JPS58220960A - Pressurized air system fuel injector - Google Patents

Pressurized air system fuel injector

Info

Publication number
JPS58220960A
JPS58220960A JP10361582A JP10361582A JPS58220960A JP S58220960 A JPS58220960 A JP S58220960A JP 10361582 A JP10361582 A JP 10361582A JP 10361582 A JP10361582 A JP 10361582A JP S58220960 A JPS58220960 A JP S58220960A
Authority
JP
Japan
Prior art keywords
air
valve
compressor
fuel injection
pressure
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
JP10361582A
Other languages
Japanese (ja)
Inventor
Hirobumi Nakano
博文 中野
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.)
Yanmar Co Ltd
Original Assignee
Yanmar Diesel Engine Co Ltd
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 Yanmar Diesel Engine Co Ltd filed Critical Yanmar Diesel Engine Co Ltd
Priority to JP10361582A priority Critical patent/JPS58220960A/en
Publication of JPS58220960A publication Critical patent/JPS58220960A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M67/00Apparatus in which fuel-injection is effected by means of high-pressure gas, the gas carrying the fuel into working cylinders of the engine, e.g. air-injection type
    • F02M67/02Apparatus in which fuel-injection is effected by means of high-pressure gas, the gas carrying the fuel into working cylinders of the engine, e.g. air-injection type the gas being compressed air, e.g. compressed in pumps

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

PURPOSE:To prevent defective operation of a change-over mechanism due to heat thereof and improve the injection property and combustion property of fuel by providing a check valve having high heat resisting property and pressure resisting property in the change-over mechanism for a pressurized air supply source. CONSTITUTION:While a fuel injector Z1 supplies pressurized air from an air tank 3 to a fuel injection valve 2 in the start of an engine having low discharge pressure of a compressor 1, it shuts off air from the tank 3 to supply pressurized air from the compressor 1 when the discharge pressure reaches at least a set value. A check valve 15 having high heat and pressure resisting properties is arranged at the very hot air path 21 side of this change-over mechanism so that a solenoid change-over valve 6 and a constant differential pressure valve 7 in an air path 22 connected from the air tank 3 to the downstream air side of the check valve 15 are not exposed directly to hot air from the compressor 1, the solenoid change-over valve 6 does not have any defective operations due to temperature rise and the change-over operation of an air supply source has no troubles.

Description

【発明の詳細な説明】 本発明は、空気式燃料噴射弁を使用した加圧空気式燃料
噴射装置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a pressurized pneumatic fuel injection device using a pneumatic fuel injection valve.

この種の燃料噴射装置は、エンジンによって駆動される
圧縮機からの加圧空気を燃料噴射弁に導専、この加圧空
気によって燃料を霧化してシリンダ内に噴射するように
なっているが、エンジン始動時には圧縮機の吐出圧力が
低く、しかも、その空気微も少ないため、この場合には
別置きのエアータンク等から所定圧力に圧力設定された
加圧空気を一時的に燃料噴射弁に供給する必要がある。
This type of fuel injection device directs pressurized air from a compressor driven by an engine to a fuel injection valve, and uses this pressurized air to atomize fuel and inject it into a cylinder. When the engine starts, the discharge pressure of the compressor is low and the amount of air is small, so in this case, pressurized air set to a predetermined pressure is temporarily supplied to the fuel injection valve from a separate air tank, etc. There is a need to.

このよう罠、空気供給源をエンジンの運転状態に応じて
切換えるために従来の燃料噴射装置においては、空気供
給路中に空気源の切換え装置として圧縮機の吐出圧(即
ち、エンジンの運転状態)K応じて開閉作動する電磁切
換弁を設け、仁の電磁切換弁によって圧縮機とエアータ
ンクとを燃料噴射弁に択一的に接続するようにしていた
In conventional fuel injection systems, an air source switching device is installed in the air supply path in order to switch the air supply source according to the operating state of the engine. An electromagnetic switching valve that opens and closes depending on the timing is provided, and the compressor and the air tank are selectively connected to the fuel injection valve by the electromagnetic switching valve.

