JPH0441932A - Hot air supply device for turbo supercharging engine with fuel combustion device - Google Patents

Hot air supply device for turbo supercharging engine with fuel combustion device

Info

Publication number
JPH0441932A
JPH0441932A JP2144345A JP14434590A JPH0441932A JP H0441932 A JPH0441932 A JP H0441932A JP 2144345 A JP2144345 A JP 2144345A JP 14434590 A JP14434590 A JP 14434590A JP H0441932 A JPH0441932 A JP H0441932A
Authority
JP
Japan
Prior art keywords
air
supercharger
engine
exhaust
air supply
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.)
Pending
Application number
JP2144345A
Other languages
Japanese (ja)
Inventor
Yasunori Akiyama
秋山 恭徳
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
AKASAKA TEKKOSHO KK
Original Assignee
AKASAKA TEKKOSHO KK
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 AKASAKA TEKKOSHO KK filed Critical AKASAKA TEKKOSHO KK
Priority to JP2144345A priority Critical patent/JPH0441932A/en
Publication of JPH0441932A publication Critical patent/JPH0441932A/en
Pending legal-status Critical Current

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  • Supercharger (AREA)
  • Drying Of Solid Materials (AREA)

Abstract

PURPOSE:To increase hot air energy by providing a fuel combustion device in the middle of an air supply bypass passage branching from an air supply passage which connects an engine body to an air compressor of a supercharger, by mixing the combustion gas with an exhaust gas from the engine body, and by introducing it to an exhaust turbine. CONSTITUTION:In this hot air supply device 2 in a turbo supercharging engine 1, an air flow regulating valve 20 is provided in an air supply bypass passage 19 branching from an air supply passage 27 which connects an engine body 10 to an air compressor 16 of a supercharger 13, and a fuel combustion device 22 is provided at the lower stream of this air flow regulating valve 20. And a mixed gas of combustion gas from this fuel combustion device 22 and an exhaust gas from the engine body 10 is introduced to an exhaust turbine 14 of the supercharger 13 by a manifold 23. Also, a supplied air discharge passage 29 branches from the air supply passage 27 connected to the air compressor 16 of the supercharger 13, and at the lower stream of this supplied air discharging passage 29, a heat exchanger 30 is provided for heating supplied air by an exhaust gas from a connecting pipe 33 connected to an exhaust outlet of the exhaust turbine 14 of the supercharger.

Description

【発明の詳細な説明】 [産業上の利用分野1 この発明は燃料燃焼装置く以下燃焼装置と言う)を備え
た排気ターボ過給機付内燃機関(以下ターボ過給機関と
言う)の熱風供給装置に関するものである。
[Detailed Description of the Invention] [Industrial Application Field 1] This invention provides hot air supply for an internal combustion engine with an exhaust turbocharger (hereinafter referred to as a turbocharged engine) equipped with a fuel combustion device (hereinafter referred to as a combustion device). It is related to the device.

[従来の技術] 従来、ターボ過給機関の排気ガスにより駆動する過給機
の排気タービンのタービン面積を小さくして排気タービ
ンが回収する排気ガスエネルギの熱落差を大きく採るこ
とによって過給機の空気圧縮機が吸入吐出する給気の一
部をターボ過給機関の外部へ供給して、残りの給気で機
関本体の性能、出力を満足する方式が採られている。タ
ーボ過給機関の外部へ供給された給気の一部は過給機出
口に設けられた熱交換器によって排気ガスから廃熱を回
収して熱風エネルギとして船舶の船舶に送られて船舶の
湿度調整乾燥の用途に供せられる等の例が見られる。
[Prior Art] Conventionally, the turbine area of the exhaust turbine of a supercharger driven by the exhaust gas of a turbocharged engine is reduced to increase the heat drop of the exhaust gas energy recovered by the exhaust turbine, thereby increasing the efficiency of the supercharger. A method is adopted in which a portion of the air taken in and discharged by the air compressor is supplied to the outside of the turbocharged engine, and the remaining air is used to satisfy the performance and output of the engine itself. Part of the air supplied to the outside of the turbocharged engine recovers waste heat from the exhaust gas through a heat exchanger installed at the turbocharger outlet and sends it to the vessel as hot air energy to reduce the humidity of the vessel. There are examples where it is used for controlled drying.

