JPH045702Y2 - - Google Patents

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Publication number
JPH045702Y2
JPH045702Y2 JP1983120017U JP12001783U JPH045702Y2 JP H045702 Y2 JPH045702 Y2 JP H045702Y2 JP 1983120017 U JP1983120017 U JP 1983120017U JP 12001783 U JP12001783 U JP 12001783U JP H045702 Y2 JPH045702 Y2 JP H045702Y2
Authority
JP
Japan
Prior art keywords
compressor
case
oxygen
air
gas 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.)
Expired
Application number
JP1983120017U
Other languages
Japanese (ja)
Other versions
JPS6028233U (en
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 filed Critical
Priority to JP12001783U priority Critical patent/JPS6028233U/en
Publication of JPS6028233U publication Critical patent/JPS6028233U/en
Application granted granted Critical
Publication of JPH045702Y2 publication Critical patent/JPH045702Y2/ja
Granted legal-status Critical Current

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Description

【考案の詳細な説明】 本考案は、酸素含有ガスを加圧供給するコンプ
レツサーをガスタービンに連動連結し、前記コン
プレツサーから前記ガスタービンへの給気路に燃
焼器を介装し、前記燃焼器に燃料を供給する流路
を設けた過給機に関する。
[Detailed Description of the Invention] The present invention provides a system in which a compressor that supplies oxygen-containing gas under pressure is connected to a gas turbine, a combustor is interposed in the air supply path from the compressor to the gas turbine, and the combustor The present invention relates to a supercharger provided with a flow path for supplying fuel.

従来、第2図に示すように、ガスタービン2に
対して強制冷却風供給用の電動フアン17を付設
し、そのフアン17からの冷却風でタービン車室
を冷却するようにしていた。しかし、冷却作用後
の冷却風によつて系外に持ち去られる熱量が極め
て多大であるために、装置全体としての熱効率が
大巾に低下する問題があり、又、電動フアン17
を設けるために構造が複雑になると共に、フアン
17の専用電源18が必要なことから電気工事の
ための諸経費が高くなり、全体としての製作コス
トが高価になる問題も合わせてあつた。
Conventionally, as shown in FIG. 2, an electric fan 17 for supplying forced cooling air was attached to the gas turbine 2, and the cooling air from the fan 17 was used to cool the turbine casing. However, since the amount of heat carried out of the system by the cooling air after the cooling effect is extremely large, there is a problem that the thermal efficiency of the entire device is drastically reduced.
The structure becomes complicated due to the provision of the fan 17, and since a dedicated power source 18 for the fan 17 is required, the overhead for electrical work increases, and the overall manufacturing cost increases.

本考案の目的は、所定のタービン車室冷却を、
電源が不要な状態で、かつ、装置全体としての熱
効率を高く維持しながら行えるようにし、しか
も、タービン、及び、コンプレツサーの騒音防止
と安全性の向上を同時に達成できるようにする点
にある。
The purpose of this invention is to achieve a specified turbine casing cooling.
The purpose is to enable operation without requiring a power source, while maintaining high thermal efficiency of the entire device, and to simultaneously achieve noise prevention and safety improvement of the turbine and compressor.

本考案の特徴構成は、冒記過給機において、前
記コンプレツサー及びガスタービンを内装するケ
ースを設け、前記燃焼器を前記ケースの外部に配
置し、前記ケースに吸音材を内張りし、前記コン
プレツサー及びガスタービンの冷却に伴つて予熱
された酸素含有ガスを燃焼用として吸入する前記
コンプレツサーの給気路を前記ケースに接続し、
前記コンプレツサーの吸引力で前記コンプレツサ
ー及びガスタービンの冷却のための酸素含有ガス
を前記ケース内に供給する酸素含有ガス供給路を
設けたことにあり、その作用・効果は次の通りで
ある。
The characteristic configuration of the present invention is that, in the above-mentioned supercharger, a case is provided in which the compressor and the gas turbine are housed, the combustor is arranged outside the case, the case is lined with a sound absorbing material, and the compressor and the gas turbine are Connecting an air supply path of the compressor that sucks oxygen-containing gas preheated as the turbine is cooled for combustion to the case;
An oxygen-containing gas supply path is provided for supplying oxygen-containing gas for cooling the compressor and gas turbine into the case using the suction force of the compressor, and its functions and effects are as follows.

