JPS59173549A - Device for preventing fuel vapor from scattering - Google Patents

Device for preventing fuel vapor from scattering

Info

Publication number
JPS59173549A
JPS59173549A JP4786883A JP4786883A JPS59173549A JP S59173549 A JPS59173549 A JP S59173549A JP 4786883 A JP4786883 A JP 4786883A JP 4786883 A JP4786883 A JP 4786883A JP S59173549 A JPS59173549 A JP S59173549A
Authority
JP
Japan
Prior art keywords
fuel
fuel vapor
space
tank
vapor
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
JP4786883A
Other languages
Japanese (ja)
Inventor
Shigenori Sakurai
桜井 茂徳
Mikio Murachi
村知 幹夫
Yoshihiro Shikame
鹿目 義弘
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.)
Toyota Motor Corp
Original Assignee
Toyota Motor 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 Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP4786883A priority Critical patent/JPS59173549A/en
Publication of JPS59173549A publication Critical patent/JPS59173549A/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
    • F02M25/00Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture
    • F02M25/08Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture adding fuel vapours drawn from engine fuel reservoir
    • F02M25/0854Details of the absorption canister
    • 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
    • F02M25/00Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture
    • F02M25/08Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture adding fuel vapours drawn from engine fuel reservoir
    • F02M2025/0863Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture adding fuel vapours drawn from engine fuel reservoir with means dealing with condensed fuel or water, e.g. having a liquid trap

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Abstract

PURPOSE:To prevent fuel vapor from scattering into the atmosphere, and as well to enhance the power performance of an engine, by disposing a gas separating membrane parting between a fuel vapor introducing space into which fuel vapor from a fuel tank is introduced and an atmospheric space so that condensed fuel is returned into the tank. CONSTITUTION:During rest of an engine fuel vapor generated in fuel tank 1 is introduced into a fuel vapor introduction space 14 in a fuel vapor separating container 3 from a inlet port 4 by way of a vapor passage 2. Then air permeates a gas separating membrane 26 in a gas separating part 12 and enters into an atmospheric space, accompanied with increase in the pressure of the above-mentioned space 14. At this time fuel vapor is inhibited from permeating the gas separating membrane 26, and therefore, is pooled in this space 14. Fuel vapor in the space 14 is finally condensed, and is pooled in a fuel pooling section 18. When the engine is operated so that gas pressure within a gas space in the tank 1 lowers resulting in that a pressure differential across a check valve 8 reaches a predetermined value, the check valve 8 opens so that fuel in a fuel pooling section 18 is returned to the tank 1 through a return passage 5 due to negative pressure of the tank 1.

Description

【発明の詳細な説明】 本発明は、機関の停止中に自動車の燃料タンクにおいて
発生する燃料蒸気が大気へ発散することを防止する燃料
蒸気発散防止装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a fuel vapor emission prevention device that prevents fuel vapor generated in a fuel tank of an automobile from escaping into the atmosphere while the engine is stopped.

周知の燃料蒸気発散防止装置では、機関の停止中に燃料
タンクにおいて発生する燃料蒸気を活性炭に吸着させ、
次の機関運転時に燃料蒸気を活性炭から脱離して吸気通
路へ放出し、燃焼室において燃焼させている。この場合
、燃料成分が吸気系へ戻されているために空燃比が変動
するとともに混合気が過濃となり、空燃比制御精度の悪
化、排気中の有害成分量の増大、失火による動力性能の
低下等の不具合の原因になる。
In the well-known fuel vapor emission prevention device, activated carbon adsorbs fuel vapor generated in the fuel tank while the engine is stopped.
During the next engine operation, fuel vapor is desorbed from the activated carbon, released into the intake passage, and burned in the combustion chamber. In this case, since the fuel components are returned to the intake system, the air-fuel ratio fluctuates and the air-fuel mixture becomes overrich, resulting in deterioration of air-fuel ratio control accuracy, increase in the amount of harmful components in the exhaust, and reduction in power performance due to misfire. This may cause other problems.

本発明の目的は、吸気通路への燃料蒸気の放出に因る不
具合を防止することができる燃料蒸気発散防止装置を提
供することである。
An object of the present invention is to provide a fuel vapor diffusion prevention device that can prevent problems caused by the release of fuel vapor into an intake passage.

この目的を達成するために本発明の燃料、蒸気発散防止
装置は、燃料タンクからの燃料蒸気が導入される燃料蒸
気導入空間、大気空間と燃料蒸気導入空間の間を仕切る
ガス分灘膜、および燃料蒸気導入空間の下部にたまる凝
縮燃料を燃料タンクへ戻す戻し通路を備えている。
To achieve this objective, the fuel and vapor diffusion prevention device of the present invention includes a fuel vapor introduction space into which fuel vapor from a fuel tank is introduced, a gas partition membrane that partitions between the atmospheric space and the fuel vapor introduction space, and A return passage is provided for returning condensed fuel that accumulates at the bottom of the fuel vapor introduction space to the fuel tank.