とξろが、このように電磁切換弁を使用した切換装置を
有する従来の燃料噴射装置においては、電磁切換弁が直
接に/ 001.!〜4100℃という高圧高温の圧縮
機からの吐出空気に晒されるため、電磁切換弁のソレノ
イドコイルの磁力吸引力が温度上昇に伴って次第に低下
して該電磁切換弁が作動不良となり、その結果、燃料の
噴射特性及び燃焼特性が悪化するという問題があった。
However, in a conventional fuel injection device having a switching device using an electromagnetic switching valve as described above, the electromagnetic switching valve directly operates /001. ! Because it is exposed to air discharged from the compressor at a high pressure and high temperature of ~4100°C, the magnetic attraction force of the solenoid coil of the electromagnetic switching valve gradually decreases as the temperature rises, causing the electromagnetic switching valve to malfunction. There was a problem that the injection characteristics and combustion characteristics of the fuel deteriorated.

本発明は、上記の如き従来の加圧空気式燃料噴射装置の
問題に鑑み、熱による切換装置の作動不良を未然に防止
することによυ、燃料の噴射特性及び燃焼特性の向上を
図シ得るようにした加圧空気式燃料噴射装置を提供する
ことを目的としてなされたものであって、加圧空気によ
って燃料を霧化して噴射するようKした空気式燃料噴射
弁とエンジンによって駆動される圧縮機を、その途中に
前記燃料噴射弁側から前記圧縮機側への空気の逆流を防
止す杢如く作用する逆止弁を介在せしめた第1空気路を
介して接続するとともに、該第1空気路の前記逆止弁よ
り空気下流側位置に第2空気路を介してエアータンクを
接続し、さらK、前記第2空気路には、エンジンの運転
状態に応じてれ第!空気路を適宜に開閉制御する制御弁
と前記第!空気路を通って前記第1空気路側に供給され
る前記エアータンクからの空気圧を前記圧縮機/の吐出
圧より一定圧力だけ高圧に設定する如く作用する定差圧
弁を介在せしめたことを特徴とするものである。
In view of the problems of the conventional pressurized air fuel injection device as described above, the present invention aims to improve the injection characteristics and combustion characteristics of fuel by preventing malfunction of the switching device due to heat. The purpose of this invention is to provide a pressurized air fuel injection device which is driven by an engine and a pneumatic fuel injection valve designed to atomize and inject fuel using pressurized air. The compressor is connected to the compressor via a first air passage having a check valve interposed therebetween that acts like a heather to prevent backflow of air from the fuel injection valve side to the compressor side; An air tank is connected to a position downstream of the check valve in the air passage via a second air passage, and an air tank is connected to the second air passage depending on the operating state of the engine. A control valve for controlling the opening and closing of the air passage as appropriate; A constant differential pressure valve is interposed that operates to set the air pressure from the air tank supplied to the first air path side through the air path to a pressure higher than the discharge pressure of the compressor by a certain pressure. It is something to do.

/実施例罠係る燃料噴射装置Z、が示されている。/Embodiment A fuel injection device Z according to the embodiment is shown.

この燃料噴射装置z1け、ガスタービンエンジンに装着
される空気式の燃料噴射弁、、l:、エンジンによって
駆動される圧縮機/の加圧空気とエンジンとは別に設置
したエアタンク3内の加圧空気をエンジンの運転状態(
エンジン始動時とエンジン始動後)に応じて択−的罠供
給し、この供給された加圧空気によって燃料管ノ0を介
して燃料ポンプj側から圧送された燃料を空気と混合し
て各気筒内に噴射するよう罠なっておシ、圧縮機lと燃
料噴射弁ノを接続する第1空気路、2/の中間部にエア
ータンク3からの第2空気路、?ノが接続されている。
This fuel injection device is a pneumatic fuel injection valve installed in a gas turbine engine, and the pressurized air in a compressor driven by the engine and the air tank 3 installed separately from the engine are pressurized. Air is controlled by engine operating conditions (
The supplied pressurized air mixes the fuel pumped from the fuel pump J side through the fuel pipe No. 0 with air and supplies it to each cylinder. The first air path connects the compressor 1 and the fuel injection valve, and the second air path from the air tank 3 is in the middle of 2/2. is connected.

