JPS613496U - Turbine missile protection device - Google Patents

Turbine missile protection device

Info

Publication number
JPS613496U
JPS613496U JP1984087566U JP8756684U JPS613496U JP S613496 U JPS613496 U JP S613496U JP 1984087566 U JP1984087566 U JP 1984087566U JP 8756684 U JP8756684 U JP 8756684U JP S613496 U JPS613496 U JP S613496U
Authority
JP
Japan
Prior art keywords
protection device
turbine
missile
low
pressure turbine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP1984087566U
Other languages
Japanese (ja)
Other versions
JPH0348558Y2 (en
Inventor
繁利 小野
寿雄 山下
Original Assignee
株式会社東芝
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 株式会社東芝 filed Critical 株式会社東芝
Priority to JP1984087566U priority Critical patent/JPS613496U/en
Publication of JPS613496U publication Critical patent/JPS613496U/en
Application granted granted Critical
Publication of JPH0348558Y2 publication Critical patent/JPH0348558Y2/ja
Granted legal-status Critical Current

Links

Classifications

    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00—Energy generation of nuclear origin
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00—Energy generation of nuclear origin
    • Y02E30/30—Nuclear fission reactors

Landscapes

  • Structure Of Emergency Protection For Nuclear Reactors (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【図面の簡単な説明】[Brief explanation of drawings]

第１図は、既に提案されているタービンミサイルの防護
装置の平面図、第２図は、第１図中の鎖線Ａ−Ａに沿う
側面図、第３図は、本考案によるタービンミサイルの保
護装置の平面図、第４図は、第３図中の鎖線Ｂ−Ｈに沿
う断面図、第５図は、第３図中の鎖線Ｃ−Ｃに沿う断面
図、第６図は、本考案に使用されるミサイル防護体の取
付部を示す断面図であるら ２・・・低圧タービン、５・・・遮蔽体、７・・・ミサ
イル防護体、９・・・蒸気放出口、１０・・・蓋体、１
１・・・階段。Fig. 1 is a plan view of a turbine missile protection device that has already been proposed, Fig. 2 is a side view taken along the chain line A-A in Fig. 1, and Fig. 3 is a turbine missile protection device according to the present invention. 4 is a sectional view taken along the dashed line B-H in FIG. 3, FIG. 5 is a sectional view taken along the dashed line C-C in FIG. 3, and FIG. 6 is a sectional view taken along the dashed line C-C in FIG. 2. Low pressure turbine, 5. Shielding body, 7. Missile protection body, 9. Steam outlet, 10.・Lid body, 1
1...Stairs.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 低圧タービンの両側に遮蔽体を設け、上記低圧タービン
に軸方向に二分割し得る断面が半円筒状をなすミサイル
防護体を上記低圧タービン奔覆うようにして設け、この
ミサイル防護体の一部に複数の蒸気放出口を設け、この
各蒸気放出口に各蓋体を付設したことを特徴とするター
ビンミサイルの防護装置。A shield is provided on both sides of the low-pressure turbine, a missile protector having a semi-cylindrical cross section that can be divided into two in the axial direction is provided over the low-pressure turbine, and a part of the missile protector is provided with a shield on both sides of the low-pressure turbine. A protection device for a turbine missile, characterized in that a plurality of steam discharge ports are provided, and a lid body is attached to each steam discharge port.
JP1984087566U 1984-06-13 1984-06-13 Turbine missile protection device Granted JPS613496U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1984087566U JPS613496U (en) 1984-06-13 1984-06-13 Turbine missile protection device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1984087566U JPS613496U (en) 1984-06-13 1984-06-13 Turbine missile protection device

Publications (2)

Publication Number Publication Date
JPS613496U true JPS613496U (en) 1986-01-10
JPH0348558Y2 JPH0348558Y2 (en) 1991-10-16

Family

ID=30639903

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1984087566U Granted JPS613496U (en) 1984-06-13 1984-06-13 Turbine missile protection device

Country Status (1)

Country Link
JP (1) JPS613496U (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8316129B2 (en) 2005-05-25 2012-11-20 Microsoft Corporation Data communication coordination with sequence numbers
US9331955B2 (en) 2011-06-29 2016-05-03 Microsoft Technology Licensing, Llc Transporting operations of arbitrary size over remote direct memory access
US8856582B2 (en) 2011-06-30 2014-10-07 Microsoft Corporation Transparent failover

Also Published As

Publication number Publication date
JPH0348558Y2 (en) 1991-10-16

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