Nothing Special   »   [go: up one dir, main page]

JPS62178756A - Air preheater and combustor for external combustion engine - Google Patents

Air preheater and combustor for external combustion engine

Info

Publication number
JPS62178756A
JPS62178756A JP1964086A JP1964086A JPS62178756A JP S62178756 A JPS62178756 A JP S62178756A JP 1964086 A JP1964086 A JP 1964086A JP 1964086 A JP1964086 A JP 1964086A JP S62178756 A JPS62178756 A JP S62178756A
Authority
JP
Japan
Prior art keywords
air
spiral
combustion
air preheater
combustor
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
JP1964086A
Other languages
Japanese (ja)
Inventor
Hideki Koseki
秀規 小関
Masahiro Sakai
正博 酒井
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP1964086A priority Critical patent/JPS62178756A/en
Publication of JPS62178756A publication Critical patent/JPS62178756A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02GHOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G2243/00Stirling type engines having closed regenerative thermodynamic cycles with flow controlled by volume changes

Landscapes

  • Air Supply (AREA)

Abstract

PURPOSE:To perform flame holding action, by forming an air preheater of a Stirling engine in a spiral-type air preheater and supplying preheated air in a spiral state into a combustion chamber. CONSTITUTION:Two sheets of discs are spirally wound in the periphery of a combustion chamber 6 in the upper part of a Stirling engine, forming spiral- shaped passages of two systems in the inside. One of the passages serves as a combustion gas passage from a hole 12, and the other passage serves as a combustion air passage from a hole 13. Combustion air, which passes through the spiral-shaped passage being heated, is allowed to flow into a combustion chamber 6 from a hole 9. Since an inflow of the combustion air rotates in a spiral state, the inflow air in the combustion chamber acts so as to hold a flame of a burner.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明は、外燃機関の空気予熱器及び燃焼器に関する
ものである。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] This invention relates to an air preheater and combustor for an external combustion engine.

〔従来技術〕[Prior art]

第4図は従来のスターリングエンジン用空気予熱器及び
燃焼器を示す断面図であり、図において、■はシェルア
ンドチューブ形空気予熱器、2は空気予熱器1のチュー
ブ、3は同じくシェル、4は燃焼器の空気旋回用案内羽
根、5は燃料ノズル、6は燃焼室、7は作動ガスと燃焼
ガス間で熱交換を行う熱交換器、8は断熱材である。
Fig. 4 is a sectional view showing a conventional air preheater and combustor for a Stirling engine. 5 is a fuel nozzle, 6 is a combustion chamber, 7 is a heat exchanger for exchanging heat between working gas and combustion gas, and 8 is a heat insulating material.

次に動作について説明する。Next, the operation will be explained.

空気予熱器1に導入された常温の燃焼用空気は、チュー
ブ2の内部を通過する際に該チューブ2の周囲に存在す
る燃焼ガスとの間で熱交換され、燃焼ガスより熱エネル
ギを受けて高温の予熱空気となることにより、排熱回収
が行われる。その後予熱空気は案内羽根4によって旋回
がかけられ、燃料ノズル5より噴射された燃料と混合さ
れて着火。
When the combustion air at room temperature introduced into the air preheater 1 passes through the tube 2, it exchanges heat with the combustion gas existing around the tube 2, and receives heat energy from the combustion gas. Exhaust heat is recovered by becoming high-temperature preheated air. Thereafter, the preheated air is swirled by the guide vanes 4, mixed with fuel injected from the fuel nozzle 5, and ignited.

燃焼される。ここで、案内羽根4は空気に旋回をかける
ことにより燃焼室6内に逆流領域を形成し、保炎を行う
ために設けられたものである。そして上記燃焼室6を出
た燃焼ガスは、熱交換器7において作動ガスに熱エネル
ギを与えた後、空気予熱器Iに導入され、チューブ2の
中の燃焼用空気に熱エネルギを与えた後に系外に排出さ
れる。このとき空気予熱器1の外部には、周囲雰囲気へ
の熱損失を減少させるために断熱材8が配設されている
be burned. Here, the guide vanes 4 are provided to form a backflow region in the combustion chamber 6 by swirling the air and to perform flame stabilization. The combustion gas leaving the combustion chamber 6 imparts thermal energy to the working gas in the heat exchanger 7, and then is introduced into the air preheater I, where it imparts thermal energy to the combustion air in the tube 2. It is discharged outside the system. At this time, a heat insulating material 8 is disposed outside the air preheater 1 in order to reduce heat loss to the surrounding atmosphere.