つまり、コンプレツサーに供給するための酸素
含有ガスをケース内に流動させることにより、そ
のガスを強制冷却風に有効利用する状態でタービ
ン車室を冷却するのである。そして、発熱する燃
焼器をケースの外部に配置することにより、ケー
ス内を十分に低温に維持して、タービン車室の冷
却を十分に実現するのである。したがつて、単な
るケースの付加だけで、従来構成の如き強制冷却
風供給用の電動フアンを省くことができて、装置
全体としての構造を大巾に簡略化することがで
き、かつ、電源設備による設置上の制約や製作コ
ストの増大を回避することができた。
In other words, by flowing oxygen-containing gas to be supplied to the compressor into the case, the turbine casing is cooled while the gas is effectively used as forced cooling air. By arranging the combustor that generates heat outside the case, the inside of the case is maintained at a sufficiently low temperature and the turbine casing is sufficiently cooled. Therefore, by simply adding a case, it is possible to omit the electric fan for supplying forced cooling air as in conventional configurations, greatly simplifying the overall structure of the device, and reducing the power supply equipment. This made it possible to avoid installation restrictions and increases in manufacturing costs.

しかも、タービン車室冷却により、コンプレツ
サーに供給する酸素含有ガスが予熱されることと
なり、そのことによつて、装置の過給効率を高め
ることができるから、冷却によるタービン車室か
らの多大な放熱熱量が系内に有効に回収されるこ
ととなり、装置全体としての熱効率を大巾に向上
することができた。
In addition, by cooling the turbine casing, the oxygen-containing gas supplied to the compressor is preheated, which increases the supercharging efficiency of the device, so a large amount of heat is dissipated from the turbine casing due to cooling. The amount of heat was effectively recovered within the system, making it possible to significantly improve the thermal efficiency of the entire device.

その上、吸音材を内貼したケース本来の機能と
して、1分間当り数万回転以上もの高速で回転す
るコンプレツサー及び、ガスタービンから発生す
る騒音の外部波及を効果的に抑制することがで
き、かつ、コンプレツサーやガスタービンの運転
中における万が一の破損による事故防止をも図る
ことができ、全体として、実用性に極めて優れた
過給機を提供し得るに至つた。
In addition, the original function of the case, which is lined with sound-absorbing material, is to effectively suppress the external effects of noise generated from compressors and gas turbines, which rotate at high speeds of tens of thousands of revolutions per minute or more. Therefore, it is possible to prevent accidents caused by damage to the compressor or gas turbine during operation, and as a whole, it has been possible to provide a supercharger that is extremely practical.

次に、実施例を示す。 Next, examples will be shown.

第1図に示すように、空気を加圧供給するコン
プレツサー1をガスタービン2に連動連結し、コ
ンプレツサー1とガスタービン2を給気路3で接
続し、開閉弁V1付流路4からの燃料ガスとコン
プレツサー1からの空気を燃焼させるバーナ式燃
焼器5を給気路3に介装し、ガスタービン2から
の高圧熱風を適宜装置7に供給する回収流路6を
設け、もつて、高圧の熱風を例えば燃焼用酸素含
有ガス、加熱用ガス等として供給するための過給
機を構成してある。
As shown in Fig. 1, a compressor 1 that supplies air under pressure is connected to a gas turbine 2, the compressor 1 and the gas turbine 2 are connected through an air supply path 3, and a flow path 4 with an on-off valve V1 is connected. A burner type combustor 5 that burns fuel gas and air from the compressor 1 is interposed in the air supply path 3, and a recovery flow path 6 is provided to appropriately supply high-pressure hot air from the gas turbine 2 to the device 7. A supercharger is configured to supply high-pressure hot air as, for example, oxygen-containing gas for combustion, gas for heating, or the like.

コンプレツサー1、及び、ガスタービン2を内
装するケース8を設けると共に、そのケース8に
石綿材等の吸音材9を内貼りし、もつて、騒音防
止、並びに、運転中における安全性の向上を図つ
てある。
A case 8 is provided to house the compressor 1 and the gas turbine 2, and a sound absorbing material 9 such as asbestos material is lined inside the case 8 to prevent noise and improve safety during operation. It is attached.