こうして燃料蒸気はガス分離膜(酸素富化膜と呼ばれる
こともある。)を経ての通過を阻止されて燃料蒸気空間
に滞留し、やがて凝縮し、戻し通路を経て燃料タンクへ
回収される。したがって混合気の空燃比が燃料蒸気の放
出により乱されることは回避され、空燃比制御精度の悪
化、排気中の有害成分量の増大および動力性能の低下を
防止することができる。
The fuel vapor is thus prevented from passing through the gas separation membrane (sometimes referred to as an oxygen enrichment membrane) and remains in the fuel vapor space, where it eventually condenses and is recovered into the fuel tank via the return passage. Therefore, the air-fuel ratio of the air-fuel mixture is prevented from being disturbed by the release of fuel vapor, and it is possible to prevent deterioration of air-fuel ratio control accuracy, increase in the amount of harmful components in the exhaust gas, and deterioration of power performance.

本発明では吸着剤を省略することができる。In the present invention, the adsorbent can be omitted.

図面を参照して本発明の詳細な説明する。The present invention will be described in detail with reference to the drawings.

第1図において燃料タンク1の上部は、ベーパ通路2を
経て燃料蒸気分離容器3上部の入口4へ、および戻し通
路5を経て燃料蒸気分離容器3下部の出口6へ接続され
ている。ベーパ通路2および戻し通路5にはそれぞれ、
燃料タンクlから燃料蒸気分離容器3へ、および燃料蒸
気分離容器3から燃料タンク1へ順方向となるように逆
止弁7,8が設けられている。燃料蒸気分離容器3は下
部に大気口9を有している。
In FIG. 1, the upper part of the fuel tank 1 is connected through a vapor passage 2 to an inlet 4 at the upper part of the fuel vapor separation vessel 3, and through a return passage 5 to an outlet 6 at the lower part of the fuel vapor separation vessel 3. The vapor passage 2 and the return passage 5 each have
Check valves 7 and 8 are provided in a forward direction from the fuel tank l to the fuel vapor separation container 3 and from the fuel vapor separation container 3 to the fuel tank 1. The fuel vapor separation vessel 3 has an atmosphere port 9 at the bottom.

第2図は燃料蒸気分離容器3の内部を示している。ガス
分離膜部12は環状に延び、半径方向外側の燃料蒸気導
入空間14と半径方向内側の中心空間16との間を仕切
っている。入口4は燃料蒸気導入空間14へ接続され、
中心空間16は大気空間として大気口9を経て燃料蒸気
分離容器3の外部へ接続されている。燃料だまり18は
、燃料蒸気導入空間14の下部に設けられ、出口6へ接
続されている。なお燃料蒸気分離容器3の容積は燃料タ
ンクlの容積が例えば60Aであるものに対し41が適
当である。
FIG. 2 shows the inside of the fuel vapor separation vessel 3. The gas separation membrane section 12 extends annularly and partitions a radially outer fuel vapor introduction space 14 from a radially inner central space 16 . The inlet 4 is connected to a fuel vapor introduction space 14,
The central space 16 is connected as an atmospheric space to the outside of the fuel vapor separation vessel 3 via the atmospheric port 9. The fuel reservoir 18 is provided at the lower part of the fuel vapor introduction space 14 and is connected to the outlet 6. The capacity of the fuel vapor separation vessel 3 is suitably 41 when the capacity of the fuel tank 1 is, for example, 60A.

第3図はガス分離膜部12の垂直断面図である。FIG. 3 is a vertical sectional view of the gas separation membrane section 12.

セルロースろ紙とテフロン材から成るガス分離膜26と
が半径方向へ交互に積層されている。
Gas separation membranes 26 made of cellulose filter paper and Teflon material are alternately stacked in the radial direction.

本装置の作用を説明する。The operation of this device will be explained.

機関の停止中、燃料タンク1において発生しqし る。逆止弁7は圧力差が例えば300 Aqになると開
く。燃料蒸気導入空間14の圧力の増大に伴って空気は
ガス分離膜部12のガス分離膜26を通過して大気空間
へ至るが、燃料蒸気はガス分離膜26の通過を阻止され
、燃料蒸気導入空間14に滞留する。こうして燃料蒸気
はやがて凝縮し、燃料たまり18にたまる。
This occurs in the fuel tank 1 while the engine is stopped. The check valve 7 opens when the pressure difference reaches, for example, 300 Aq. As the pressure in the fuel vapor introduction space 14 increases, air passes through the gas separation membrane 26 of the gas separation membrane section 12 and reaches the atmospheric space, but the fuel vapor is blocked from passing through the gas separation membrane 26 and the fuel vapor is not introduced. It stays in the space 14. Thus, the fuel vapor eventually condenses and accumulates in the fuel reservoir 18.

