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55results about How to "Ratio" patented technology

Shaving head with pivotable shaving unit

A shaving head (3) for a shaving apparatus comprises: a support structure (33) including a coupling structure (29) for coupling the shaving head to the main housing (2) of the shaving apparatus (1); a shaving unit (8) comprising a shaving unit frame (27) and a skin contacting face (12) and at least two cutting units (10) each having an external cutting member (16) and an internal cutting member (20) which is rotatable relative to the external cutting member; a pivot structure (44, 46) for allowing the shaving unit to pivot relative to the support structure; and a central driving member (24) arranged to be driven by the motor (6) when the shaving head is coupled to the main housing. Each internal cutting member is rotatable by the central driving member via a separate cutter driving member (26), the central driving member transmitting a driving force to each cutter driving member in a transmission location L The pivot structure is located in an internal area of the shaving head located between the skin contacting face, the cutter driving members and the transmission locations of the central driving member. The central driving member and the cutter driving members each have a bearing (48, 261) which is connected to the frame of the shaving unit to allow the central driving member and the cutter driving members to pivot together with the shaving unit relative to the support structure.
Owner:KONINKLJIJKE PHILIPS NV

Iodine satellite thruster working medium supply system and application method thereof

The invention discloses an iodine satellite thruster working medium supply system. The iodine satellite thruster working medium supply system comprises a propellant storage tank, wherein the propellant storage tank is arranged at the rear end of a thruster and communicates with a main pipe. The main pipe is divided into two branch pipes through a three-way valve. The two branch pipes are connectedwith a negative pole and a positive pole of the thruster correspondingly. The propellant storage tank, the main pipe and the two branch pipes are each provided with a heating device. The two branch pipes are each provided with a proportional flow rate control valve. The invention further discloses an application method of the iodine satellite thruster working medium supply system. The applicationmethod comprises the specific steps that the propellant storage tank is heated to 90 DEG C, and the main pipe and the branch pipes are each heated to 125 DEG C; and the branch pipe flow rates are controlled through the proportional flow rate control valves correspondingly, and furthermore, the flow rates of a working medium entering the negative pole and the positive pole of the thruster are controlled. The iodine satellite thruster working medium supply system and the application method thereof have the beneficial effects that the iodine working medium supply system is provided, flow of theiodine working medium can be adjusted through heating, and the system works at the relatively-low temperature; and the system is easy and reliable to apply, and the high specific impulse and propulsive efficiency required by propelling of a cubesat can be continuously generated.
Owner:HENAN POLYTECHNIC UNIV

Pneumatic tire with tread having cutaway portions formed in center rib

ActiveUS8474496B2Improve on-ice performanceLarge ratioTyre tread bands/patternsNon-skid devicesMechanical engineeringTread
A pneumatic tire includes a pair of first circumferential main grooves formed in the center region of a tread, a pair of second circumferential main grooves formed respectively outward of the corresponding first main grooves, a plurality of first lug grooves which each extend from one of the two shoulder ends of the tread inward in the tire-width direction and communicate with the corresponding first main groove, a plurality of second lug grooves alternately arranged in the tire circumferential direction which each extend from one of the two shoulder ends of the tread inward in the tire-width direction but do not communicate with the corresponding first main groove, a center rib defined between the pair of first main grooves and extends continuously in the tire circumferential direction, a shoulder block row defined between each of the second main grooves and a corresponding one of the shoulder ends and includes a plurality of blocks, and an intermediate block row defined between each of the first main grooves and a corresponding one of the second main grooves. Each intermediate block row includes long blocks each of which has a tire-circumferential-direction length equivalent to the total length of each two blocks included in the corresponding shoulder block row.
Owner:YOKOHAMA RUBBER CO LTD
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