中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

280 records (took 0.023 seconds)

    Methane Synthesis Device
    71.
    发明申请
    Methane Synthesis Device 有权

    公开(公告)号：US20220267232A1

    公开(公告)日：2022-08-25

    申请号：US17708838

    申请日：2022-03-30

    Applicant: Japan Aerospace Exploration Agency

    Inventor： Yoshitsugu Sone ,  Omar Mendoza ,  Asuka Shima ,  Takayuki Abe ,  Mitsuhiro Inoue ,  Hiroshige Matsumoto ,  Yuki Terayama ,  Motohiko Sato

    IPC: C07C1/12 ,  C25B9/015 ,  C25B9/77 ,  C25B3/03 ,  C25B11/053 ,  B01J35/04 ,  C25B1/04 ,  C25B15/08

    Abstract: An object is to provide a methane synthesis device having as a whole a reduced size and a simplified configuration. A methane synthesis device 100 is composed of respective components from an end plate 2 at the leftmost side to an end plate 23 at the rightmost side and is compactly assembled by fastening plural bolts and nuts to bring these individual components into tightly contact with each other. The components may be divided into a Sabatier reaction unit of signs 3 to 9, a water electrolysis unit of signs 13 to 19, and other components. Hydrogen gas generated in the water electrolysis unit is mixed with carbon dioxide gas and supplied to the Sabatier reaction unit, and methane is synthesized in the Sabatier reaction unit. The size of the device is reduced as a whole and configuration is simplified by integrally stacking the water electrolysis unit, the Sabatier reaction unit, a carbon dioxide supplying unit, and a hydrogen gas supplying unit.

    Supersonic aircraft and method of reducing sonic booms
    72.
    发明授权
    Supersonic aircraft and method of reducing sonic booms 有权

    公开(公告)号：US11420759B2

    公开(公告)日：2022-08-23

    申请号：US17044178

    申请日：2019-03-25

    Applicant: JAPAN AEROSPACE EXPLORATION AGENCY

    Inventor： Atsushi Ueno ,  Tatsunori Yuhara ,  Masashi Kanamori

    IPC: F02K1/34 ,  B64C5/02 ,  B64C30/00 ,  B64D27/20 ,  B64D29/04

    Abstract: [Object] To provide a supersonic aircraft and a method of reducing sonic booms, by which sonic booms due to engine exhaust can be reduced.
    [Solving Means] A supersonic aircraft includes: a pair of engine nacelles 12R, 12L mounted on a fuselage 11 of an airframe 10; fins 13R, 13L as a pair of shielding plates that inhibits engine exhaust 15 discharged from jet engines (not shown) accommodated in the engine nacelles 12R, 12L from wrapping downward around the airframe 10; and a pair of horizontal tails 14R, 14L disposed behind the engine nacelles 12R, 12L. The fins 13R, 13L are disposed on the horizontal tails 14R, 14L so as to sandwich the engine exhaust 15, respectively.

    Method and apparatus for removing CO2
    73.
    发明授权
    Method and apparatus for removing CO2 有权

    公开(公告)号：US11338242B2

    公开(公告)日：2022-05-24

    申请号：US16956514

    申请日：2017-12-27

    Applicant: Renaissance Energy Research Corporation ,  JAPAN AEROSPACE EXPLORATION AGENCY

    Inventor： Osamu Okada ,  Masaaki Teramoto ,  Tamotsu Nonouchi ,  Nobuaki Hanai ,  Junya Miyata ,  Yasato Kiyohara ,  Masato Sakurai ,  Shinichi Furukawa

    IPC: B01D53/22 ,  B01D69/02 ,  B01D71/60

    Abstract: Provided is a method for removing CO2 comprising: supplying a gas to be processed containing CO2, N2 and O2 to a feed side of a CO2/O2 selective permeation membrane within a temperature range of 15° C. to 50° C.; generating water vapor and supplying the water vapor to the CO2/O2 selective permeation membrane; selectively removing CO2 from the gas to be processed by permeating CO2 in the gas to be processed from the feed side to a permeate side of the CO2 selective permeation membrane selectively to O2 and N2 in the gas to be processed; and using a CO2 facilitated transport membrane having CO2/O2 selectivity and CO2/N2 selectivity within the temperature range as the CO2 selective permeation membrane, the CO2 facilitated transport membrane being configured with a hydrophilic polymer containing an amino acid and a deprotonating agent for preventing protonation of an amino group of the amino acid supported by a porous membrane, wherein a CO2 concentration in the gas to be processed is 3 mol % or less on a dry basis.

    ABNORMALITY DETECTION DEVICE, ABNORMALITY DETECTION METHOD, AND PROGRAM
    75.
    发明申请
    ABNORMALITY DETECTION DEVICE, ABNORMALITY DETECTION METHOD, AND PROGRAM 有权

    公开(公告)号：US20210397175A1

    公开(公告)日：2021-12-23

    申请号：US17288611

    申请日：2019-10-29

    Applicant: Japan Aerospace Exploration Agency

    Inventor： Seiji TSUTSUMI ,  Miki HIRABAYASHI

    IPC: G05B23/02 ,  G01D21/02

    Abstract: An abnormality detection device includes an acquirer configured to acquire a plurality of detection results of a plurality of sensors that have detected a state of a detection target at predetermined time intervals and an estimator configured to estimate a specific sensor among the plurality of sensors on the basis of a plurality of mode information acquisition process data elements for enabling various types of feature extraction according to properties of the abnormality obtained from a plurality of detection results acquired by the acquirer.

    LIGHTNING THREAT INFORMATION-PROVIDING APPARATUS, LIGHTNING THREAT INFORMATION-PROVIDING METHOD, AND PROGRAM
    80.
    发明申请
    LIGHTNING THREAT INFORMATION-PROVIDING APPARATUS, LIGHTNING THREAT INFORMATION-PROVIDING METHOD, AND PROGRAM 有权

    公开(公告)号：US20210072423A1

    公开(公告)日：2021-03-11

    申请号：US16642323

    申请日：2018-08-09

    Applicant: JAPAN AEROSPACE EXPLORATION AGENCY

    Inventor： Eiichi YOSHIKAWA ,  Tomoo USHIO

    IPC: G01W1/16 ,  G01W1/10 ,  G08G5/00 ,  G06N20/00

    Abstract: [Object] To provide a lightning threat information-providing apparatus, a lightning threat information-providing method, and a program that are capable of providing a user with accurate information regarding a lightning threat.
    [Solving Means] A lightning threat information-providing apparatus 1 includes: an input unit 10 that inputs observation parameters 11 regarding weather observation data, prediction parameters 12 regarding weather prediction data, and case data 13 regarding a case that occurs in association with lightning occurrence; an intermediate parameter calculation unit that calculates, on the basis of the input observation parameters 11 and prediction parameters 12, an intermediate parameter 27 which is a parameter regarding physical quantity associated with the lightning occurrence and cannot be directly obtained from the observation data or the prediction data; and an arithmetic control unit 20 that estimates a lightning threat on the basis of the observation parameters 11, the prediction parameters 12, the case data 13, and the intermediate parameter 27.

Patent Agency Ranking