Patent classifications
B23P15/28
Blade for a cutting instrument, scalpel holder for a blade, and method for producing a blade
A blade for a cutting instrument, in particular for medical use, includes a first ceramic layer, a second ceramic layer, and a heating device arranged between the first ceramic layer and the second ceramic layer.
Blade for a cutting instrument, scalpel holder for a blade, and method for producing a blade
A blade for a cutting instrument, in particular for medical use, includes a first ceramic layer, a second ceramic layer, and a heating device arranged between the first ceramic layer and the second ceramic layer.
Tool having a boron doped diamond coating
To provide a tool that ensures improved durability even when a diamond coating containing boron is formed. A diamond coating (40) includes a first layer (41) that is formed as a layer on a surface layer side of the diamond coating (40) and is regarded as containing no boron, and a second layer (42) positioned on a side of a base material (30) with respect to the first layer (41) and contains at least 1000 ppm or more of the boron. Since the first layer (41) with a larger compressive stress is formed on the surface layer of the diamond coating (40), a crack generation from the surface layer side of the diamond coating (40) during the process can be reduced. Consequently, the durability of a tool (1) can be improved even when the diamond coating (40) containing 1,000 ppm or more of boron is formed.
METHOD FOR IMPROVING THE AERODYNAMIC BEHAVIOR OF ROTORCRAFT BLADES DURING HOVERING FLIGHT BY MOVING THE LEADING EDGE OF THE AERODYNAMIC PROFILES OF THESE BLADES
A method for improving a blade in an end zone of the blade, spanwise along the blade, and such an improved blade and a rotor comprising the improved blades. The leading edge of the aerodynamic profiles situated in the end zone is shifted from the upper surface half-profile towards the lower surface half-profile, then the leading edge sections of the two half-profiles are modified in order to connect the leading edge to the intermediate sections of the two half-profiles. Next, the blade is manufactured according to the modified aerodynamic profiles. Consequently, the negative camber of the aerodynamic profiles of the blade is thus increased, helping improve the aerodynamic performances of the blade during hovering flight.
METHOD FOR IMPROVING THE AERODYNAMIC BEHAVIOR OF ROTORCRAFT BLADES DURING HOVERING FLIGHT BY MOVING THE LEADING EDGE OF THE AERODYNAMIC PROFILES OF THESE BLADES
A method for improving a blade in an end zone of the blade, spanwise along the blade, and such an improved blade and a rotor comprising the improved blades. The leading edge of the aerodynamic profiles situated in the end zone is shifted from the upper surface half-profile towards the lower surface half-profile, then the leading edge sections of the two half-profiles are modified in order to connect the leading edge to the intermediate sections of the two half-profiles. Next, the blade is manufactured according to the modified aerodynamic profiles. Consequently, the negative camber of the aerodynamic profiles of the blade is thus increased, helping improve the aerodynamic performances of the blade during hovering flight.
IN-MOLD INJECTION MOLDING PROCESS FOR PCBA SOFT MATERIAL
The present disclosure provides an in-mold injection molding process for a Printed Circuit Board Assembly (PCBA) soft material, including the following steps: 1) preheating a Polyethylene Terephthalate (PET) thin film; 2) printing patterns; 3) preparing a diaphragm A; 4) laminating a diaphragm on a Flexible Printed Circuit (FPC) board; 5) scraping printing ink; 6) scraping an adhesive; 7) preparing an inner diaphragm B; and 8) placing prepared diaphragm A and FPC board laminated diaphragm in a mold cavity of an injection mold of a Haitian 130T injection molding machine, preheating injection mold to 30° C., and injecting Thermoplastic Polyurethane (TPU) resin through an injection hole, so that diaphragm A is on an outer side of a product mobile phone protective shell, FPC board laminated diaphragm is on an inner side of the product mobile phone protective shell, and temperature of the TPU resin is at 180° C.
IN-MOLD INJECTION MOLDING PROCESS FOR PCBA SOFT MATERIAL
The present disclosure provides an in-mold injection molding process for a Printed Circuit Board Assembly (PCBA) soft material, including the following steps: 1) preheating a Polyethylene Terephthalate (PET) thin film; 2) printing patterns; 3) preparing a diaphragm A; 4) laminating a diaphragm on a Flexible Printed Circuit (FPC) board; 5) scraping printing ink; 6) scraping an adhesive; 7) preparing an inner diaphragm B; and 8) placing prepared diaphragm A and FPC board laminated diaphragm in a mold cavity of an injection mold of a Haitian 130T injection molding machine, preheating injection mold to 30° C., and injecting Thermoplastic Polyurethane (TPU) resin through an injection hole, so that diaphragm A is on an outer side of a product mobile phone protective shell, FPC board laminated diaphragm is on an inner side of the product mobile phone protective shell, and temperature of the TPU resin is at 180° C.
Method for improving the aerodynamic behavior of rotorcraft blades during hovering flight by moving the leading edge of the aerodynamic profiles of these blades
A method for improving a blade in an end zone of the blade, spanwise along the blade, and such an improved blade and a rotor comprising the improved blades. The leading edge of the aerodynamic profiles situated in the end zone is shifted from the upper surface half-profile towards the lower surface half-profile, then the leading edge sections of the two half-profiles are modified in order to connect the leading edge to the intermediate sections of the two half-profiles. Next, the blade is manufactured according to the modified aerodynamic profiles. Consequently, the negative camber of the aerodynamic profiles of the blade is thus increased, helping improve the aerodynamic performances of the blade during hovering flight.
Method for improving the aerodynamic behavior of rotorcraft blades during hovering flight by moving the leading edge of the aerodynamic profiles of these blades
A method for improving a blade in an end zone of the blade, spanwise along the blade, and such an improved blade and a rotor comprising the improved blades. The leading edge of the aerodynamic profiles situated in the end zone is shifted from the upper surface half-profile towards the lower surface half-profile, then the leading edge sections of the two half-profiles are modified in order to connect the leading edge to the intermediate sections of the two half-profiles. Next, the blade is manufactured according to the modified aerodynamic profiles. Consequently, the negative camber of the aerodynamic profiles of the blade is thus increased, helping improve the aerodynamic performances of the blade during hovering flight.
Cutting tool and method for manufacturing a cutting tool
A cutting tool, in particular for machining metal, is described. It comprises a tool main body that has at least one interface for receiving a cutting insert that can be attached to the tool main body. At least one cooling duct is provided in the tool main body and has, at its end on the interface side, an outlet section with an elongate outlet cross-section on the interface side. The tool main body is manufactured at least in sections by means of a generative manufacturing process. A method for manufacturing such a cutting tool is also presented.