[発明が解決しようとする問題点] 併し乍ら、この様な船舶における船舶の湿度調整乾燥の
場合に、ターボ過給機関から外部に供給する給気の一部
が機関本体からの排気エネルギを過給機で回収変換した
空気の圧力エネルギであるので、その量がターボ過給機
関の出力の大きさによって変化する結果、船舶の湿度調
整乾燥の需要負荷に熱量的にも時間的にも応じられない
場合がある。すなわち、船舶の目的港における待機碇泊
または輸送途中の気象、海象条件悪化による目的港以外
の港への避難碇泊、更には時間調整のための減速航行等
でターボ過給機関が停止または低負荷運転によって排気
ガスエネルギが得られない或は減少して負荷需要に応じ
られない場合等の不都合が見られる。
[Problems to be Solved by the Invention] However, in the case of humidity adjustment and drying in such a ship, a part of the supply air supplied to the outside from the turbocharged engine supercharges the exhaust energy from the engine body. Since it is the pressure energy of the air recovered and converted by the machine, the amount changes depending on the output of the turbocharged engine, and as a result, it cannot meet the demand load of humidity adjustment and drying on ships, both in terms of heat and time. There are cases. In other words, the turbocharged engine may stop or operate at low load due to the ship's berthing at a waiting port at its destination port, evacuation berthing at a port other than the destination port due to poor weather or sea conditions during transit, or slowing down sailing to adjust time, etc. Therefore, there are disadvantages such as cases where exhaust gas energy cannot be obtained or is reduced and cannot meet the load demand.

従って、この発明の目的はこの様な従来における問題点
を解決するために、ターボ過給機関の過給機の排気ター
ビンのタービン面積を小さくして排気タービンが回収す
る排気ガスエネルギの熱落差を大きくすることによって
常用負荷においては過給機の空気圧縮機から吐出する給
気の一部をターボ過給機関の外部に供給可能にすると共
に、過給機の空気圧縮機と連通ずる給気通路から分岐す
る給気バイパス通路中に空気流量調節弁および燃料燃焼
装置を設けて、ターボ過給機関の低負荷運転中は燃料燃
焼装置の追焚き燃焼による燃焼ガスを機関本体からの排
気ガスと混合して過給機の排気タービンに導入して排気
タービンの出力を増加させて過給機の空気圧縮機からの
給気量と給気圧力を増加させると共に、過給機の排気タ
ービン出口の排気ガス量と排気温度を上昇させてターボ
過給機関の外部に供給する給気量と過給機出口に設けた
熱交換器によって給気が回収する排気ガスからの廃熱回
収量を増加させて船舶に供給する熱風エネルギを増加し
て湿度調整乾燥能力を満足することが出来る。また、常
用負荷運転においても船舶の湿度調整乾燥に必要な熱風
エネルギと給気量がターボ過給機関の出力が相対的に小
さいために不足する場合には燃料燃焼装置の追焚き燃焼
による燃焼ガスエネルギを過給機の排気タービンに供給
することで補うことが出来るようにした燃料燃焼装置を
備えたターボ過給機関の熱風供給装置を提供することに
ある。
Therefore, an object of the present invention is to reduce the turbine area of the exhaust turbine of the supercharger of a turbocharged engine to reduce the thermal drop of the exhaust gas energy recovered by the exhaust turbine, in order to solve these conventional problems. By increasing the size, it is possible to supply part of the air discharged from the air compressor of the turbocharger to the outside of the turbocharged engine during normal load, and the air supply passage that communicates with the air compressor of the turbocharger. An air flow control valve and a fuel combustion device are installed in the air supply bypass passage that branches from the engine, and during low-load operation of the turbocharged engine, the combustion gas from the reheating combustion of the fuel combustion device is mixed with the exhaust gas from the engine body. The air is introduced into the exhaust turbine of the turbocharger to increase the output of the exhaust turbine, thereby increasing the amount and pressure of air supplied from the air compressor of the turbocharger. By increasing the gas volume and exhaust temperature, the amount of supply air supplied to the outside of the turbocharged engine and the amount of waste heat recovered from the exhaust gas recovered by the heat exchanger installed at the outlet of the turbocharger are increased. By increasing the hot air energy supplied to the ship, the humidity control and drying ability can be satisfied. In addition, even during normal load operation, if the hot air energy and air supply required for humidity adjustment and drying of the ship are insufficient due to the relatively low output of the turbocharged engine, the combustion gas is generated by reheating the fuel combustion device. An object of the present invention is to provide a hot air supply device for a turbocharged engine equipped with a fuel combustion device capable of supplementing energy by supplying energy to an exhaust turbine of a supercharger.