コンプレツサー1に対する空気取入れ用の供給
路10を、ケース8のタービン2内装部分近くに
接続すると共に、コンプレツサー1に接続した吸
気路11の上流側端を、ケース8に接続し、もつ
て、コンプレツサー1に供給する空気をケース8
内に流動させることにより、その供給空気を強制
冷却風に有効利用する状態でタービン2のタービ
ン車室冷却を行なうように、又、そのタービン車
室冷却に伴ない供給空気を予熱することで、ター
ビン2から放熱熱量を系内に有効に回収し、装置
全体としての熱効率を向上するように構成してあ
る。
A supply passage 10 for air intake to the compressor 1 is connected to the case 8 near the interior of the turbine 2, and an upstream end of the intake passage 11 connected to the compressor 1 is connected to the case 8. Case 8
By making the supply air flow into the air, the turbine casing of the turbine 2 is cooled while effectively using the supplied air as forced cooling air, and by preheating the supplied air in conjunction with cooling the turbine casing, The system is configured to effectively recover the amount of heat radiated from the turbine 2 into the system, thereby improving the thermal efficiency of the entire system.

コンプレツサー1、及び、タービン2の軸受部
12に潤滑油を循環供給する給油路13を設ける
と共に、その循環給油路13に、ポンプ14、及
び、空冷式オイルクーラ15を介装してある。
An oil supply path 13 is provided to circulately supply lubricating oil to the bearings 12 of the compressor 1 and the turbine 2, and a pump 14 and an air-cooled oil cooler 15 are interposed in the circulation oil path 13.

そして、前記コンプレツサー1の吸気路11に
合流接続させた空気合流供給路16に、オイルク
ーラ15を、その冷却風流動路がコンプレツサー
1への合流供給空気の流動路となるように接続
し、もつて、コンプレツサー1への供給空気をオ
イルクーラ用冷却風に更に有効利用する状態で、
冷却風供給用電動フアンを設けること無く、循環
潤滑油を強制冷却できるように構成してある。
An oil cooler 15 is connected to the air merging supply path 16 connected to the air intake path 11 of the compressor 1 so that the cooling air flow path becomes a flow path for the merging supply air to the compressor 1. In this state, the air supplied to the compressor 1 is used more effectively as cooling air for the oil cooler.
The structure is such that the circulating lubricating oil can be forcibly cooled without providing an electric fan for supplying cooling air.

図中V2、V3は流量調節弁であり、それら弁の
調節により両空気供給路10,16からの空気の
合流比を設定する。
In the figure, V 2 and V 3 are flow control valves, and by adjusting these valves, the merging ratio of air from both air supply paths 10 and 16 is set.

次に、別の実施例を示す。 Next, another example will be shown.

前記コンプレツサー1に供給するガスは、酸素
含有量や組成を必要に応じて適宜変更でき、それ
らを酸素含有ガスと総称する。
The oxygen content and composition of the gas supplied to the compressor 1 can be changed as necessary, and these gases are collectively referred to as oxygen-containing gas.

又、その酸素含有ガスの供給路10、及び、コ
ンプレツサー1の吸気路11のケース8に対する
具体的接続箇所は、例えば、供給路10の接続口
をケース8のタービン内装部分近くに分散配置す
る等、適宜変更が可能である。
Further, the specific connection points of the oxygen-containing gas supply passage 10 and the intake passage 11 of the compressor 1 to the case 8 may be, for example, the connection ports of the supply passage 10 are distributed near the turbine interior portion of the case 8, etc. , can be changed as appropriate.

更に、ケース8の具体的形状、構造、並びに、
それに内貼する吸音材9の材質等は、種々の変更
改良が可能である。
Furthermore, the specific shape and structure of case 8, as well as
Various changes and improvements can be made to the material of the sound-absorbing material 9 that is attached to the inside.

