ガスタービン用流体温度検出器

Material type: 文書・図像類

Author: 西尾, 健二ほか

Publisher: 航空宇宙技術研究所

Publication date: 1972-01

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: There have been investigated and published many applications of fluidic amplifier device to large variety of engineering fields because of its trouble...

Search by Bookstore

Holdings of Libraries in Japan

This page shows libraries in Japan other than the National Diet Library that hold the material.

List of Cooperating Institutions and Databases

Please contact your local library for information on how to use materials or whether it is possible to request materials from the holding libraries.

other

JAXA Repository
Digital
You can check the holdings of institutions and databases with which 学術機関リポジトリデータベース（IRDB）（機関リポジトリ） is linked at the site of 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）.
JAXA Repository

Search by Bookstore

Bibliographic Record

You can check the details of this material, its authority (keywords that refer to materials on the same subject, author's name, etc.), etc.

Digital

Material Type: 文書・図像類
Title: ガスタービン用流体温度検出器
Author/Editor: 西尾, 健二
遠藤, 征紀
遠藤, 篤和
NISHIO, Kenji
ENDO, Masanori
ENDO, Atsukazu
Author Heading: 西尾, 健二
遠藤, 征紀
遠藤, 篤和
NISHIO, Kenji
ENDO, Masanori
ENDO, Atsukazu
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1972-01
Publication Date (W3CDTF): 1972-01
Alternative Title: Fluidic Turbine Inlet Gas Temperature Sensor
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-265
No. or year of volume/issue: 265
Volume: 265
Pages: 28-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): There have been investigated and published many applications of fluidic amplifier device to large variety of engineering fields because of its trouble-proof, heat-and vibration-resisting characteristics derived from the fact that it has no moving parts. Fluidic turbine inlet gas temperature sensor should be cited as one of the most important and right applications. Although some papers on it are already published, they are all confined to show the final test results or performances of the sensor. Prototype fluidic turbine inlet gas temperature sensors we have designed and manufactured for experimental use on the consideration of basic mechanism of oscillation have two outstanding features in its geometry; first, they have the output port whose corss area is smaller than that of main nozzle. second, they have the feedback path whose cross area suddenly increases and remains constant up to control port. These features made it possible, at least principally, to get the fluidic turbine inlet gas temperature sensor with high resolution and low noise,large amplitude output signal. In this report, we described the basic design consideration and philosophy of fluidic turbine inlet gas temperature sensor as well as some test results and performances of them. In appendix, we analyzed and calculated the phase shift of pressure wave caused by sudden increase of wave guide cross area.
資料番号: NALTR0265000
レポート番号: NAL TR-265
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44508&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44508&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