子分类：
- G01P5/001： .{全流域流动测量,例如在整个区域内同时测定流动速度及方向,流动可视化}
- G01P5/003： .{通过测量流体在障碍物前的水平面}
- G01P5/005： .{通过应用注入流体的射流}
- G01P5/008： .{通过应用电解液加入流体的方法}
- G01P5/01： .利用涡流式流量计
- G01P5/02： .通过测量流体作用于固体上的力,例如风速表
- G01P5/08： .通过测量受流量直接影响的电变量的变化,例如应用机-电效应的
- G01P5/10： .通过测量热变量
- G01P5/14： .通过测量流体中的压差
- G01P5/18： .通过测量流体移动一定距离所需的时间
- G01P5/24： .通过测量对探测声波流动的直接影响
- G01P5/26： .通过测量液体流动对探测光波特性的直接影响
| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 161 | レーザレーダ装置 | JP2016527530 | 2014-06-10 | JPWO2015189915A1 | 2017-04-20 | 隼也 西岡; 英介 原口; 俊行 安藤 |
| 基準光源(2)により発振された送信種光の周波数νに対して、予め設定された周波数であるオフセット周波数(fofs)から移動体の移動速度に対応するドップラシフト周波数(fmove)を差し引いた周波数(fofs−fmove)を付与し、周波数(ν+fofs−fmove)の送信種光をパルス変調してパルス光を出力する変調ユニット(4)を設け、光ヘテロダイン受信機(8)が、光アンテナ(7)により受信された周波数(ν+fofs+fdop)の後方散乱光と周波数νの局部発振光とを光学的に合波して、その後方散乱光と局部発振光の差周波数(fofs+fdop)のビート信号を求める。 | ||||||
| 162 | 表層流推定装置、表層流推定システム、海洋モデル推定装置、及び危険度判定装置 | JP2016505097 | 2015-01-20 | JPWO2015129337A1 | 2017-03-30 | 尚志 今坂; 仁 前野; 千津 川崎 |
| 【課題】表層流の速度を容易に算出する。【解決手段】海上において船舶が位置する対象地点における船舶の対地速度ベクトルを算出する対地速度算出部11と、船舶の対水速度ベクトルに影響を与える少なくとも1つのパラメータの、対象地点における値の入力を受け付けるとともに、受け付けられた各値の組み合わせにより特定される各条件に対応する値を船舶の対水速度ベクトルと推定して出力する推定器12aと、推定器12aで推定された対水速度ベクトルとしての出力値と、対地速度算出部11で算出された対地速度ベクトルとに基づき、対象地点における表層流速度ベクトルを算出する表層流算出部13と、を備えた表層流推定装置1aを構成する。【選択図】図5 | ||||||
| 163 | 風力発電装置のモニタリングシステム及びモニタリング方法 | JP2013263610 | 2013-12-20 | JP5984791B2 | 2016-09-06 | 刈込 界; 松尾 竜 |
| 164 | 流体の移動の半径方向速度の遠隔測定から該流体の運動を決定する方法及び装置 | JP2013547890 | 2011-12-28 | JP5961188B2 | 2016-08-02 | ボケ マチュー; ニバール マクシム; アルベルジェル アルマン |
| 165 | Wind estimation for unmanned aerial vehicle | JP2011053953 | 2011-03-11 | JP2011246105A | 2011-12-08 | HAMKE ERIC E; ENNS DALE F; LOE GREGORY R; WACKER ROGER A; SCHUBERT OLIVER |
| PROBLEM TO BE SOLVED: To provide a device, a system, and a technology that estimate the speed of wind during the operation of an unmanned aerial vehicle (UAV) based on the modeled acceleration of the UAV during flight and the actual acceleration of the UAV during the flight.SOLUTION: The speed of the wind during operation of the UAV is estimated. In one example the speed of the wind is estimated by modeling the acceleration of the UAV based on a measured ground speed of the UAV, by determining the actual acceleration of the UAV with one or more sensors, and by estimating the speed of the wind as an integral of a difference between the modeled acceleration and the actual acceleration. | ||||||
| 166 | Measuring apparatus and method of the liquid and solute flux in the flow system | JP2001535010 | 2000-10-16 | JP2003513263A | 2003-04-08 | マイケル デヴィッド アナブル、; ティモシー ジェイ． キャンベル、; カーク ハットフィールド、; ピー． スレッシュ スィー． ラオ、 |
| (57)【要約】 流れ場内で液体流束及び溶解汚染物質流束を同時に監視するための改良された方法及び装置を提供する。 この方法及び装置は、溶解された汚染物質を保持する不溶性吸着材保持体を含む浸透性ユニットを使用する。 保持体には、液体流れによって置き換わることができるトレーサを含めることができる。 この監視方法は、浸透性ユニットを汚染された流れ場と接触させておき、汚染物質を浸透性ユニットを通して流し、不溶性吸着材保持体上に吸着させる。 十分な時間に亘って、流れ場内の汚染物質濃度を平衡に到達させる。 次いで、浸透性ユニットを流れ場との接触から除き、分析して、累積汚染物質流束及び累積液体流束を決定する。 | ||||||
| 167 | How to measure the vapor permeation amount with respect to the material | JP13227998 | 1998-05-14 | JP2957990B2 | 1999-10-06 | UIRIAMU ENU MEIYAA; SUTEFUAN DEII TSUOMERA; GASU ERU KUREIKU |
| 168 | Fast flow measurement method using a Nmr imaging equipment | JP22246691 | 1991-08-08 | JPH0616766B2 | 1994-03-09 | NOOBAATO JOSEFU PERUKU |
| An NMR system measures the velocity of flowing spins in the presence of stationary spins by performing three separate measurement cycles. The first cycle is a reference, the second cycle includes a magnetic field gradient having an incremental, flow sensitizing first moment DELTA M1, and a third measurement cycle includes a magnetic field gradient having an incremental flow sensitizing first moment - DELTA M1. The resulting NMR signals are processed to produce a velocity measurement. | ||||||
| 169 | Adjustable light multi-probe | JP2867391 | 1991-02-22 | JPH04215067A | 1992-08-05 | GURAIN JIIN MARII |
| PURPOSE: To observe a flow in any direction in two-phase emulsion (medium) and measure its flow speed without inserting a plurality of probes into the medium a number of times for changing their direction by using a single adjustable light multi-probe. CONSTITUTION: An orthogonal axis 18 is mounted to be perpendicular to a long axis XY of a hollow cylindrical tube 2, and a cylindrical, support 4 rotates around the orthogonal axis 18. A rod assembly 20 is coupled to the cylindrical support 4 along the hollow cylindrical tube 2, and the cylindrical support 4 is rotated around the orthogonal axis 18 by moving the rod assembly 20. COPYRIGHT: (C)1992,JPO | ||||||