この第1空気m、2iと第2空気路Ωノには、なす切換
装RXが取付けられている。
A switching device RX is attached to the first air paths m, 2i and the second air path Ω.

切換装RX i、i、第1空気路、、2/と第2空気路
〃の合流点よシ空気上流位置に配置されて燃料噴射弁!
側から圧縮機/側への空気の逆流を阻止する如く作用す
る第1逆止弁/jと、第1空気路λ!中に配置されて圧
縮機/の吐出圧に応じて該第2空気路、2.2を自閉す
る如く作用する電磁切換非Aと、同じく第1空気路、2
2中の前記電磁切換非Aよシ空気下流側圧配置されてエ
アータンク3側から燃料噴射弁!側に供給される空気の
圧力を圧縮機/の吐出圧より一定圧力だけ高圧に設定す
る如く6用する定差圧弁7より構成されている。
Switching equipment RX i, i, the fuel injection valve is located at the air upstream position from the confluence of the first air path, 2/ and the second air path!
A first check valve /j acts to prevent backflow of air from the side to the compressor/side, and a first air path λ! an electromagnetic switching switch A disposed in the compressor and acting to self-close the second air passage 2.2 in response to the discharge pressure of the compressor;
In 2, the electromagnetic switching non-A side air pressure is arranged on the downstream side of the air tank 3 side to the fuel injection valve! It is comprised of a constant differential pressure valve 7 which is used to set the pressure of air supplied to the side at a constant pressure higher than the discharge pressure of the compressor.

又、電磁切換非Aの制御回路YKは、エンジンの起動ス
イッチ(図示省略)と連動する主スィッチ10と、第j
空気M、ltを介して負荷される圧縮機/の吐出圧によ
って開閉する圧カス・イツヂグ/が介設さり、ている。
Further, the electromagnetic switching non-A control circuit YK includes a main switch 10 that operates in conjunction with an engine starting switch (not shown), and a j-th
There is interposed a pressure valve which opens and closes depending on the discharge pressure of the compressor which is loaded via air M, lt.

尚、この圧力スイッチll/は、圧縮機/の吐出圧が所
定の設定圧以下に下がった場合に電磁切換非Aを開弁す
るようにされている。
The pressure switch ll/ is configured to open the electromagnetic switching valve A when the discharge pressure of the compressor/ falls below a predetermined set pressure.

尚、符号/乙は第1空気路、2/と第1空気路、2.2
をバイパスするバイパス路23に設けた逆止弁、□、2
Aは定差圧弁7の流出圧を設定するためのバ、イロット
空気路である。
In addition, the code /O is the first air path, 2/ and the first air path, 2.2
A check valve provided in the bypass passage 23 that bypasses the
A is an air passage for setting the outflow pressure of the constant differential pressure valve 7.

一方、エアータンク3には、充気路、2I1.を介して
充気用圧縮機グが接続されている。この充気用圧縮機≠
は、制御回路Qに設けた圧力スイッチ/、2によって検
知されたエアータンク3内の空気圧力が設定圧力(圧縮
機/の吐出圧力よ、bttんの少し低い圧力)より降下
した場合に運転され、該エアータンク3内の空気圧力を
設定値に保持する如く作用する。尚、符号/7は、エア
ータンク3内の加圧空気が充気用圧縮機j側に逆流する
のを防止する逆止弁である。
On the other hand, the air tank 3 has a charging path, 2I1. The charging compressor is connected via the. This charging compressor≠
is operated when the air pressure in the air tank 3 detected by the pressure switch /2 installed in the control circuit Q drops below the set pressure (compressor discharge pressure, a pressure slightly lower than btt). , acts to maintain the air pressure in the air tank 3 at a set value. In addition, the code|symbol /7 is a check valve which prevents the pressurized air in the air tank 3 from flowing back to the charging compressor j side.