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

従来の空気予熱器及び燃焼器は以上のように構成されて
おり、高温の燃焼ガスが直接シェル3に接し、そのため
外部への熱損失を減少させるために断熱材8を必要とし
た。また空気予熱器1を通過した予熱空気は、保炎のた
め改めて案内羽根4で旋回を与える必要があり、このた
め装置の小型化が困難であるという問題があった。
The conventional air preheater and combustor are constructed as described above, and the high-temperature combustion gas comes into direct contact with the shell 3, so that the heat insulating material 8 is required to reduce heat loss to the outside. Furthermore, the preheated air that has passed through the air preheater 1 needs to be swirled again by the guide vanes 4 in order to stabilize the flame, which makes it difficult to miniaturize the device.

この発明は、上記のような点に鑑み、断熱材、案内羽根
を不要とし、構造的に簡素化、小型化された外燃機関用
空気予熱器及び燃焼器を得ることを目的とする。
In view of the above-mentioned points, it is an object of the present invention to provide an air preheater and a combustor for an external combustion engine that do not require heat insulating materials or guide vanes and are structurally simplified and downsized.

〔問題点を解決するための手段〕[Means for solving problems]

この発明に係る外燃機関用空気予熱器及び燃焼器は、燃
焼器の周囲にスパイラル形空気予熱器を配設し、これに
より所定の角運動量を有する旋回空気流を燃焼器に導入
Qて燃焼器をサイクロン形としたものである。
The air preheater and combustor for an external combustion engine according to the present invention include a spiral air preheater disposed around the combustor, whereby a swirling air flow having a predetermined angular momentum is introduced into the combustor and combusted. The vessel is shaped like a cyclone.

〔作用〕[Effect]

この発明においては、燃焼室周囲にスパイラル形空気予
熱器が配設されているから燃焼室から周囲雰囲気への熱
損失が減少し、また燃焼用空気番こより高温部が断熱さ
れるため特に断熱材を必要としない。さらに、燃焼用空
気はスパイラル状の空気予熱器を通過する際に角運動量
を持つことになり、これが燃焼器に導入されることによ
って旋回空気流が得られるから、特に案内羽根を必要と
しない。
In this invention, since the spiral air preheater is disposed around the combustion chamber, heat loss from the combustion chamber to the surrounding atmosphere is reduced, and since the high temperature part is insulated from the combustion air chamber, especially the heat insulating material is used. does not require. Furthermore, the combustion air has angular momentum when passing through the spiral air preheater, and a swirling air flow is obtained by introducing this into the combustor, so that no guide vanes are particularly required.

〔実施例〕〔Example〕

以下、本発明の実施例を図について説明する。 Hereinafter, embodiments of the present invention will be described with reference to the drawings.

第1図において、14は燃焼室6の周囲に配設されたス
パイラル形空気予熱器であり、その内部には隔壁15に
より空気、燃焼ガスの各通路がらせん状に形成されてい
る(第2図参照)。また16は上記隔壁15とともに空
気予熱器14を構成するパツキン、17はパツキン押さ
えである。5は燃料ノズル、18は該燃料ノズル5の先
端に設けられた燃料噴射孔、7はエンジンの作動ガスと
燃焼ガス間で熱交換を行う熱交換器、9,13はスパイ
ラル形空気予熱器1の空気出口、入口、10は空気旋回
室、11は空気絞り、12.19はスパイラル形空気予
熱器1の燃焼ガス入口、出口である。なお、図中空気予
熱器1の中の口 で示した個所は燃焼ガス、その他の個
所は空気を示し、またこの第1図においては隔壁15間
に挿入され、該隔壁15を支持するスペーサは図示して
いない。
In FIG. 1, reference numeral 14 denotes a spiral air preheater disposed around the combustion chamber 6, inside which air and combustion gas passages are formed in a spiral shape by partition walls 15 (second (see figure). Further, 16 is a packing that constitutes the air preheater 14 together with the partition wall 15, and 17 is a packing holder. 5 is a fuel nozzle; 18 is a fuel injection hole provided at the tip of the fuel nozzle 5; 7 is a heat exchanger for exchanging heat between the working gas of the engine and combustion gas; 9 and 13 are spiral air preheaters 1; 10 is an air swirling chamber, 11 is an air throttle, and 12.19 is a combustion gas inlet and outlet of the spiral air preheater 1. In the figure, the part indicated by the opening in the air preheater 1 represents combustion gas, and the other parts represent air. In addition, in FIG. 1, the spacer inserted between and supporting the partition wall 15 is Not shown.

