Devices for minimizing losses in fluid conduits
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1. A DEVICE TO MINIMIZE LOSSES IN A FLUID CONDUIT AT THE PASSAGE FROM A FIRST SECTION IN WHICH THE FLUID FOLLOWS A SUBSTANTIALLY CIRCULAR PATH ABOUT A CENTER, TO A SECOND SECTION IN WHICH THE FLUID FOLLOWS A SUBSTANTIALLY RECTILINEAR PATH SUBSTANTIALLY TANGENTIAL TO SAID CIRCULAR PATH, OR VICE VERSA, COMPRISING A STATIONARY VANE DISPOSED AGAINST THE SIDE OF SAID SECOND PORTION OF SAID CONDUIT NEAREST TO THE CENTER OF SAID CIRCULAR PATH IN CLOSE PROXIMITY TO THE END OF SAID SECOND SECTION NEAREST TO SAID FIRST SECTION, THE EXPOSED SIDE OF SAID VANE ELEMENT HAVING THE CONTOUR OF THE LOW-PRESSURE SIDE OF AN AIRCRAFT WING;
- AT LEAST ONE MOVABLE VANE HAVING THE FULL CONTOUR OF AN AIRCRAFT WING, DISPOSED IN SAID CONDUIT BETWEEN SAID STATIONARY VANE AND THE OPPOSED SIDE OF SAID CONDUIT;
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1. A DEVICE TO MINIMIZE LOSSES IN A FLUID CONDUIT AT THE PASSAGE FROM A FIRST SECTION IN WHICH THE FLUID FOLLOWS A SUBSTANTIALLY CIRCULAR PATH ABOUT A CENTER, TO A SECOND SECTION IN WHICH THE FLUID FOLLOWS A SUBSTANTIALLY RECTILINEAR PATH SUBSTANTIALLY TANGENTIAL TO SAID CIRCULAR PATH, OR VICE VERSA, COMPRISING A STATIONARY VANE DISPOSED AGAINST THE SIDE OF SAID SECOND PORTION OF SAID CONDUIT NEAREST TO THE CENTER OF SAID CIRCULAR PATH IN CLOSE PROXIMITY TO THE END OF SAID SECOND SECTION NEAREST TO SAID FIRST SECTION, THE EXPOSED SIDE OF SAID VANE ELEMENT HAVING THE CONTOUR OF THE LOW-PRESSURE SIDE OF AN AIRCRAFT WING;
- AT LEAST ONE MOVABLE VANE HAVING THE FULL CONTOUR OF AN AIRCRAFT WING, DISPOSED IN SAID CONDUIT BETWEEN SAID STATIONARY VANE AND THE OPPOSED SIDE OF SAID CONDUIT;
- AT LEAST ONE MOVABLE VANE HAVING THE FULL CONTOUR OF AN AIRCRAFT WING, DISPOSED IN SAID CONDUIT BETWEEN SAID STATIONARY VANE AND THE OPPOSED SIDE OF SAID CONDUIT;
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