[問題点を解決するための手段] この発明に依れば、燃料燃焼装置を備えたターボ過給機
関の熱風供給装置は、内燃機関の機関本体と過給機の空
気圧縮機とを連通ずる給気通路から分岐する給気バイパ
ス通路を有するターボ過給機関において、給気バイパス
通路中に設けられた空気流量調節弁、該空気流量調節弁
の後に設けられた燃料燃焼装置、該燃料燃焼装置の燃焼
ガスと該機関本体からの排気ガスとを混合して該過給機
の排気タービンに導入する連結管を備えると共に、該過
給機の空気圧縮機と連通ずる給気通路から分岐する給気
放出通路、該給気放出通路の後に段けられて該過給機の
排気タービン出口の排気ガスによって給気を加熱する熱
交換器を備えたことを特徴としている。
[Means for Solving the Problems] According to the present invention, a hot air supply device for a turbocharged engine equipped with a fuel combustion device communicates between the engine body of the internal combustion engine and the air compressor of the supercharger. In a turbocharged engine having an air intake bypass passage branching from an air intake passage, an air flow rate control valve provided in the air intake bypass passage, a fuel combustion device provided after the air flow rate adjustment valve, and the fuel combustion device a connecting pipe that mixes combustion gas from the engine and exhaust gas from the engine main body and introduces the mixture into the exhaust turbine of the supercharger, and an air supply branching from an air supply passage that communicates with the air compressor of the supercharger. The present invention is characterized in that it includes a heat exchanger that is arranged after the air discharge passage and the supply air discharge passage and heats the supply air with the exhaust gas from the exhaust turbine outlet of the supercharger.

し作  用] 上述のこの発明の手段に依って、ターボ過給機関の低負
荷運転および常用負荷運転においてターボ過給機関の外
部に給気の一部を取り出して過給機出口に設けられた熱
交換器によって排気ガス廃熱を給気の熱風エネルギとし
て回収利用する場合に、熱エネルギと給気量を増加させ
るために機関本体と過給機の空気圧縮機を連通ずる給気
通路から分岐する給気バイパス通路に設けられた空気流
量調節弁を経たバイパス給気が燃料燃焼装置において導
入された燃料と混合する燃焼用空気に一部が利用されて
、他の部分が燃料燃焼装置を冷却すると共に燃焼ガスを
希釈して下流で機関本体からの排気ガスと混合した後に
過給機の排気タービンを駆動して燃料燃焼装置から供給
した燃料の燃焼ガスの仕事量相当分を過給機の空気圧縮
機が給気圧力と給気量を増加させて過給機の排気タービ
ン出口の排気ガス量と排気温度をも増加上昇するので、
ターボ過給機関の外部に取り出す給気の一部も給気量が
増加されて過給機の排気タービン出口に設けられた熱交
換器で回収する排気ガス廃熱の回収量も増加されて熱風
エネルギを増加することが出来る。
[Function] According to the above-described means of the present invention, a part of the charge air is taken out to the outside of the turbocharged engine during low load operation and regular load operation of the turbocharged engine, and a part of the charge air is provided at the turbocharger outlet. When exhaust gas waste heat is recovered and used as hot air energy for supply air using a heat exchanger, it is branched from the supply air passage that communicates between the engine body and the air compressor of the supercharger in order to increase the heat energy and the amount of supply air. A portion of the bypass supply air that passes through an air flow control valve installed in the supply air bypass passage is used for combustion air to be mixed with the fuel introduced in the fuel combustion device, and the other portion is used to cool the fuel combustion device. At the same time, the combustion gas is diluted and mixed with the exhaust gas from the engine main body downstream, and then the exhaust turbine of the supercharger is driven to absorb the work of the combustion gas of the fuel supplied from the fuel combustion device into the turbocharger. The air compressor increases the air supply pressure and air intake, which also increases the exhaust gas amount and exhaust temperature at the exhaust turbine outlet of the supercharger.
The amount of air supplied to the outside of the turbocharged engine is also increased, and the amount of exhaust gas waste heat recovered by the heat exchanger installed at the exhaust turbine outlet of the turbocharger is also increased. Energy can be increased.

この発明の他の目的と特長および利点は以下の添付図面
に沿っての詳細な説明から明らかになろう。
Other objects, features and advantages of the invention will become apparent from the following detailed description taken in conjunction with the accompanying drawings.