第2図にスパイラル形熱交換器の概略断面図を示す。図
中、−一一一は燃焼ガスの流れ、−は空気の流れを表す
FIG. 2 shows a schematic cross-sectional view of a spiral heat exchanger. In the figure, -111 represents the flow of combustion gas, and - represents the flow of air.

次に作用効果について説明する。Next, the effects will be explained.

スパイラル形熱交換器14の空気人口13より導入され
た燃焼用空気は、うず巻状の流路を有するスパイラル形
空気予熱器内部を通過する際に、燃焼ガスと隔壁15ご
しに接触して燃焼ガスより熱エネルギを受け、高温空気
となりつつ流路に沿って流れる。このため燃焼用空気は
角運動量を有するようになる。この角運動量を持つ予熱
空気はスパイラル形空気予熱器14の空気出口9より旋
回室10に入る。予熱空気は空気絞り11で一度絞られ
た後に燃料ノズル5の燃料噴射孔18より噴射される燃
料と混合され燃焼する。このとき予熱空気は旋回流とな
って燃焼室6に導入されるため、従来のような特別の保
炎器を必要としない。
The combustion air introduced from the air port 13 of the spiral heat exchanger 14 comes into contact with the combustion gas through the partition wall 15 when passing through the spiral air preheater having a spiral flow path. It receives thermal energy from the combustion gas and becomes high-temperature air as it flows along the flow path. Therefore, the combustion air has angular momentum. The preheated air with this angular momentum enters the swirling chamber 10 through the air outlet 9 of the spiral air preheater 14. After the preheated air is once throttled by the air throttle 11, it is mixed with fuel injected from the fuel injection hole 18 of the fuel nozzle 5 and combusted. At this time, the preheated air becomes a swirling flow and is introduced into the combustion chamber 6, so there is no need for a special flame stabilizer as in the conventional case.

燃焼ガスは熱交換器7で作動ガスと熱交換された後、ス
パイラル形空気予熱器14の燃焼ガス人口12より空気
予熱器14内に入り、新たに該空気予熱器14内に導入
された空気に熱エネルギを与えた後に系外に出口19よ
り排出される。このときスパイラル形空気予熱器14は
、燃焼室6.熱交換器7なる高温部を空気によってうず
巻状に取り囲んでいるため、従来装置のような特別の断
熱材は必要としない。
After the combustion gas exchanges heat with the working gas in the heat exchanger 7, the combustion gas enters the air preheater 14 through the combustion gas port 12 of the spiral air preheater 14, and the air newly introduced into the air preheater 14 enters the air preheater 14. After imparting thermal energy to it, it is discharged from the system through the outlet 19. At this time, the spiral air preheater 14 is connected to the combustion chamber 6. Since the high-temperature part of the heat exchanger 7 is surrounded by air in a spiral shape, no special heat insulating material is required as in conventional devices.

なお、上記実施例では特に旋回を強める手段を用いてい
ないが、第3図に示すように、空気予熱器14の空気通
路の出口近傍に空気流を静圧から動圧へ変換する変換板
20、即ち空気の流通路を狭めて空気流速を上げるため
の仕切り板20を設けることにより、さらに強い旋回流
が得られる。
Although the above embodiment does not use any means to strengthen the swirl, as shown in FIG. 3, a conversion plate 20 for converting the air flow from static pressure to dynamic pressure is provided near the outlet of the air passage of the air preheater 14. That is, by providing the partition plate 20 to narrow the air flow path and increase the air flow velocity, a stronger swirling flow can be obtained.

なおこの第3図は、スパイラル形空気予熱器14を一部
展開して示したものである。
Note that FIG. 3 shows the spiral air preheater 14 partially expanded.

〔発明の効果〕〔Effect of the invention〕

以上のように、この発明によれば、燃焼室等の高温部を
スパイラル形空気予熱器で取り囲み、燃焼用空気で断熱
を行っているので特別な断熱材が不要となり、また燃焼
用空気はスパイラル形空気予熱器を通過する際に角運動
量を得るので、特別な保炎器なしで旋回流が得られ、こ
の結果構造の簡素化が達成でき、装置が安価に作成でき
る効果がある。
As described above, according to the present invention, a high-temperature part such as a combustion chamber is surrounded by a spiral air preheater and is insulated with combustion air, so there is no need for special insulation material, and the combustion air is spiral-shaped. Since angular momentum is obtained when passing through the shaped air preheater, a swirling flow can be obtained without a special flame stabilizer, and as a result, the structure can be simplified and the device can be manufactured at low cost.