続いて、上述の如く構成された第1実施例の燃料噴射装
@Z、の作用を説明すると、エンジンが適宜の始動装置
(図示省略)Kよって回転せしめられると(主スィッチ
10がON)、圧縮機/が回転し空気を圧送し始めるが
、この場合にはエンジンの回転数が低いため吐出圧及び
吐出量が少ない。
Next, the operation of the fuel injection system @Z of the first embodiment configured as described above will be explained. When the engine is rotated by an appropriate starter device (not shown) K (main switch 10 is turned on), The compressor starts rotating and pumping air, but in this case, the engine speed is low, so the discharge pressure and discharge amount are low.

このため、圧カスイツヂll/l−1:ON状態のまま
保持され、電磁切換非Aが開弁してエアータンク3内に
貯溜されていた加圧空気が第2空気路、2.2を通って
燃料噴射弁!側に供給される。この場合、定差圧弁7に
よって該定差圧弁7から流出する空気圧が圧縮機/の吐
出圧より一定圧だけ高くなるように設定されているため
、第1逆止弁/jは閉弁状態のまま保持され、燃料噴射
弁λにはエアータンク3のみから加圧空気が供給される
ととKなる。尚、燃料噴射弁2への空気供給によってエ
アータンク3内の圧力が設定値より降下した場合には、
圧力スイッチ/2がONとなり充気用圧縮機グによって
エアータンク3必;充気される。尚、エアータンク3内
の空気圧が設定値に達した場合(即ち、充気完了時)に
社、圧力スイッチ/2がONとなって充気用圧縮機グの
運転が停止される。
For this reason, the pressure valve 1/1 is kept in the ON state, and the electromagnetic switching valve A is opened and the pressurized air stored in the air tank 3 passes through the second air path 2.2. Fuel injection valve! Supplied on the side. In this case, the constant differential pressure valve 7 is set so that the air pressure flowing out from the constant differential pressure valve 7 is higher than the discharge pressure of the compressor by a constant pressure, so the first check valve /j is in the closed state. If the fuel injection valve λ is maintained as it is and pressurized air is supplied only from the air tank 3, the value becomes K. Furthermore, if the pressure inside the air tank 3 drops below the set value due to the air supply to the fuel injection valve 2,
The pressure switch 2 is turned on and the air tank 3 is filled with air by the filling compressor. Incidentally, when the air pressure in the air tank 3 reaches a set value (that is, when filling is completed), the pressure switch 2 is turned on and the operation of the filling compressor is stopped.

エンジンが始動して圧縮機/の吐出圧が設定圧に達する
と、圧カスイツヂlI−/がOFFになり、電磁切換非
Aが閉弁されてエアータンク3からの空気供給が遮断さ
iすると同時圧、今度は圧縮機/から第1逆止弁/jを
介して加圧空気が燃料噴射弁コに供給される。即ち、空
気供給源がエアータンク3から圧縮機/に切換わる。
When the engine starts and the discharge pressure of the compressor reaches the set pressure, the pressure switch I-/ turns OFF, the electromagnetic switch A closes, and the air supply from the air tank 3 is cut off. Pressurized air, in turn from the compressor/, is supplied to the fuel injection valve via the first check valve/j. That is, the air supply source is switched from the air tank 3 to the compressor.

