vane opening. 10. A moving-vane angle of attack probe according to claim 1, further comprising at least a first static pressure system, said first static pressure system comprising at least a first static pressure port that opens through one of the first and second vane surfaces, and a first static pressure conduit in fluid communication with the first static pressure port. 11. A moving-vane angle of attack probe according to claim 10, wherein the first static pressure system further comprises a first manifold internal to the vane, wherein the first static pressure port is configured to open into the first manifold, wherein the first static pressure conduit is configured to open into the first manifold, and wherein the first static pressure conduit is configured to transmit a static pressure in the first manifold. 12. A moving-vane angle of attack probe according to claim 11 wherein the first static pressure system further comprises a second static pressure port, and wherein the first static pressure port opens through the first vane surface, and the second static pressure port opens through the second vane surface, and wherein the second static pressure port opens into the first manifold. 13. A moving-vane angle of attack probe according to claim 10, further comprising a second static pressure system, wherein the second static pressure system comprises a third static pressure port that opens through one of the first and second vane surfaces, and a second static pressure conduit in fluid communication with the third static pressure port. 14. A moving-vane angle of attack probe according to claim 10, wherein at least the first static pressure port is located in a depression in the first or second vane surface, and wherein preferably each static pressure port is located in a separate depression in the first or second vane surface. 15. A moving-vane angle of attack probe according to claim 1, further comprising an electronics assembly for taking angle of attack and/or pressure readings, the electronics assembly having an external housing, wherein the vane is connected to the electronics assembly external housing by a pivot, and wherein the vane is configured to rotate relative to the electronics assembly external housing. 16. A moving-vane angle of attack probe according to claim 15, further comprising a counterweight system located inside the electronics assembly external housing, wherein the counterweight system is fixedly connected to the vane through the pivot, and wherein the first conduit is configured to transmit the pressure between the first and second shielding walls through the pivot and to a first pressure sensor located on the counterweight system in the electronics assembly external housing. 17. A moving-vane angle of attack probe comprising: a vane having opposed first and second vane surfaces that define a leading edge and a trailing edge, the first and second vane surfaces, each extending between the leading edge and the trailing edge;a first depression formed in the first vane surface; anda first static pressure system, said first static pressure system comprising at least a first static pressure port configured to open through said first vane surface in the region of said first depression, and a first static pressure conduit configured to transmit a static pressure;wherein the first depression is configured such that, in use, air flowing over said first vane surface undergoes a change in pressure in the region of said first static pressure port. 18. A moving-vane angle of attack probe according to claim 17, wherein the first static pressure system further comprises a first manifold internal to the vane, wherein the first static pressure port is configured to open into the first manifold, and wherein the first static pressure conduit is configured to open into the first manifold and configured to transmit a static pressure in the first manifold. 19. A moving-vane angle of attack probe according to claim 18, further comprising a second depression formed in the second vane surface, wherein the first static pressure system further comprises a second static pressure port configured to open through said second vane surface in the region of said second depression, and wherein the second depression is configured such that, in use, air flowing over said second vane surface undergoes a change in pressure in the region of said second static pressure port. 20. A moving-vane angle of attack probe according to claim 17, further comprising a third depression in either the first or second vane surface, and a second static pressure system, said second static pressure system comprising at least a third static pressure port configured to open through either the first or second vane surface in the region of said third depression, wherein the third depression is configured such that, in use, air flowing over said first or second vane surface undergoes a change in pressure in the region of said third static pressure port.
연구과제 타임라인
LOADING...
LOADING...
LOADING...
LOADING...
LOADING...
이 특허에 인용된 특허 (9)
Beigbeder Grard (Paris FRX) Leblond Henri (Versailles FRX), Aircraft probe for measuring aerodynamic parameters of amient flow.
Seidel, Greg A.; Cronin, Dennis J.; Mette, John H.; Koosmann, Mark R.; Schmitz, James A.; Fedele, John R.; Kromer, Dana A., Multi-function air data sensing probe having an angle of attack vane.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.