Abstract: A swirling flow identification apparatus includes an eigenequation calculation section 3 and a swirl axis calculation section 4. The eigenequation calculation section 3, based on velocity data of a fluid at a coordinate point, calculates an eigenvalue through an eigenequation concerning the coordinate point and the velocity data. The swirl axis calculation section 4, if the eigenvalue is a complex number, defines an imaginary part of the complex number as a swirl function, calculates a coordinate point providing a local maximum value in the swirl function and defines the coordinate point providing the local maximum value as the position of a swirling axis of a swirling flow in the fluid. With this, even under the presence of another flow or a plurality of swirling flow, the swirling flow can be adequately identified by using the velocity vector at each of node points (coordinate points).

Abstract: A swirling flow identification apparatus includes an eigenequation calculation section 3 and a swirl axis calculation section 4. The eigenequation calculation section 3, based on velocity data of a fluid at a coordinate point, calculates an eigenvalue through an eigenequation concerning the coordinate point and the velocity data. The swirl axis calculation section 4, if the eigenvalue is a complex number, defines an imaginary part of the complex number as a swirl function, calculates a coordinate point providing a local maximum value in the swirl function and defines the coordinate point providing the local maximum value as the position of a swirling axis of a swirling flow in the fluid. With this, even under the presence of another flow or a plurality of swirling flow, the swirling flow can be adequately identified by using the velocity vector at each of node points (coordinate points).

Abstract: In a nuclear reactor internal structure, generation and promotion of object-downstream separating vortices are suppressed so that coolant uniformly flows in a reactor core and pressure loss of flow of the coolant is reduced so that the flow of the coolant is stabilized. A lower connecting plate 30 arranged in a lower plenum 8 comprises a ring portion 31 in which an arcuate portion 32 and a cut-off portion are alternately formed. An outer peripheral portion of the ring portion 31 is asymmetric relative to a flow direction of main flow and also asymmetric relative to a separating flow generation direction.

Abstract: In a nuclear reactor internal structure, generation and promotion of object-downstream separating vortices are suppressed so that coolant uniformly flows in a reactor core and pressure loss of flow of the coolant is reduced so that the flow of the coolant is stabilized. A lower connecting plate 30 arranged in a lower plenum 8 comprises a ring portion 31 in which an arcuate portion 32 and a cut-off portion are alternately formed. An outer peripheral portion of the ring portion 31 is asymmetric relative to a flow direction of main flow and also asymmetric relative to a separating flow generation direction.

Abstract: A cross-linked silicone adhesive sheet has stability of peeling surfaces during peeling protective films away from both sides of the sheet. An adhesive sheet of a cross-linked silicone has protective films on both sides of the sheet. The protective films each have a thickness of 100 ?m or less. A force of peeling of the protective films from the sheet is equal to or below 5.0 N/m. The difference between peeling forces of the films is equal to or exceeds 0.2 N/m. A method of manufacturing the adhesive sheet of a cross-linked silicone includes the steps of forming a film-like body by placing a cross-linkable silicone composition in a layer having a thickness of 100 ?m or less between two protective films of different materials and then cross-linking the composition.

Abstract: An object of the present invention is to provide a practical gear and gear train which can be used in an actual gear drive system. Another object of the present invention is to provide a non-circular and asymmetrical gear which is practically used in view of durability, a gear train using that gear, and a barrel finishing machine using that gear. Non-circular and asymmetrical gear 10 has a plurality of tooth profiles 20, each of which comprises a substantially semicircular top curve line 16 and a substantially semicircular bottom curved line 18. A center point 22 of the top curved line 16 is on a pitch line 24, and a center point 26 of the bottom curved line 18 lies inside the pitch line 24.

Abstract: A cross-linked silicone adhesive sheet has stability of peeling surfaces during peeling protective films away from both sides of the sheet. An adhesive sheet of a cross-linked silicone has protective films on both sides of the sheet. The protective films each have a thickness of 100 &mgr;m or less. A force of peeling of the protective films from the sheet is equal to or below 5.0 N/m. The difference between peeling forces of the films is equal to or exceeds 0.2 N/m. A method of manufacturing the adhesive sheet of a cross-linked silicone includes the steps of forming a film-like body by placing a cross-linkable silicone composition in a layer having a thickness of 100 &mgr;m or less between two protective films of different materials and then cross-linking the composition.

Abstract: An object of the present invention is to provide a practical gear and gear train which can be used in an actual gear drive system. Another object of the present invention is to provide a non-circular and asymmetrical gear which is practically used in view of durability, a gear train using that gear, and a barrel finishing machine using that gear. Non-circular and asymmetrical gear 10 has a plurality of tooth profiles 20 in which an addendum circle 16 of a substantially semicircular shape is connected to a dedendum circle 18 of a substantially semicircular shape. A center point 22 of the addendum circle 16 is on a pitch line 24, and a center point 26 of the dedendum circle 18 lies inside the pitch line 24.