一方、エンジンが定常運転に移行した後には、主スィッ
チ/θがOF Fとされているため、電磁切換非Aは圧
縮機/の吐出圧に関係なく閉弁状態のまま保持され圧縮
機/からの加圧空気が連続的に燃料噴射弁Jに供給され
る。尚、仁の場合、エアータンク3は、8L2逆止弁/
6を介してバイパス路、23から流入する圧縮機/の吐
出空気によって充気される。このように、エンジン始動
後にエアータンク3を圧縮機/の吐出空気によって充気
しておくと、エンジiン、、再起動時に燃料噴・射弁λ
に対して圧縮機/の吐出圧に相当する圧力の加圧空気を
エアータンク3かも迅速に供給してエンジンの始動を容
易且つ迅速ならしめることができる。
On the other hand, after the engine has transitioned to steady operation, the main switch /θ is turned OFF, so the electromagnetic switching switch A remains closed regardless of the discharge pressure of the compressor. of pressurized air is continuously supplied to the fuel injection valve J. In addition, in the case of Jin, the air tank 3 has an 8L2 check valve/
It is charged with discharge air of the compressor/compressor which enters from bypass line 23 via 6. In this way, if the air tank 3 is filled with air discharged from the compressor after the engine is started, the fuel injection valve λ will be activated when the engine is restarted.
The air tank 3 also quickly supplies pressurized air at a pressure corresponding to the discharge pressure of the compressor, thereby making it possible to start the engine easily and quickly.

又、図示実施例の場合には非常に高温となる第1空気路
、27側に耐熱、耐圧性に優れた逆止弁/jを配設し、
この逆止弁/jより空気下流側に接続シれたエアータン
ク3からの第2空気路2.2中に電磁切換弁を及び定差
圧弁7を設けているため、該電磁切換非Aあるいけ定差
圧弁7が直接圧縮機/からの高温空気に晒されることが
なく、従来の燃料噴射装置の如く電磁切換弁が温度上昇
によシ作動不良となって空気供給源の切換操作に支障を
きたすというようなトラブルの発生を未然に防市する仁
とができる。
In addition, in the case of the illustrated embodiment, a check valve /j with excellent heat resistance and pressure resistance is provided on the first air path 27 side, which becomes extremely high temperature.
Since the electromagnetic switching valve and the constant differential pressure valve 7 are provided in the second air passage 2.2 from the air tank 3 connected to the air downstream side of this check valve /j, the electromagnetic switching valve is not A. The fixed differential pressure valve 7 is not directly exposed to high-temperature air from the compressor, and unlike conventional fuel injection systems, the electromagnetic switching valve malfunctions due to temperature rise, which interferes with the switching operation of the air supply source. It is possible to prevent such troubles from occurring before they occur.

上述の如く、この第1実施例の燃料噴射装置Z。As mentioned above, the fuel injection device Z of this first embodiment.