[実 錐 例] 図面に示される様に、この発明の燃料燃焼装置を備えた
ターボ過給機関1の熱風供給装置2は、内燃機関の機関
本体1oと過給機13の空気圧縮機16とを連通ずる給
気通路27力弓分岐する給気バイパス通#819を有す
るターボ過給機関1において、給気バイパス通路19中
に設けられた空気流量調節弁2o、この空気流1調節弁
2oの後すなわち下流に設けられた燃料燃焼装置22、
この燃料燃焼装置22の燃焼ガスと内燃機関の機関本体
10からの排気ガスとを混合して過給機13の排気ター
ビン14に導入する連結管23、過給機13の空気圧縮
l116と連通する給気通路27から分岐する給気放出
通路29、この給気放出通路29の下流に設けられて過
給機13の排気タービン14の排気出口に接続された接
続管33からの排気ガスによって給気を加熱する熱交$
11830から主に構成されている。
[Actual Example] As shown in the drawings, the hot air supply device 2 of the turbocharged engine 1 equipped with the fuel combustion device of the present invention has an engine main body 1o of the internal combustion engine, an air compressor 16 of the supercharger 13, In a turbocharged engine 1 having an air supply bypass passage #819 which is connected to an air supply passage 27 and branched, an air flow control valve 2o provided in the air supply bypass passage 19, and an air flow control valve 2o provided in the air supply bypass passage 19 a fuel combustion device 22 provided after or downstream;
A connecting pipe 23 that mixes the combustion gas of this fuel combustion device 22 and exhaust gas from the engine body 10 of the internal combustion engine and introduces the mixture into the exhaust turbine 14 of the supercharger 13 communicates with the air compressor 116 of the supercharger 13. A supply air discharge passage 29 branches from the supply air passage 27, and the supply air is supplied by exhaust gas from a connecting pipe 33 provided downstream of the supply air discharge passage 29 and connected to the exhaust outlet of the exhaust turbine 14 of the supercharger 13. heat exchanger to heat
It is mainly composed of 11830.

図示される様に、この発明の熱風供給装置2が設けられ
るターボ過給機関1は内燃機関の機関本体10と、機関
本体】0に夫々接続された排気管11a、llb、11
 cから成る第1の排気管11と排気管12a、12b
、12cから成る第2の排気管12と、これら第1、第
2の排気管11.12に夫々流入した排気ガスが導入さ
れる排気タービン14および排気タービン14と軸15
を介して接続された空気圧縮機16を有する過給機13
と、過給機13の空気圧縮機16により吸入した給気を
内燃機関の機関本体10に供給するよう給気出口17に
空気冷却器26を介して接続された給気通路27とから
構成されている。
As shown in the figure, a turbocharged engine 1 equipped with a hot air supply device 2 of the present invention has an engine body 10 of an internal combustion engine, and exhaust pipes 11a, llb, 11 connected to the engine body 0, respectively.
The first exhaust pipe 11 and exhaust pipes 12a and 12b consisting of c.
, 12c, an exhaust turbine 14 into which the exhaust gases flowing into the first and second exhaust pipes 11, 12, respectively, are introduced, and the exhaust turbine 14 and the shaft 15.
A supercharger 13 with an air compressor 16 connected via
and an air supply passage 27 connected to the air supply outlet 17 via an air cooler 26 so as to supply air sucked in by the air compressor 16 of the supercharger 13 to the engine body 10 of the internal combustion engine. ing.

この様に構成されたターボ過給機関1の過給機13の空
気圧縮機16の給気出口17に連接された給気通路27
から分岐管18を介して給気バイパス通路19が分岐さ
れ、この給気バイパス通路1つに空気流量調節弁20が
設けられると共に、この空気流量調節弁20の後ずなわ
ち下流に、燃料供給管32を有する燃料燃焼装置22が
設けられている。これら第1、第2の排気管11.12
と燃料燃焼装置22は、接続管24と付加容積管25か
ら成る連結管23によって過給機13の排気タービン1
4に接続され、第1、第2の排気管11.12からの排
気ガスと燃料燃焼装置22からの燃焼ガスが過給機13
の排気タービン14に導入される。第1、第2の排気管
11.12に交互に流入した排気ガスは、過給機13の
排気タービン14の入口で第1、第2の排気管11.1
2と燃料燃焼装置22からの燃焼ガスを排気タービン1
4に導入する連結管23の接続管24とを連結する付加
容積管25.25の容積効果およびバイパス効果によっ
て圧力波が減衰されて、タービン面積の小さい排気ター
ビン14が回収する熱落差を大きく採ることが出来る。
Air supply passage 27 connected to air supply outlet 17 of air compressor 16 of supercharger 13 of turbocharged engine 1 configured in this manner
An air supply bypass passage 19 is branched from the air supply bypass passage 19 via a branch pipe 18, and an air flow rate control valve 20 is provided in one of the air supply bypass passages. A fuel combustion device 22 having a tube 32 is provided. These first and second exhaust pipes 11.12
The fuel combustion device 22 is connected to the exhaust turbine 1 of the supercharger 13 through a connecting pipe 23 consisting of a connecting pipe 24 and an additional volume pipe 25.
The exhaust gas from the first and second exhaust pipes 11 and 12 and the combustion gas from the fuel combustion device 22 are connected to the supercharger 13.
The exhaust gas is introduced into the exhaust turbine 14 of the engine. The exhaust gas that has alternately flowed into the first and second exhaust pipes 11.12 passes through the first and second exhaust pipes 11.1 at the inlet of the exhaust turbine 14 of the supercharger 13.
2 and the combustion gas from the fuel combustion device 22 to the exhaust turbine 1
The pressure wave is attenuated by the volume effect and bypass effect of the additional volume pipe 25.25 that connects the connecting pipe 24 to the connecting pipe 23 introduced into the exhaust gas turbine 4, and the heat drop recovered by the exhaust turbine 14 having a small turbine area is increased. I can do it.

この排気タービン14で回収した回転エネルギは軸15
によって過給機13の空気圧縮機16に伝達されて空気
圧縮機16によって大気から吸入した給気を圧縮して給
気出口17から空気冷却器26を介して給気通路27か
ら内燃機r!Jj1oの機関本体10に送り込むと共に
、分岐管18から給気の一部が分岐されてバイパス給気
として給気バイパス通路19に送り込まれる。また、同
様に分岐管18からは弁28を介して給気放出通118
29が接続されていて、この給気放出通路29に送り込
まれた他の一部の給気が熱交換器3oの二次側に導入さ
れて、排気タービン14を出た排気ガスの廃熱を回収し
て熱風に変換されて接続管31から供給される。従って
、過給機13の排気タービン14からの排気ガスは接続
管33および伸縮継手34を介して熱交換器3oの一次
側に導入されてこの熱交換器3oにおいて給気放出通’
71B 29からの給気と熱交換されて、排気ガスの廃
熱が回収されて接続管35から大気に放出される。
The rotational energy recovered by this exhaust turbine 14 is transferred to the shaft 15.
The air is transmitted to the air compressor 16 of the supercharger 13, and the air compressor 16 compresses the air sucked in from the atmosphere, and from the air air outlet 17, via the air cooler 26, and from the air air intake passage 27 to the internal combustion engine r! At the same time, part of the air supply is branched from the branch pipe 18 and sent to the air supply bypass passage 19 as bypass air supply. Similarly, the branch pipe 18 is connected to a supply air discharge port 118 via a valve 28.
29 is connected, and the other part of the supply air sent into this supply air discharge passage 29 is introduced into the secondary side of the heat exchanger 3o, and the waste heat of the exhaust gas exiting the exhaust turbine 14 is absorbed. It is collected, converted into hot air, and supplied from the connecting pipe 31. Therefore, the exhaust gas from the exhaust turbine 14 of the supercharger 13 is introduced into the primary side of the heat exchanger 3o via the connecting pipe 33 and the expansion joint 34, and the supply air is discharged through the heat exchanger 3o.
71B 29, waste heat of the exhaust gas is recovered and released to the atmosphere through the connecting pipe 35.

図示される櫟に、内燃機関の機関本体1oの負荷が低い
場合、または熱風エネルギの需要負荷に対して相対的に
機関本体1oの出力が小さい場合には、内燃機関の機関
本体1oから流出して第1の排気管11の各排気管1 
】−a、llb、llcと第2の排気管12の各排気管
12a、12b12cに夫々流入して過給I!13のの
排気タービン14に導入された排気ガスエネルギが不足
するために、排気タービン14で回収された回転エネル
ギが軸15によって空気圧縮機16に伝達されるが、空
気圧縮機16が大気から吸入して圧縮する給気の圧縮仕
事が不足して給気圧力や給気量が不足する結果、空気圧
縮機16の給気出口17から分岐管18、弁28、給気
放出通路29を経て熱交換器30で廃熱を回収して加熱
される給気は排気タービン14からの流出する排気ガス
の廃熱も不足するために回収廃熱が小さく、接続管31
から供給される給気の一部を変換した熱風のエネルギお
よび風量とも共に不足することになる。
As shown in the diagram, when the load on the engine body 1o of the internal combustion engine is low, or when the output of the engine body 1o is small relative to the demand load of hot air energy, the flow out from the engine body 1o of the internal combustion engine is shown. Each exhaust pipe 1 of the first exhaust pipe 11
]-a, llb, llc and each exhaust pipe 12a, 12b12c of the second exhaust pipe 12, supercharging I! Since the exhaust gas energy introduced into the exhaust turbine 14 of 13 is insufficient, the rotational energy recovered by the exhaust turbine 14 is transmitted to the air compressor 16 by the shaft 15, but the air compressor 16 draws in air from the atmosphere. As a result, heat is released from the air supply outlet 17 of the air compressor 16 via the branch pipe 18, the valve 28, and the air supply discharge passage 29. The supply air heated by recovering waste heat in the exchanger 30 also lacks the waste heat of the exhaust gas flowing out from the exhaust turbine 14, so the recovered waste heat is small, and the connecting pipe 31
Both the energy and volume of the hot air, which is obtained by converting a portion of the supply air supplied from the source, will be insufficient.

従って、この場合には、空気圧縮機16の給気出口17
から給気バイパス通路19を経て空気流量調節弁20で
流量調節された給気を接続管2】から燃料燃焼装置22
に供給して、外部から燃料供給管32によって供給され
た燃料と共に追焚き燃焼を行って得た燃焼ガスを燃焼ガ
ス用の連結管23の接続管24で第1、第2の排気管1
1.12と夫々付加容積管25.25で連結した流路で
内燃機関の機関本体】0からの排気ガスと混合して過給
機13の排気タービン14に第1、第2の排気管11.
12と、燃料燃焼装置22の連結管23の接続管24か
ら導入して排気タービン14から軸15を経て不足した
回転エネルギを補って空気圧縮機16の圧縮仕事を増加
して、給気出口17、分岐管18、弁28、給気放出通
路29を経て熱交換器30に導入される給気の圧力と量
を増加すると共に、排気タービン14から流出する排気
ガス量、温度の増加上昇を得て熱交換器30で回収する
廃熱も増加して接続管31から供給する熱風エネルギと
その風量の不足を補うことが出来る。
Therefore, in this case, the air supply outlet 17 of the air compressor 16
The supply air whose flow rate is adjusted by the air flow control valve 20 is passed through the supply air bypass passage 19 from the connecting pipe 2 to the fuel combustion device 22.
The combustion gas obtained by reheating and combustion together with the fuel supplied from the outside through the fuel supply pipe 32 is transferred to the first and second exhaust pipes 1 through the connecting pipe 24 of the connecting pipe 23 for combustion gas.
1.12 and the engine body of the internal combustion engine through flow paths connected with additional volume pipes 25 and 25 respectively. ..
12, and is introduced from the connecting pipe 24 of the connecting pipe 23 of the fuel combustion device 22 and passes from the exhaust turbine 14 through the shaft 15 to supplement the insufficient rotational energy and increase the compression work of the air compressor 16. , the pressure and amount of the supply air introduced into the heat exchanger 30 through the branch pipe 18, the valve 28, and the supply air discharge passage 29 are increased, and the amount and temperature of the exhaust gas flowing out from the exhaust turbine 14 are increased. The waste heat recovered by the heat exchanger 30 also increases, making it possible to compensate for the shortage of hot air energy and air volume supplied from the connecting pipe 31.

図示される様に、排気タービン14を流出した排気ガス
は接続管33、伸縮継手34を経て熱交換器30の一次
側に導入されて二次側の給気によって廃熱が回収された
後に接続管35から大気に放出される。
As shown in the figure, the exhaust gas flowing out of the exhaust turbine 14 is introduced into the primary side of the heat exchanger 30 via a connecting pipe 33 and an expansion joint 34, and after waste heat is recovered by supply air on the secondary side, the exhaust gas is connected. It is discharged to the atmosphere through pipe 35.

[発明の効果] この様に、この発明の燃料燃焼装置を備えたターボ過給
機関の熱風供給装置に依れば、ターボ過給機関の低負荷
域の運転においても、過給機の空気圧縮機から内燃機関
の機関本体をバイパスする給気バイパス通路を設けてバ
イパスする給気量を空気流量調節弁で調節した後に、バ
イパス給気を燃料燃焼装置の燃焼空気に利用した燃焼ガ
スを機関本体からの排気ガスと混合して過給機の排気タ
ービンに供給することによって、ターボ過給機関の外部
に供給する一部の給気量と給気圧力の上昇を得ると共に
、過給機の排気タービンから流出する排気ガスの廃熱量
の上昇も得て、排気タービン出口に設けられた熱交換器
によってターボ過給機関の外部へ供給する一部の給気を
変換した熱風の温度と風量とを増加させることを可能に
する。また、ターボ過給機関の常用負荷域の運転におい
ても、過給機の排気タービンのタービン面積を小さくす
ることによって排気タービンにおける熱落差を大きくし
て給気の一部をターボ過給機関の外部へ取り出して排気
タービンの出口に設けられた熱交換器によって排気ガス
廃熱を回収した熱風のエネルギと風量とが需要負荷に対
して不足する場合には機関本体をバイパスする給気バイ
ノくス通路に設けられた燃料燃焼装置の追焚き燃焼ガス
を機関本体から流出する排気ガスと混合して過給機の排
気タービンに供給することによって熱風のエネルギと風
量とを増加させて補うことが出来る。
[Effects of the Invention] As described above, according to the hot air supply device for a turbocharged engine equipped with the fuel combustion device of the present invention, even when the turbocharged engine is operated in a low load range, the air compression of the turbocharger can be improved. After installing an air supply bypass passage that bypasses the engine body of the internal combustion engine from the aircraft and adjusting the amount of bypass air supply with an air flow control valve, the combustion gas that uses the bypass air supply as combustion air for the fuel combustion device is transferred to the engine body. By mixing with the exhaust gas from the turbocharger and supplying it to the exhaust turbine of the turbocharger, a part of the charge air amount and pressure to be supplied to the outside of the turbocharged engine can be obtained, and at the same time, the exhaust gas of the turbocharger By obtaining an increase in the amount of waste heat of the exhaust gas flowing out from the turbine, the temperature and air volume of the hot air converted from a part of the supply air supplied to the outside of the turbocharged engine by the heat exchanger installed at the exhaust turbine outlet are increased. allow to increase. In addition, when operating a turbocharged engine in the normal load range, by reducing the turbine area of the exhaust turbine of the turbocharger, the heat drop in the exhaust turbine is increased and a portion of the charge air is transferred outside the turbocharged engine. When the energy and air volume of the hot air, which is extracted from exhaust gas waste heat and recovered by a heat exchanger installed at the exit of the exhaust turbine, is insufficient for the demand load, an air supply binox passage bypasses the engine main body. The energy and volume of the hot air can be increased and supplemented by mixing the reheated combustion gas from the fuel combustion device installed in the engine with the exhaust gas flowing out from the engine body and supplying the mixture to the exhaust turbine of the supercharger.

従って、ターボ過給機関から外部に供給する給気の一部
を排気タービン出口に設けられた熱交換器によって排気
ガスの廃熱を回収した熱風のエネルギを利用する場合に
おいてもターボ過給I!!関の負荷に拘わらず所要の熱
風のエネルギと風量との供給を可能にして、本来の目的
である廃熱利用のターボ過給機関の熱風供給装置の不都
合を解消して、廃熱利用の機会の増大による省エネルギ
等の効果が得られるものであり、熱風の温度が200℃
以上の温度レベルにおいて加熱、暖房、更には空気エネ
ルギの特性を活かして吸着除湿装置と組み合せた調湿、
乾燥の用途等の省エネルギ効果が得られるものである。
Therefore, even when part of the air supplied to the outside from a turbocharged engine is used as the energy of hot air, which is the waste heat of the exhaust gas recovered by the heat exchanger installed at the exhaust turbine outlet, the turbocharger I! ! By making it possible to supply the necessary amount of hot air energy and air volume regardless of the load on the engine, it eliminates the inconveniences of hot air supply devices for turbocharged engines that use waste heat, which is the original purpose, and creates opportunities to use waste heat. Effects such as energy saving can be obtained by increasing the temperature of the hot air at 200°C.
At the above temperature level, heating, space heating, and even humidity control in combination with an adsorption dehumidifier that takes advantage of the characteristics of air energy,
This provides an energy saving effect for drying purposes, etc.

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

図面はこの発明の燃料燃焼装置を備えたターボ過給機関
の熱風供給装置の概要図である6図中、1:ターボ過給
機関、2;熱風供給装置、10:内燃機関の機関本体・
、11、lla、llb、11c、12.12a、12
b、12c:排気管、13:過給機、14:排気タービ
ン、15:軸、16:空気圧縮機、17:給気出口、1
8:分岐管、19:給気バイパス通路、20:空気流量
調節弁、21;接続管、22・燃料燃焼装置、23二連
結管、24:接続管、25:負荷容積管、26:空気冷
却器、27:給気道路、28:弁、29;給気放出通路
、30:熱交換器、31.33.35:接続管、34:
伸縮継手。
The drawing is a schematic diagram of a hot air supply device for a turbocharged engine equipped with a fuel combustion device of the present invention.In Figure 6, 1: turbocharged engine; 2: hot air supply device;
, 11, lla, llb, 11c, 12.12a, 12
b, 12c: exhaust pipe, 13: supercharger, 14: exhaust turbine, 15: shaft, 16: air compressor, 17: air supply outlet, 1
8: Branch pipe, 19: Air supply bypass passage, 20: Air flow rate control valve, 21; Connecting pipe, 22 - Fuel combustion device, 23 Two connecting pipes, 24: Connecting pipe, 25: Load volume pipe, 26: Air cooling vessel, 27: air supply road, 28: valve, 29; air supply discharge passage, 30: heat exchanger, 31.33.35: connecting pipe, 34:
Expansion joints.

Claims (1)

【特許請求の範囲】 内燃機関の機関本体と過給機の空気圧縮機とを連通する
給気通路から分岐する給気バイパス通路を有するターボ
過給機関において、 給気バイパス通路中に設けられた空気流量調節弁、該空
気流量調節弁の後に設けられた燃料燃焼装置、該燃料燃
焼装置の燃焼ガスと該機関本体からの排気ガスとを混合
して該過給機の排気タービンに導入する連結管を備える
と共に、該過給機の空気圧縮機と連通する給気通路から
分岐する給気放出通路、該給気放出通路の後に設けられ
て該過給機の排気タービン出口の排気ガスによって給気
を加熱する熱交換器を備えたことを特徴とする、燃料燃
焼装置を備えたターボ過給機関の熱風供給装置。
[Scope of Claims] In a turbocharged engine having an air intake bypass passage that branches from an air intake passage that communicates the engine body of the internal combustion engine with an air compressor of a supercharger, the turbocharged engine is provided in the air intake bypass passage. An air flow control valve, a fuel combustion device provided after the air flow control valve, and a connection that mixes combustion gas from the fuel combustion device and exhaust gas from the engine main body and introduces the mixture into the exhaust turbine of the supercharger. A supply air discharge passage branching from a supply air passage communicating with the air compressor of the supercharger, and a supply air discharge passage provided after the supply air discharge passage and supplied with exhaust gas from the exhaust turbine outlet of the supercharger. A hot air supply device for a turbocharged engine equipped with a fuel combustion device, characterized in that it is equipped with a heat exchanger that heats air.
JP2144345A 1990-06-04 1990-06-04 Hot air supply device for turbo supercharging engine with fuel combustion device Pending JPH0441932A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2144345A JPH0441932A (en) 1990-06-04 1990-06-04 Hot air supply device for turbo supercharging engine with fuel combustion device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2144345A JPH0441932A (en) 1990-06-04 1990-06-04 Hot air supply device for turbo supercharging engine with fuel combustion device

Publications (1)

Publication Number Publication Date
JPH0441932A true JPH0441932A (en) 1992-02-12

Family

ID=15359952

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2144345A Pending JPH0441932A (en) 1990-06-04 1990-06-04 Hot air supply device for turbo supercharging engine with fuel combustion device

Country Status (1)

Country Link
JP (1) JPH0441932A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010274905A (en) * 2009-05-26 2010-12-09 Man Diesel Se Ship propulsion system and ship equipped with the system
CN108481899A (en) * 2018-02-12 2018-09-04 西北大学 A kind of thermally equilibrated backheating type air, which can be dried, utilizes method and system

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010274905A (en) * 2009-05-26 2010-12-09 Man Diesel Se Ship propulsion system and ship equipped with the system
CN108481899A (en) * 2018-02-12 2018-09-04 西北大学 A kind of thermally equilibrated backheating type air, which can be dried, utilizes method and system
CN108481899B (en) * 2018-02-12 2019-07-09 西北大学 A kind of thermally equilibrated backheating type air, which can be dried, utilizes method and system

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