機関の運転中は、燃料タンク1から吸気系への燃料の送
りに伴って燃料タンク1の気体空間の気体圧は低下する
。こうして逆止弁18における圧力差が200 mmA
4以上になると、逆止弁8が開いて燃料だまり18内の
燃料は、燃料タンク1の負圧により戻し通路5を経て燃
料タンクlへ回収される。
While the engine is operating, the gas pressure in the gas space of the fuel tank 1 decreases as fuel is sent from the fuel tank 1 to the intake system. In this way, the pressure difference at the check valve 18 is 200 mmA.
4 or more, the check valve 8 opens and the fuel in the fuel reservoir 18 is recovered to the fuel tank 1 via the return passage 5 due to the negative pressure in the fuel tank 1.

第4図は燃料蒸気分離容器3の他の実施例を示している
。ろ紙28.30が燃料蒸気導入空間14の上下にそれ
ぞれ設けられ、吸着剤としての活性炭32が燃料蒸気導
入空間14内に充てんされる。この実施例では、燃料蒸
気のうち重い成分が活性炭32により吸着され、軽い成
分はガス分層膜部12により空気から分離され、次の機
関運転時に凝縮燃料および脱離した燃料蒸気は負圧によ
り吸引されて戻し通路5を経て燃料タンク1へ戻される
。活性炭32による吸着を免れ易い燃料蒸気成分がガス
分離膜部12により大気への放出を防止されるので、大
気空間への燃料蒸気の発散を確実に防□止することがで
きる。
FIG. 4 shows another embodiment of the fuel vapor separation vessel 3. In FIG. Filter papers 28 and 30 are provided above and below the fuel vapor introduction space 14, respectively, and the fuel vapor introduction space 14 is filled with activated carbon 32 as an adsorbent. In this embodiment, the heavy components of the fuel vapor are adsorbed by the activated carbon 32, the light components are separated from the air by the gas separation membrane section 12, and the condensed fuel and desorbed fuel vapor are removed by negative pressure during the next engine operation. It is sucked in and returned to the fuel tank 1 via the return passage 5. Since fuel vapor components that tend to escape adsorption by the activated carbon 32 are prevented from being released into the atmosphere by the gas separation membrane section 12, it is possible to reliably prevent fuel vapor from dispersing into the atmosphere.

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

第1図は本発明の実施例の全体の構成図、第2図は燃料
蒸気分離容器の内部の構造図、第3図は燃料蒸気分脈容
器内のガス分離膜部の構成を示す図、第4図は燃料蒸気
分離容器の他の構造例を示す図である。 1・・・燃料タンク、5・・・戻し通路、14・・・燃
料蒸気導入空間、26・・・ガス分離膜。 第1図 第2図 4 第4図
FIG. 1 is an overall configuration diagram of an embodiment of the present invention, FIG. 2 is an internal structural diagram of a fuel vapor separation vessel, FIG. 3 is a diagram showing the configuration of a gas separation membrane section in a fuel vapor separation vessel, and FIG. FIG. 4 is a diagram showing another example of the structure of the fuel vapor separation vessel. DESCRIPTION OF SYMBOLS 1... Fuel tank, 5... Return passage, 14... Fuel vapor introduction space, 26... Gas separation membrane. Figure 1 Figure 2 Figure 4 Figure 4

Claims (1)

【特許請求の範囲】[Claims] a料タンクからの燃料蒸気が導入される燃料蒸気導入空
間、大気空間と燃料蒸気導入空間の間を仕切るガス分即
1膜、および燃料蒸気導入空間の下部にたまる凝縮燃料
を燃料タンクへ戻す戻し通路を備えていることを特徴と
する、燃料蒸気発散防止装置。
A fuel vapor introduction space into which fuel vapor from the fuel vapor tank is introduced, a gas membrane that partitions the atmospheric space and the fuel vapor introduction space, and a return for returning condensed fuel that accumulates at the bottom of the fuel vapor introduction space to the fuel tank. A fuel vapor diffusion prevention device characterized by comprising a passage.
JP4786883A 1983-03-24 1983-03-24 Device for preventing fuel vapor from scattering Pending JPS59173549A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4786883A JPS59173549A (en) 1983-03-24 1983-03-24 Device for preventing fuel vapor from scattering

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4786883A JPS59173549A (en) 1983-03-24 1983-03-24 Device for preventing fuel vapor from scattering

Publications (1)

Publication Number Publication Date
JPS59173549A true JPS59173549A (en) 1984-10-01

Family

ID=12787350

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4786883A Pending JPS59173549A (en) 1983-03-24 1983-03-24 Device for preventing fuel vapor from scattering

Country Status (1)

Country Link
JP (1) JPS59173549A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7413824B2 (en) 2000-01-18 2008-08-19 Tel Aviv University Future Technology Development L.P. Direct oxidation fuel cell with a divided fuel tank having a movable barrier pressurized by anode effluent gas

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7413824B2 (en) 2000-01-18 2008-08-19 Tel Aviv University Future Technology Development L.P. Direct oxidation fuel cell with a divided fuel tank having a movable barrier pressurized by anode effluent gas
US8092955B2 (en) 2000-01-18 2012-01-10 Tel-Aviv Univrsity Future Technology Development L.P. Fuel cell having fuel tank directly attached to anode allowing pump-free fuel delivery

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