公开(公告)号：EP2985650A4

公开(公告)日：2016-11-30

申请号：EP14782429

申请日：2014-04-08

Applicant: KONICA MINOLTA INC

Inventor： ISHIKAWA RYOUTA ,  MATSUDA HIROYUKI ,  KAGEYAMA MASASHI ,  YONETAKE JUNICHIRO ,  FUJII HIDEYUKI ,  SHINDO HIROYUKI

IPC: G02B26/10 ,  G01S7/481 ,  G01S17/42 ,  G01S17/93 ,  G02B26/12

CPC classification number: G01S7/4817 ,  G01S17/42 ,  G01S17/936 ,  G02B26/129

Abstract: The present invention provides a scanning optical system and radar that can suppress longitudinal distortion and spot rotation of a spot light radiated on an object, the scanning optical system and radar also being able to suppress changes in resolution while maintaining a wide range of view. A light beam emitted from a light source, after being reflected by a first mirror surface of a mirror unit, progresses along a rotational axis, is reflected by a second mirror surface, and is projected on the object while being scanned across the object along a scanning angle direction around a scanning angle center in correspondence with rotation of the mirror unit. The light beam radiated from a projection system is longer in a width scanning angle direction than in the scanning angle direction in the measurement range of the object, and satisfies the following equation. |¸1 - 90| × |±| ‰¤ 225 (1); ¸1: angle (°) of intersection between first mirror surface and second mirror surface, ±: angle of rotation (°; 1/2 of the scanning angle)

公开(公告)号：EP3315937A4

公开(公告)日：2018-07-11

申请号：EP16832835

申请日：2016-07-26

Applicant: KONICA MINOLTA INC

Inventor： NAGASAWA HIKARU ,  IMADE KYUICHIRO ,  KAGEYAMA MASASHI ,  ISHIKAWA RYOUTA

IPC: G01M3/38 ,  B64C39/02 ,  B64D47/00 ,  G01B11/00 ,  G01N21/3504 ,  G01N21/39 ,  G01S17/42 ,  G01S17/89

CPC classification number: B64C39/02 ,  B64D47/00 ,  G01B11/00 ,  G01M3/38 ,  G01N21/3504 ,  G01N21/39 ,  G01N2021/399 ,  G01N2201/0214 ,  G01S17/42 ,  G01S17/89

Abstract: The unmanned flying body is provided with a gas detector, a distance meter, and an altitude controller. The gas detector emits diagonally downward to the forward side in a moving direction of the unmanned flying body a detecting light frequency-modulated by a predetermined modulation frequency setting a predetermined frequency as a central frequency. The gas detector receives the light, returned from a measurement target to which the detecting light is emitted (an area on a pipe member for transferring gas, irradiated with the detecting light), as first light. The measurement target is checked for gas leakage based on the received first light. The distance meter measures the distance between the gas detector and the measurement target. The altitude controller controls the flight altitude of the unmanned flying body based on the measured distance.

公开(公告)号：EP3296719A4

公开(公告)日：2018-05-02

申请号：EP16792579

申请日：2016-04-28

Applicant: KONICA MINOLTA INC

Inventor： IMADE KYUICHIRO ,  KAGEYAMA MASASHI ,  ISHIKAWA RYOUTA ,  NAGASAWA HIKARU

IPC: G01N21/27

CPC classification number: G01N21/27

Abstract: An object of the present invention is to provide a gas concentration measuring device that can accurately superimpose and display a gas concentration image and a background image so that a gas concentration distribution on the background image can be grasped at a glance. The gas concentration measuring device 1 of the present invention includes an imaging camera 20 that captures an image of a background 100, a light source 12 that emits constant light to the background, a light receiver 14 that receives light of the light source 12, a gyro sensor 30 for detecting an irradiation spot of the light of the light source 12, and a control device 40 that generates a background image based on an image capturing result of the imaging camera 20, creates a gas concentration distribution based on a light receiving result of the light receiver 14 and a detection result of the gyro sensor 30, and superimposes the gas concentration distribution on the background image.