け、圧縮機/の吐出圧の低いエンジン始動時Kiiエア
ータンク3から燃料噴射弁ノに加圧空気を供給するが、
エンジンが始動し圧縮機/の吐出圧力が設定圧以上に達
した場合にはエアータンク3からの空気供給を遮断して
圧縮機/から燃料噴射弁λに加圧空気な供給するよう罠
なっている。又、この実施例においては1、空気供給源
の切換えを圧縮機/の吐出圧によって制御するようにな
っているO 次に、第1図に示す本発明第!実施例の燃料噴射装置Z
、を説明すると、この第2実施例の燃料噴射装置2.は
、前記第7実施例の燃料噴射装置Fjt、Z、とほぼ同
一の基本構成を有するが、ただ電磁切換弁2の制御方法
のみが、第1実施例の場合と相違している。即ち、第1
実、流側の燃料噴射装flZ、においては電磁切換非A
を圧縮機/の吐出圧によって制御するようになっている
が、この第2実施例の燃料噴射装置Z管の場合には圧縮
機/の吐出圧がエンジンの回転数にほぼ比例するという
ことに着目し、電磁切換非Aの制御回路Y中に、エンジ
ンの回転数を検知する回転数センサー37から発信され
る電気的信号によって開閉制御される電磁スイッチグ2
を設けて電磁切換弁tをエンジンの回転数に応じて開閉
制御するようにしている。この場合、エンジンの回転数
が、例えば定格回転数の40〜70%に達した時点で電
磁切換弁tを閉弁して空気供給源をエアータンク3側か
ら圧縮機/側に切換えるようにする。  。
However, when starting the engine when the discharge pressure of the compressor is low, pressurized air is supplied from the Kii air tank 3 to the fuel injection valve.
When the engine starts and the discharge pressure of the compressor reaches the set pressure or higher, the air supply from the air tank 3 is cut off and pressurized air is supplied from the compressor to the fuel injection valve λ. There is. In addition, in this embodiment, 1. switching of the air supply source is controlled by the discharge pressure of the compressor; Example fuel injection device Z
To explain, the fuel injection device 2 of this second embodiment. This has almost the same basic configuration as the fuel injection device Fjt, Z of the seventh embodiment, but differs from the first embodiment only in the control method of the electromagnetic switching valve 2. That is, the first
In fact, in the upstream fuel injection system flZ, the electromagnetic switching non-A
is controlled by the discharge pressure of the compressor, but in the case of the Z-pipe of the fuel injection device of this second embodiment, the discharge pressure of the compressor is approximately proportional to the engine speed. Focusing on the control circuit Y of the electromagnetic switching non-A, an electromagnetic switching device 2 whose opening and closing are controlled by an electrical signal transmitted from a rotation speed sensor 37 that detects the engine rotation speed is used.
is provided to control the opening and closing of the electromagnetic switching valve t according to the engine speed. In this case, when the engine speed reaches, for example, 40 to 70% of the rated speed, the electromagnetic switching valve t is closed to switch the air supply source from the air tank 3 side to the compressor/side. . .

この第2実施例の如く電磁切換非Aをエンジンの回転数
に応じて開閉制御するようにした場合には、前記第7実
施例の如く電磁切換弁制御用のエアー配管(第1図にお
いて符号、2j)を設ける必要がなくなり、それだけ装
置の簡略化を促進せしめることができる。
When the electromagnetic switching valve A is controlled to open and close according to the engine speed as in the second embodiment, the air piping for controlling the electromagnetic switching valve (reference numeral in FIG. 1) is used as in the seventh embodiment. , 2j) is no longer necessary, and the simplification of the device can be promoted accordingly.

第3図に示す本発明第3実施例の燃料噴射装置2、は、
電磁切換非Aの開閉制御を該電磁切換非Aの制御回路に
設けた遅延スイッチ弘3によって行うようにしたところ
が前記第1害施例の燃料噴射装置2.の場合と異なるだ
けで他の基本構成は全て第1実施例の場合と同様とされ
ている。即ち、この実施例の燃料噴射装置2.は、エン
ジンのスタータ(図示省略)を停止させた後、所定時間
後に遅延スイッチ弘3をOFFにして電磁切換弁6を閉
弁するようになっている。このように電磁切換弁6を遅
延スイッチ弘3で一制御するようにした場合にも、前記
第2実施例の場合と同様に電磁切換弁6を制御するため
のエアー配管を要しない分だけ前記第1実施例の場合よ
りも装置の簡略化を促進亡しめることができる。
The fuel injection device 2 according to the third embodiment of the present invention shown in FIG.
In the fuel injection device 2 of the first embodiment, the opening/closing control of the electromagnetic switching non-A is performed by a delay switch 3 provided in the control circuit of the electromagnetic switching non-A. The only difference is that all other basic configurations are the same as in the first embodiment. That is, the fuel injection device 2 of this embodiment. After stopping the engine starter (not shown), the delay switch 3 is turned off and the electromagnetic switching valve 6 is closed after a predetermined period of time. Even when the electromagnetic switching valve 6 is controlled by the delay switch 3 in this way, as in the case of the second embodiment, the air piping for controlling the electromagnetic switching valve 6 is not required. The device can be simplified more easily than in the first embodiment.