| 170 | JPH0447267B2 - | JP14719087 | 1987-06-15 | JPH0447267B2 | 1992-08-03 | BURUKUHARUTO MYURAA |
| 171 | System for measuring underwater temperature distribution using optical fiber | JP21203590 | 1990-08-09 | JPH0493732A | 1992-03-26 | AOKI TARO; HATTORI RIKUO; YAMAGUCHI MASAYOSHI; ITO TETSUJI |
| PURPOSE: To obtain distributed temperature data and water-depth correcting data by attaching a towed body to the end of an optical fiber cable, converting measured signals from various sensors in the towed body into the measured optical signals, and receiving the optical signals together with backward scattered light for measuring temperature. CONSTITUTION: An optical fiber cable 4 is suspended in the water form a winch 3 on a ship. A towed body 5 is attached to the end of the cable. Light pulses (a) for measuring temperature are emitted from an optical-fiber distributed-temperature measuring device 23 into the cable 4 through a synthesizing and splitting device 22, an optical fiber wiring 20 and an optical slip ring 18. Backward scattered light (b) of the pulses (a) is received. The Raman scattered light contained in the backward scattered light (b) is subject to the effect of the temperature at the scattered part. Therefore, distributed temperature data A are obtained based on the time (t) from the entering of the optical pulse and the detected optical power. The measured signals of sensors 6, 7 and 8 in the towed body 5 are multiplexed 9. The signal is converted 10 into the light signal. The measured light signal (e) is cast into the cable 4. Then, the wavelength component of the signal (e) is filtered through a wavelength filter 24 in a measuring device 21. The signal undergoes photoelectric conversion 25. The signal is separated with a signal separating device 26. Thus, pressure data B, flow speed data C and temperature data D can be obtained. COPYRIGHT: (C)1992,JPO&Japio | ||||||
| 172 | Method and apparatus for determining speed of helicopter to air stream | JP14973990 | 1990-06-07 | JPH03103767A | 1991-04-30 | JIYANNPIEERU ARUSEN; PATORITSUKU GUUIEEBEROO |
| PURPOSE: To accurately determine the speed to an air stream of a helicopter of every kind by introducing the variables most correlated with the estimate speeds to all of flight configurations into calculation. CONSTITUTION: An MPU measures speeds V x, V y, pitches P o, P x, P y, P z, bank angles θ x, θ y and an acceleration value γ z at a time when a helicopter is flown according to (N) kinds of flight configrations several times. Next the speeds V x, V y are estimated at every flight configuration to be set to a first matrix and all of the variable containing V x, the variables constructed of the pitches, the bank angles and the acceleration value and a pair of one set of variables are used to calculate a correlation coefficient and a second matrix is also calculated in the same way. Next, a calculation formula having first and second sets of the constructed variables as functions is obtained. Subsequently, the pitches, the bank angles and the acceleration value in usual flight are measured and the speeds V x, V y are calculated to be compared with the measured values to display calculated values V x, V y. COPYRIGHT: (C)1991,JPO | ||||||
| 173 | JPH0260144B2 - | JP1232884 | 1984-01-25 | JPH0260144B2 | 1990-12-14 | NAKAMURA KUNIO; UMEKAGE YASUHIRO |
| 174 | JPH0253145B2 - | JP2687682 | 1982-02-23 | JPH0253145B2 | 1990-11-15 | TSUBOI HIROYUKI; SUGYAMA HIROSHI |
| 175 | Daikasutoniokerusaikoshashutsusokudokeisokusochi | JP2687482 | 1982-02-23 | JPH0229425B2 | 1990-06-29 | TSUBOI HIROYUKI; SUGYAMA HIROSHI |
| 176 | Senpakunoyokosuberisokudokaisekiki | JP14817982 | 1982-08-26 | JPH0229163B2 | 1990-06-28 | KOSUGE YOSHIO |
| 177 | JPH0216971B2 - | JP14878582 | 1982-08-27 | JPH0216971B2 | 1990-04-19 | KOSUGE YOSHIO |
| 178 | JPH022540B2 - | JP14418982 | 1982-08-20 | JPH022540B2 | 1990-01-18 | YAMADA HIROYOSHI; SHIMADA MASANOBU; KONDO TOMOMASA; HISANAGA AKIRA; SASANUMA MASAO |
| 179 | JPH0134318Y2 - | JP10381186 | 1986-07-08 | JPH0134318Y2 | 1989-10-18 | |
| 180 | JPH0119544B2 - | JP15458382 | 1982-09-07 | JPH0119544B2 | 1989-04-12 | NAKADA TSUNEO; KUNIHIRO MASAFUMI; YAMAMOTO KITAO; OOE HIRONORI; TAKAHASHI YASUO |
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