| Item type |
テクニカルレポート / Technical Report(1) |
| 公開日 |
2015-03-26 |
| タイトル |
|
|
タイトル |
液体水素用高速・接触式メカニカルシールの密封特性に関する研究 |
| 言語 |
|
|
言語 |
jpn |
| 資源タイプ |
|
|
資源タイプ識別子 |
http://purl.org/coar/resource_type/c_18gh |
|
資源タイプ |
technical report |
| その他のタイトル（英） |
|
|
その他のタイトル |
Stusy on Sealing Characteristics of HighSpeed, Face-Contact Bellows Mechanical Seals for Liquid Hydrogen |
| 著者 |
野坂, 正隆
上條, 謙二郎
鈴木, 峰男
菊池, 正孝
宮川, 行雄
NOSAKA, Masataka
KAMIJO, Kenjiro
SUZUKI, Mineo
KIKUCHI, Masataka
MIYAKAWA, Yukio
|
| 著者所属 |
|
|
|
航空宇宙技術研究所角田支所 |
| 著者所属 |
|
|
|
航空宇宙技術研究所角田支所 |
| 著者所属 |
|
|
|
航空宇宙技術研究所宇宙研究グループ |
| 著者所属 |
|
|
|
航空宇宙技術研究所角田支所 |
| 著者所属 |
|
|
|
元・航空宇宙技術研究所角田支所 |
| 著者所属（英） |
|
|
|
en |
|
|
Kakuda Branch Office, National Aerospace Laboratory(NAL) |
| 著者所属（英） |
|
|
|
en |
|
|
Kakuda Branch Office, National Aerospace Laboratory(NAL) |
| 著者所属（英） |
|
|
|
en |
|
|
Space Technology Research Group, National Aerospace Laboratory(NAL) |
| 著者所属（英） |
|
|
|
en |
|
|
Kakuda Branch Office, National Aerospace Laboratory(NAL) |
| 著者所属（英） |
|
|
|
en |
|
|
Former Kakuda Branch Office, National Aerospace Laboratory(NAL) |
| 出版者 |
|
|
出版者 |
航空宇宙技術研究所 |
| 出版者（英） |
|
|
出版者 |
National Aerospace Laboratory(NAL) |
| 書誌情報 |
航空宇宙技術研究所報告
en : Technical Report of National Aerospace Laboratory TR-750
巻 750,
p. 64,
発行日 1983-01
|
| 抄録（英） |
|
|
内容記述タイプ |
Other |
|
内容記述 |
This investigation was carried out in order to develop a high speed, face-contact bellows mechanical seal for a liquid hydrogen turbopump of a liquid oxygen(LOX) and liquid hydrogen(LH2) rocket engine. The present report describes the results of experimental and analytical studies on the static and dynamic sealing performance and the wear process of a newly developed mechanical seal for an LH2 turbopump. The main results obtained in this study are as follows: (1)The starting torque and static sealing performance were markedly affected by the change of the stationary seal face distortion, which was caused by fluid pressure and temperature, due to wear. The seal friction loss power fell by a small value after the mechanical seal faces had completely run-in. (2)The sealing balance ratio of the mechanical seal, which stabilized the dynamic sealing at high rotative speed, was above 0.77. This high value was due to the large amount of the opening force. (3)The high opening force ratio noted in the experiment was well explained by the leakage flow model, in which a liquid phase was assumed to be changed, due to viscous friction, to a gas phase in parallel seal clearance. The opening force ratio increased with the increase of rotative speed and decreased with the increase of the seal clearance. (4)The temperature at the rubbing surface of the chrominum plate was about 500C at the initial operating stage, according to the measurement of the chromium plate hardness. Recrystalization also occured in a part of the chromium plate. (5)Thermal cracks, which were formed on the chromium plate sealing surface of the rotating ring, were characteristic of crack edge lifting. The carbon seal face worn by the cracks made the proper seal clearance, which increased the opening force and drastically decreased the load on the rubbing seal surface. This process occured at the initial operating stage even for a long operation. (6)The thermal distortion of the carbon seal surface due to friction heat ocurred when the seal nose-piece temperature was above 60K. This dynamical thermal distortion was prevented by the selection of a sealing balance ratio below 0.82, which allowed the seal surfaces to wear evently. (7)The wear of the seal surfaces was efficiently decreased, even under severe operating conditions, when the proper seal clearance(0.5～0.8μm) was set before the operation. |
| ISSN |
|
|
収録物識別子タイプ |
ISSN |
|
収録物識別子 |
0389-4010 |
| 資料番号 |
|
|
内容記述タイプ |
Other |
|
内容記述 |
資料番号: NALTR0750000 |
| レポート番号 |
|
|
内容記述タイプ |
Other |
|
内容記述 |
レポート番号: NAL TR-750 |
naltr00750.pdf (12.5 MB)