又、第V図に示す本発明第1実施例の燃料噴射装置z6
は、前記各実施例の場合と同様の基本構成を有するが、
電磁切換非Aの制御方法は前記各実施例の場合と相違し
ている。即ち、この燃料噴射装置z4は、電磁切換非A
の制御回路Y中に、燃料ポンプjから燃料噴射弁λに圧
送される燃料圧によって作動する圧カス°イツチI1.
弘を設け、該燃料ポンプjの吐出圧が、燃料噴射弁から
の噴霧が充分に発達すると考えられる燃料圧に達した時
点で該制御回路Yを開いて電磁切換弁6を閉弁するよう
になっている。
Moreover, the fuel injection device z6 of the first embodiment of the present invention shown in FIG.
has the same basic configuration as in each of the above embodiments, but
The control method for the electromagnetic switching non-A is different from that of the previous embodiments. That is, this fuel injection device z4 is an electromagnetic switching non-A
In the control circuit Y of the control circuit Y, a pressure switch I1.
The control circuit Y is opened and the electromagnetic switching valve 6 is closed when the discharge pressure of the fuel pump J reaches a fuel pressure at which spray from the fuel injection valve is considered to be sufficiently developed. It has become.

次に、本発明の詳細な説明すると、本発明の加圧空気式
燃料噴射装置は、燃料噴射弁に対する加圧空気供給源を
エンジンの運転状態に応じて切換制御するための切換装
置のひとつの構成部材として耐熱、耐圧性に優れた逆止
弁を使用し、この逆止弁によって切換装置の他の構成部
材である制御弁あるいけ定差圧弁が直接圧縮機からの高
温空気に晒享れてその作動特性が悪化するのを未然に防
止しイrするようにしているため、切換装置として作用
する電磁切換弁を直接圧縮機からの空気路中に設けた従
来の・燃料噴射装置の如く温度上昇によって電磁切換弁
の作動が不俯実とガり空気供給源の切換操作に支障をき
たすというよう々ことがなくなり、燃料の噴射特性及び
燃焼特性全向上せしめることができるという実用的効果
がある。
Next, to explain the present invention in detail, the pressurized air fuel injection device of the present invention is one of the switching devices for switching and controlling the pressurized air supply source to the fuel injection valve according to the operating state of the engine. A check valve with excellent heat and pressure resistance is used as a component, and this check valve allows the other components of the switching device, such as the control valve or differential pressure valve, to be directly exposed to the high temperature air from the compressor. In order to prevent the deterioration of the operating characteristics of the fuel injection system, the electromagnetic switching valve that acts as a switching device is installed directly in the air path from the compressor, similar to the conventional fuel injection system. The practical effect is that the operation of the electromagnetic switching valve becomes unstable and garbled due to temperature rise, which interferes with the switching operation of the air supply source, and the fuel injection characteristics and combustion characteristics can be completely improved. be.

弘 図面の簡#Itカ説明 第1図は本発明第1実施例に係る燃料噴射装置の基本構
成図、第2図は第1実施例に係る燃料噴射装置の基本構
成図、第3図は本発明第3実施例に係る燃料噴射装置の
基本構成図、第を図は第V実施例に係る燃料噴射装置の
基本構成図である。
Hiroshi Simple Explanation of Drawings Fig. 1 is a basic configuration diagram of a fuel injection device according to a first embodiment of the present invention, Fig. 2 is a basic configuration diagram of a fuel injection device according to a first embodiment, and Fig. 3 is a basic configuration diagram of a fuel injection device according to a first embodiment of the present invention. A basic configuration diagram of a fuel injection device according to a third embodiment of the present invention, and the second figure is a basic configuration diagram of a fuel injection device according to a Vth embodiment.

