Abstract: A leading-edge high-lift device according to an embodiment of the present invention is a leading-edge high-lift device that is deployable and retractable from/into a fixed leading edge of a main wing of an aircraft and includes a slat main body and a buffering portion. The slat main body includes a leading edge portion, a trailing edge portion that forms a gap between a trailing edge portion and the main wing during deployment, a cusp portion formed at a lower edge of the leading edge portion, a cove portion formed between the cusp portion and the trailing edge portion, and an inboard end surface that is formed between the leading edge portion and the cove portion and is positioned on a fuselage side of the aircraft. The buffering portion is provided at an inboard end portion of the slat main body including the inboard end surface and an inboard-side surface of the cove portion and reduces pressure fluctuations in airflow on the inboard end surface or the inboard-side surface of the cove portion.

Abstract: A noise reduction apparatus, an aircraft, and a noise reduction method capable of increasing the amount of noise reduction are provided. The noise reduction apparatus 1 includes a porous plate 2 disposed to face a fluid flow, the porous plate 2 including a bend region 5 bent toward an upstream side of the fluid flow. The bend region 5 is provided at the end portion 6 of the porous plate 2, and has a concave R-shape on an upstream side of the fluid flow.

Abstract: [Object] To provide a noise reduction apparatus, an aircraft, and a noise reduction method capable of increasing the amount of noise reduction. [Solving Means] The noise reduction apparatus 1 includes a porous plate 2 disposed to face a fluid flow, the porous plate 2 including a bend region 5 bent toward an upstream side of the fluid flow. The bend region 5 is provided at the end portion 6 of the porous plate 2, and has a concave R-shape on an upstream side of the fluid flow. Although the direction of the fluid flow is typically deflected toward the outside from the center of the porous plate 2 due to the porous plate 2, the deflected fluid easily passes through the porous plate 2 since the porous plate has the bend region 5. Thus, the shear layer of the fluid flow is weakened, the noise induced by the vortex is reduced, and it is possible to increase the reduction amount of noise.

Abstract: A manufacturing method of a silicon nozzle plate, having; a film forming process to provide the film representing an etching mask for etching the silicon substrate on a surface of the silicon substrate; a pattern film forming to form a pattern film by partially removing the film based on a nozzle hole forming pattern and an outer shape forming pattern; a silicon substrate etching process to form nozzle holes based on the nozzle hole forming pattern representing the etching mask, and to form a half etching portion at least in a part of the silicon substrate based on the outer shape forming pattern; and a silicon substrate separating process to separate the silicon substrate by splitting along the half etching portion.

Abstract: A manufacturing method of a silicon nozzle plate, having; a film forming process to provide the film representing an etching mask for etching the silicon substrate on a surface of the silicon substrate; a pattern film forming to form a pattern film by partially removing the film based on a nozzle hole forming patter and an outer shape forming pattern; a silicon substrate etching process to form nozzle holes based on the nozzle hole forming pattern representing the etching mask, and to form a half etching portion at least in a part of the silicon substrate based on the outer shape forming patter; and a silicon substrate separating process to separate the silicon substrate by splitting along the half etching portion.