Method and System for Cryptographic Decision-making of Set Membership

    公开(公告)号:US20170359177A1

    公开(公告)日:2017-12-14

    申请号:US15542211

    申请日:2015-02-13

    CPC classification number: H04L9/3026 H04L9/0643 H04L9/3033 H04L9/3218

    Abstract: A cryptographic decision-making of set membership is a method or system which make a secure decision-making for positive membership e∈S or negative membership e∉S in an unforgeable and non-repudiation way for any element e and a set S. The proposed method of the present invention comprises: acquire a set U={e1, . . . , en} and map each element ei in U into a random point vi in a cryptography space; acquire a set S={e′1, . . . , e′m}⊂U, determine a random point v′i corresponding to each element e′i in the set S, and construct a function ƒS(x) according to all random points v′i; introduce a random secret γ to generate ƒS(γ) by using the function ƒS(x), and produce a public parameter mpk according to the random secret γ; and generate the cryptographic representation of set S by using the function ƒS(γ) and the public parameter mpk. In the embodiments, we provide two kinds of cryptographic representations of set, including Poles-based Aggregation and Zeros-based Aggregation, to make the decision on positive membership ei∈S and negative membership ei∉S.

    VIBRATION CONTROL METHOD FOR FLAPPING-WING MICRO AIR VEHICLES

    公开(公告)号:US20170297702A1

    公开(公告)日:2017-10-19

    申请号:US15467449

    申请日:2017-03-23

    CPC classification number: B64C33/02 B64C13/16

    Abstract: The present invention provides a method for controlling the oscillation of flapping-wing air vehicle, which comprises the following steps: calculating the kinetic energy, potential energy and virtual work of the system using the flexible wing with the two-degree of freedom as the research object; establishing system dynamics model based on the Hamilton's principle; setting the boundary control rate according to said system dynamics model wherein said boundary control rate includes F(t) and M(t), said F(t) is the inputted boundary control force, and said M(t) is the inputted boundary torque; and controlling the flexible wings according to the system dynamics model in combination with the boundary control rate. The present invention establishes the system dynamics model based on the Hamilton's principle, set the boundary control rate according to said system dynamics model, sufficiently considers the situation of distributed disturbance occurring at the boundary and effectively prevents the flexible wings deformation caused by the external disturbances.

    Kiln system and method for firing ceramsite and by-producing waste heat by utilizing raw materials with heating values

    公开(公告)号:US12264879B2

    公开(公告)日:2025-04-01

    申请号:US17585591

    申请日:2022-01-27

    Inventor: Yu Li Changqing Yao

    Abstract: A kiln system is provided, including a drying section, a preheating section, a firing section, a soaking section, a cooling section, and a decarburization section arranged between the drying section and the preheating section. The decarburization section includes an ignition zone, a hot air combustion/pyrolysis zone, and a waste heat recovery pipeline. A heat source is introduced into the ignition zone so that the temperature of the ceramsite of the raw materials with heating values in the zone is 400° C. to 900° C. The hot air combustion/pyrolysis zone is configured for combusting or pyrolyzing carbon-containing materials and organic components in the raw materials with heating values in the ceramsite. The waste heat recovery pipeline is configured for discharging decarburization exhaust gas and recovering heat released after the raw materials with heating values in the ceramsite are combusted or pyrolyzed in the decarburization exhaust gas.

    High-strength and high-plasticity titanium matrix composite and preparation method thereof

    公开(公告)号:US12226826B2

    公开(公告)日:2025-02-18

    申请号:US17768737

    申请日:2020-08-17

    Abstract: The present invention provides a high-strength and high-plasticity titanium matrix composite and a preparation method thereof. The preparation method includes: preparing high-oxygen hydride-dehydride titanium powder using a high-temperature rotary ball grinding treatment process, in which the prepared hydride-dehydride titanium powder has a particle size of 10-40 μm, and has an oxygen content of 0.8-1.5 wt. %; preparing high-purity ultra-fine oxygen adsorbent powder using a wet grinding method of high-energy vibration ball grinding treatment process; in which a purity of the oxygen adsorbent powder is ≥99.9%, and a particle size of the oxygen adsorbent powder is ≤8 μm; mixing the high-oxygen hydride-dehydride titanium powder with the oxygen adsorbent powder in a protective atmosphere, and then press-forming the powder obtained after mixing to obtain a raw material blank; and performing atmosphere protective sintering treatment on the raw material blank to obtain a titanium matrix composite. The method prepares a titanium matrix composite reinforced by in-situ self-generating multi-scale Ca—Ti—O, TiC, TiB particles. The microstructure and grains are effectively refined, and the strength and plasticity of the material are significantly improved.

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