尚、ガスタービン2、及び、コンプレツサー1
を起動するに、起動用の電動モータ等を用いるに
代えて、燃焼器5の燃料に中・高圧のガス燃料を
用いる場合には、そのガス燃料のガス圧を利用し
てエアーモータ等を回転させ、その回転駆動力で
タービン2、及び、コンプレツサー1を起動して
も良く、又、潤滑油供給ポンプ14を連続駆動す
るに、同じく電動モータ等を用いるに代えて、コ
ンプレツサー1からの高圧酸素含有ガスで、ポン
プ14に連動したエアーモータを駆動するように
構成しても良く、上述起動構造、並びに、ポンプ
駆動構造を、前述コンプレツサー1への供給酸素
含有ガスを利用した潤滑油冷却構造に併用するこ
とにより、電源設備を皆無にし得る。
Furthermore, the gas turbine 2 and the compressor 1
When using medium/high pressure gas fuel as the fuel for the combustor 5 instead of using an electric motor for starting, etc., the gas pressure of the gas fuel can be used to rotate the air motor, etc. The rotational driving force may be used to start the turbine 2 and the compressor 1. Also, to continuously drive the lubricating oil supply pump 14, instead of using an electric motor or the like, high pressure oxygen from the compressor 1 may be used. The contained gas may be configured to drive an air motor linked to the pump 14, and the above-mentioned starting structure and pump drive structure may be replaced with a lubricating oil cooling structure that utilizes the oxygen-containing gas supplied to the compressor 1. By using them together, you can completely eliminate the need for power supply equipment.

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

第1図は本考案の実施例を示すフローシートで
あり、第2図は従来例のフローシートである。 1……コンプレツサー、2……ガスタービン、
3……給気路、4……燃料供給用流路、5……燃
焼器、8……ケース、9……吸音材、10……酸
素含有ガス供給路、11……吸気路。
FIG. 1 is a flow sheet showing an embodiment of the present invention, and FIG. 2 is a flow sheet of a conventional example. 1...Compressor, 2...Gas turbine,
3...Air supply path, 4...Fuel supply flow path, 5...Combustor, 8...Case, 9...Sound absorbing material, 10...Oxygen-containing gas supply path, 11...Intake path.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 酸素含有ガスを加圧供給するコンプレツサー1
をガスタービン2に連動連結し、前記コンプレツ
サー1から前記ガスタービン2への給気路3に燃
焼器5を介装し、前記燃焼器5に燃料を供給する
流路4を設けた過給機であつて、前記コンプレツ
サー1及びガスタービン2を内装するケース8を
設け、前記燃焼器5を前記ケース8の外部に配置
し、前記ケース8に吸音材9を内張りし、前記コ
ンプレツサー1及びガスタービン2の冷却に伴つ
て予熱された酸素含有ガスを燃焼用として吸入す
る前記コンプレツサー1の吸気路11を前記ケー
ス8に接続し、前記コンプレツサー1の吸引力で
前記コンプレツサー1及びガスタービン2の冷却
のための酸素含有ガスを前記ケース8内に供給す
る酸素含有ガス供給路10を設けてある過給機。
Compressor 1 that supplies oxygen-containing gas under pressure
A supercharger which is interlocked and connected to a gas turbine 2, a combustor 5 is interposed in an air supply path 3 from the compressor 1 to the gas turbine 2, and a flow path 4 for supplying fuel to the combustor 5 is provided. A case 8 is provided in which the compressor 1 and the gas turbine 2 are housed, the combustor 5 is disposed outside the case 8, the case 8 is lined with a sound absorbing material 9, and the compressor 1 and the gas turbine are The air intake passage 11 of the compressor 1, which sucks in preheated oxygen-containing gas for combustion during cooling of the compressor 2, is connected to the case 8, and the suction force of the compressor 1 cools the compressor 1 and the gas turbine 2. The supercharger is provided with an oxygen-containing gas supply path 10 for supplying oxygen-containing gas into the case 8.
JP12001783U 1983-08-01 1983-08-01 supercharger Granted JPS6028233U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12001783U JPS6028233U (en) 1983-08-01 1983-08-01 supercharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12001783U JPS6028233U (en) 1983-08-01 1983-08-01 supercharger

Publications (2)

Publication Number Publication Date
JPS6028233U JPS6028233U (en) 1985-02-26
JPH045702Y2 true JPH045702Y2 (en) 1992-02-18

Family

ID=30275217

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12001783U Granted JPS6028233U (en) 1983-08-01 1983-08-01 supercharger

Country Status (1)

Country Link
JP (1) JPS6028233U (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH1193690A (en) * 1997-09-24 1999-04-06 Sts Kk Gas turbine driving power unit

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5928093Y2 (en) * 1979-07-19 1984-08-14 ヤンマーディーゼル株式会社 Gas turbine soundproof package
JPS5677618U (en) * 1979-11-20 1981-06-24

Also Published As

Publication number Publication date
JPS6028233U (en) 1985-02-26

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