GB2093120A - Temperature responsive air induction apparatus - Google Patents
Temperature responsive air induction apparatus Download PDFInfo
- Publication number
- GB2093120A GB2093120A GB8204411A GB8204411A GB2093120A GB 2093120 A GB2093120 A GB 2093120A GB 8204411 A GB8204411 A GB 8204411A GB 8204411 A GB8204411 A GB 8204411A GB 2093120 A GB2093120 A GB 2093120A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- temperature
- flap
- induction apparatus
- temperature responsive
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M31/00—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture
- F02M31/02—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating
- F02M31/04—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating combustion-air or fuel-air mixture
- F02M31/06—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating combustion-air or fuel-air mixture by hot gases, e.g. by mixing cold and hot air
- F02M31/062—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating combustion-air or fuel-air mixture by hot gases, e.g. by mixing cold and hot air with thermostat and pneumatic actuator both working on the air mixture control valve
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Temperature-Responsive Valves (AREA)
Abstract
The temperature of air flow into a carburettor is controlled by a flap (4), Fig. 1 (not shown) to meter the amount of heated air which is mixed with cold air, the control thereof being by a temperature sensitive vacuum control element (6) and in order to prevent icing under full throttle low vacuum conditions a bimetal element 23 is arranged edge-on in the intake air flow path to prevent complete reclosure of the flap (4) for less than a predetermined intake air temperature. The bimetal element may be arranged upstream (Fig. 2) or downstream (not shown) of the flap (4) and may be formed so as to have a snap action at the predetermined temperature, Fig. 4 (not shown). <IMAGE>
Description
SPECIFICATION
Temperature responsive air induction apparatus
This invention relates to temperature responsive air induction apparatus especially for internal combustion engines.
The regulation of induction air temperatures to internal combustion engines is a widely used means of controlling exhaust gas emission and optimising the efficiency of combustion. In one known system, a temperature-sensitive valve operated by a bi-metal element controls a vacuum applied to a diaphragm device for controlling a flap valve which adjusts a mixture of cool air and air heated by exhaust manifold to obtain a predetermined mean air temperature to the filter and carburettor inlet of an internal combustion engine. As the temperature of air controlling the bi-metal element increases, the flap valve moves to permit a reduced quantity of heated air to the carburettor.
One problem with such an arrangement can be that the temperature sensitive element is one which normally controls a vacuum to control the flap, whereas with a normal carburettor at full throttle the available vacuum tends to disappear almost completely. The control flap therefore tends to close for full throttle openings thereby preventing the desired inflow of hot air and this can result in freezing within the carburettor in adverse conditions.
The object of the present invention is to reduce the above short-coming.
According to the invention there is provided a temperature responsive air induction apparatus comprising an air induction duct operable to conduct induction air from a source of relatively unheated air towards temperature sensitive means, said duct including a temperature dependent vacuum responsive air control member operable to adjust a way through for admission of relatively heated air for admixture with the unheated air and characterised by a bi-metal element arranged edge-on to the flow in the air flow path to act as a stop to prevent complete reclosure of the member across the way through for the heated air when the unheated air temperature is below a certain value.
If desired the bi-metal element may be a snapaction element.
In order that the invention may be more clearly understood, the same will be further described by way of example with reference to the accompanying drawings in which: Fig. 1 illustrates in diagrammatical form part of a known carburattor air induction system for an internal combustion engine,
Figs. 2 and 3 illustrates a modification of the apparatus of Fig. 1, in accordance with one embodiment of the invention,
Fig. 4 illustrates a snap-action element for use in accordance with a second embodiment.
Referring to Fig. 1, this shows a portion of an induction system for a carburettor of an internal combustion engine. The main flow path for air to the filter and subsequently to the carburettor is provided by a duct part of which is represented by reference 1 with an inflow end 2 and outflow end 3. The duct also includes a temperature-controlled pivotted flap 4 which in this prior art arrangement covers a hot air inlet passage 5, the flap 4 being controlled by a vacuum operable diaphragm 6 via a rod 7. The diaphragm 6 is normally biased to hold the flap 4 in the closed position by virtue of a spring 8 captive in a diaphragm chamber 9. The diaphragm chamber 9 has a port 10 which is connected by a typically flexible plastics suction tube represented by the dotted line 11 to a temperature sensitive bi-metal controlled vacuum valve unit 12.The unit 12 has a vacuum connection 1 3 for connection to a vacuum port on the carburettor of the engine and a vent port 1 4 the flow path to which is closeable by a temperature sensitive bi-metal valve 1 5.
In operation of this prior art arrangement, the temperature sensitive bi-metal valve 1 5 controls the vacuum applied to the vacuum chamber 9 which in turn controls the position of the pivotted flap 4 thereby adjusting the ratio of cool air entering via the port 2 and warm air entering via the passage 5 to obtain a predetermined mean air temperature at the carburettor inlet. With the temperature sensitive valve unit 12 located, as it normally is, within the air filter to the carburettor, the bi-metal valve opens when heated to allow a bleed of air from the vent 1 4 to thereby decrease the vacuum applied to the diaphragm chamber and the control flap therefore moves downward to reduce the flow of heated air and to increase the flow of unheated air.The temperature of air to the carburettor consequently tends to decrease and the bi-metal valve 1 5 when sensing such a decrease tends to move towards its seat to thereby increase the vacuum to the vacuum chamber 9 and lift the flap 4 to compensate for any undesired temperature decrease.