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

第1図は本発明の一実施例による外燃機関用空気予熱器
及び燃焼器を示す断面側面図、第2図は同じくその断面
平面図、第3図は本発明の他の実施例による空気予熱器
を一部展開して示す図、第4図は従来の外燃機関用空気
予熱器及び燃焼器の断面側面図である。 5・・・燃料ノズル、6・・・燃焼室、7・・・熱交換
器、10・・・空気旋回室、11・・・空気絞り、14
・・・スパイラル形空気予熱器、20・・・空気静圧動
圧変換板。 なお図中同一符号は同−又は相当部分を示す。
FIG. 1 is a sectional side view showing an air preheater and combustor for an external combustion engine according to one embodiment of the present invention, FIG. 2 is a sectional plan view thereof, and FIG. 3 is an air preheater and combustor according to another embodiment of the present invention. FIG. 4 is a partially exploded view of the preheater, and is a cross-sectional side view of a conventional air preheater and combustor for an external combustion engine. 5... Fuel nozzle, 6... Combustion chamber, 7... Heat exchanger, 10... Air swirling chamber, 11... Air throttle, 14
...Spiral type air preheater, 20...Air static pressure dynamic pressure conversion plate. Note that the same reference numerals in the figures indicate the same or equivalent parts.

Claims (1)

【特許請求の範囲】[Claims] (1)外燃機関の燃焼器の周囲に、らせん状の空気通路
及び上記燃焼器の排気ガス通路を有し上記排気ガスの保
有する熱エネルギを燃焼用空気に回収するためのスパイ
ラル形空気予熱器が設けられ、該スパイラル形空気予熱
器によって得られた角運動量を有する予熱空気を上記燃
焼器内に導入し保炎を行うようにしたことを特徴とする
外燃機関の空気予熱器及び燃焼器。
(1) A spiral air preheater having a spiral air passage and an exhaust gas passage of the combustor around the combustor of an external combustion engine and recovering the thermal energy possessed by the exhaust gas into combustion air. An air preheater and combustion for an external combustion engine, characterized in that the preheated air having angular momentum obtained by the spiral air preheater is introduced into the combustor to perform flame stabilization. vessel.
JP1964086A 1986-01-30 1986-01-30 Air preheater and combustor for external combustion engine Pending JPS62178756A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1964086A JPS62178756A (en) 1986-01-30 1986-01-30 Air preheater and combustor for external combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1964086A JPS62178756A (en) 1986-01-30 1986-01-30 Air preheater and combustor for external combustion engine

Publications (1)

Publication Number Publication Date
JPS62178756A true JPS62178756A (en) 1987-08-05

Family

ID=12004821

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1964086A Pending JPS62178756A (en) 1986-01-30 1986-01-30 Air preheater and combustor for external combustion engine

Country Status (1)

Country Link
JP (1) JPS62178756A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20220136456A1 (en) * 2020-11-02 2022-05-05 National Cheng Kung University Scroll heating device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20220136456A1 (en) * 2020-11-02 2022-05-05 National Cheng Kung University Scroll heating device
US11480133B2 (en) * 2020-11-02 2022-10-25 National Cheng Kung University Scroll heating device

Similar Documents

Publication Publication Date Title
JPH023086B2 (en)
JP2000028141A (en) Premixed fuel injector and its centerbody
WO2008047825A1 (en) Gas turbine combustor
US3015475A (en) Cylindrical heat exchanger
GB1410990A (en) Combustor and method of operating same
US2911957A (en) Resonant combustion apparatus
JPH11148605A (en) Regenerative burner
JPS62178756A (en) Air preheater and combustor for external combustion engine
JPS61184328A (en) Heat accumulation type heating system
JP2788698B2 (en) Low NOx combustion method and its burner
CA1147624A (en) Catalytic combustion system with fiber matrix burner
RU222049U1 (en) Steam turbine
SE8306420D0 (en) BURNER DEVICE
JPS5817364B2 (en) Low NOx radiant tube burner
JPS62123208A (en) Low nox duct burner for additional heating
JPS5812488B2 (en) hot gas engine combustor
JPS59131850A (en) Heat exchanger
JP3743530B2 (en) Gas turbine combustor
JPH0220890B2 (en)
RU2170881C1 (en) Ceramic gas burner
EP0266857A3 (en) Cyclonic combustor and boiler incorporating such a combustor
JPS6336052A (en) High temperature heat exchanger of stirling engine
SU1201623A1 (en) Air preheater
RU1813986C (en) Unit-type burner
RU1779880C (en) Regenerative burner