/   ・ ・・ 圧  縮  機 コ ・・・燃料噴射弁 3  ・自 エアータンク A ・・・制 御 弁 7 ・・・定差圧弁 /j ・・・逆止 弁 、2/  ・・・ 第1空気路 2.2  ・・・ 第2空気路 9′31 第2図/   ・ ・・ Compression Machine K...Fuel injection valve 3. Own air tank A...Control valve 7... Constant differential pressure valve /j...Check valve , 2/... First air path 2.2...Second air path 9'31 Figure 2

Claims (1)

【特許請求の範囲】 /、加圧空気忙よって燃料を霧化して噴射するようにし
た空気式燃料噴射弁(,2)とエンジン忙よって駆動さ
れる圧縮機(1)を、その途中に前記燃料噴射弁(,2
) 11111から前記圧縮機(1)側への空気の逆流
を防止する如く作用する逆止弁(/j)接 を介在せしめた第7空気路(2/)を介して続続すると
ともに、該第1空気路(−2))の前記逆止弁(/j)
よシ空気下流側位置に第2空気路(,2,2)を介して
エアータンク(3)を接続し、さらK。 前記第2空気路(,2−2)にはエンジンの運転状態に
応じて該第、2吻気路(,2,2)を適宜に開閉制御す
る制御弁(1,>と前記第2空気路(,2,2)を通っ
て前記第1空気路(,2/ )側圧供給される前記エア
ータンク(3)からの空気圧を前記圧縮機(1)の吐出
圧よυ一定圧力だけ高圧に設定する如く作用する定差圧
弁(7)を介在きしめたことを特徴とする加圧空気式燃
料噴射装置。
[Scope of Claims] / A pneumatic fuel injection valve (2) which atomizes and injects fuel using pressurized air and a compressor (1) driven by an engine are installed in the middle thereof. Fuel injection valve (,2
) 11111 to the compressor (1) side via a seventh air passage (2/) interposed with a check valve (/j) that acts to prevent air from flowing back into the compressor (1) side, and 1 air passage (-2)) said check valve (/j)
Connect the air tank (3) to the downstream side of the air tank via the second air path (2, 2), and then proceed further. The second air passage (, 2-2) is provided with a control valve (1,>) that controls opening and closing of the second proboscis air passage (, 2, 2) as appropriate depending on the operating state of the engine. The air pressure from the air tank (3) supplied to the first air passage (, 2/ ) through the passage (, 2, 2) is made higher than the discharge pressure of the compressor (1) by a constant pressure A pressurized air fuel injection device characterized in that a constant differential pressure valve (7) is interposed and acts as a setting.
JP10361582A 1982-06-15 1982-06-15 Pressurized air system fuel injector Pending JPS58220960A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10361582A JPS58220960A (en) 1982-06-15 1982-06-15 Pressurized air system fuel injector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10361582A JPS58220960A (en) 1982-06-15 1982-06-15 Pressurized air system fuel injector

Publications (1)

Publication Number Publication Date
JPS58220960A true JPS58220960A (en) 1983-12-22

Family

ID=14358674

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10361582A Pending JPS58220960A (en) 1982-06-15 1982-06-15 Pressurized air system fuel injector

Country Status (1)

Country Link
JP (1) JPS58220960A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61112772A (en) * 1984-07-25 1986-05-30 オ−ビタル、エンジン、カンパニ−、プロプライエタリ、リミテツド Air feeder to fuel injection system
JPH01182529A (en) * 1988-01-13 1989-07-20 Hitachi Ltd Controlling method and device for atomizing air of gas turbine
US5255658A (en) * 1990-10-12 1993-10-26 Coltec Industries Inc. System and apparatus to improve atomization of injected fuel

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61112772A (en) * 1984-07-25 1986-05-30 オ−ビタル、エンジン、カンパニ−、プロプライエタリ、リミテツド Air feeder to fuel injection system
JPH01182529A (en) * 1988-01-13 1989-07-20 Hitachi Ltd Controlling method and device for atomizing air of gas turbine
US5255658A (en) * 1990-10-12 1993-10-26 Coltec Industries Inc. System and apparatus to improve atomization of injected fuel

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