Under steady running conditions, an equilibrium condition for the flap 4 is therefore establishable TO maintain a predetermined mean carburettor input temperature. However, as foreshadowed above, a system such as that shown in Fig. 1 can have a disadvantage to the extent that at full throttle settings, the vacuum which is provided at the port 1 3 of the unit 12 can substantially disappear with the result that the flap 4 closes regardless of the temperature of air flowing to the carburettor. This can result in carburettor freezing and engine malfunction or failure.
Referring to Figs. 2 and 3, the latter being a view over section AA in Fig. 2, a detent 21 is attached to the pivotted flap 4 such as to be engageable with a bi-metal strip 23 when deflected towards it. As seen in Fig. 3, the bimetal strip 23 is mounted on the upper surface 24 of the input duct such that in the event of the temperature of air flowing through the duct 1 falling below a given level the bi-metal 23 deflects leftwards so that the end thereof is engageable with the upper service of the detent 21 when the flap 4 tends to move towards the closed position.
It is therefore seen that for a given predetermined
low temperature of air in the duct 1, the flap 4,
once having been open due to normal carburettor suction whilst moving towards a full throttle condition, cannot return to its fuliy closed position and thereby provides a predetermined waythrough for heated air in the event of the unheated air being at less than said predetermined temperature. If the incoming air temperature increases, the bi-metal strip is deflectable rightwards in Fig. 3, thereby permitting the flap 4 to reclose passage 5 under control of the bi-metal vacuum valve and the system operates in a normal manner for induction air temperature and exhaust emission control.
In the foregoing, the temperature sensitive means for ensuring a way-through for heated air in the event of incoming air tending to be less than a predetermined temperature, operates in response to the temperature of incoming air flowing past it.
This is regarded as the simplest way of achieving the desired result but the means for ensuring a predetermined way through may alternatively be controlled by means directly dependent upon the temperature of air flowing out of the end 3 of the duct. In other words, the control may be achieved by sensing unheated air temperature as a function of the temperature of air entering the carburettor.
In the arrangements described in the foregoing, adjustment of the position of the bi-metal strip 23 in relation to the detent 21 can be rather critical and for quantity production this is therefore something which may preferably be avoided.
Referring now to Fig. 4, this shows a bi-metal element formed with three limbs and arranged to give a snap-action. If the element 23 of Figs. 2 and 3 is replaced with the element of Fig. 4 it will switch with a snap action from a position which is clear of the detent 21 to a position where it is engaged by the detent 2 when the incoming air temperature falls below a set value.
The element of Fig. 4, comprises three distinct limbs 41, 42 and 43 joined at one end by a section 44 and at the other end by a section 45 with a mounting flange 46. The central limb 42 is bi-metal and has a curvature imparted to it by virtue of crimps 47 and 48 in limbs 41 and 43.
The curvature of limb 42 at below a critical temperature is in the same sense as the crimps as shown. However, at more normal temperatures the curvature is in the other sense.
If the element shown in Fig. 4 is substituted for the strip 23 of Figs. 2 and 3, because the amount of movement of the lower end section 44 at critical snap-over temperature is appreciable, positioning of this element is less critical than that of element 23.
Claims (6)
1. A temperature responsive air induction apparatus comprising an air induction duct operable to conduct induction air from a source of relatively unheated air towards temperature sensitive means, said duct including a temperature dependent vacuum responsive air control member operable to adjust a way through for admission of relatively heated air for admixture with the unheated air and characterised by a bi-metal element arranged edge-on to the flow in the air flow path to act as a stop to prevent complete reclosure of the member across the way-through for the heated air when the unheated air temperature is below a certain value.
2. A temperature responsive air induction apparatus as claimed in claim 1, characterised by the bi-metal element being located in the unheated air flow path upstream of the member.
3. A temperature responsive air induction apparatus as claimed in claim 1, characterised by the bi-metal element being located in the airflow path down-stream of the member.
4. A temperature responsive air induction apparatus as claimed in claims 1, 2 or 3 characterised in that the bi-metal element is a snap-action element.
5. Temperature responsive air induction apparatus as claimed in claims 1, 2, 3 or 4 characterised in that said member comprises a flap hinged at one end to move towards and away from the way through for heated air, said flap being provided with a detent extending backwards from the hinge of the flap for engagement with the bi-metal element.
6. Temperature responsive air induction apparatus substantially as described herein with reference to Figs. 1, 2 and 3 or Figs. 1, 2, 3 and 4 of the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8204411A GB2093120B (en) | 1981-02-17 | 1982-02-15 | Temperature responsive air induction apparatus |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8104995 | 1981-02-17 | ||
GB8204411A GB2093120B (en) | 1981-02-17 | 1982-02-15 | Temperature responsive air induction apparatus |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2093120A true GB2093120A (en) | 1982-08-25 |
GB2093120B GB2093120B (en) | 1985-04-17 |
Family
ID=26278476
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8204411A Expired GB2093120B (en) | 1981-02-17 | 1982-02-15 | Temperature responsive air induction apparatus |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2093120B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6327980B1 (en) * | 2000-02-29 | 2001-12-11 | General Electric Company | Locomotive engine inlet air apparatus and method of controlling inlet air temperature |
-
1982
- 1982-02-15 GB GB8204411A patent/GB2093120B/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6327980B1 (en) * | 2000-02-29 | 2001-12-11 | General Electric Company | Locomotive engine inlet air apparatus and method of controlling inlet air temperature |
Also Published As
Publication number | Publication date |
---|---|
GB2093120B (en) | 1985-04-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |