Device for aspiration of lubricating oil from the supply of a combustion engine

A device for aspiration of lubricating oil from the supply of a combustion engine that may at times be moved out of a normal position into a different position, in particular an upside-down position, by means of a lubricant pump delivering the oil to the bearing surfaces of the engine.

BACKGROUND OF THE INVENTION 
Devices have been provided in combustion engines serving, for example, as 
power plants of aircraft, in order to maintain supply of lubricant to the 
engine when the attitude of the aircraft varies, and especially in 
upside-down attitudes. 
There is a known system of maintaining dependable lubricant supply in which 
a plurality of oil pumps are arranged in the engine, with the oil to be 
delivered by that pump whose point of intake is immersed in the oil 
supply, being according to the tilt of the engine. This pump must then 
first deliver the oil to a reservoir to which another oil pump is 
connected, which finally delivers the oil to the lubricating circuit of 
the engine. In this known arrangement, however, the multiplicity of oil 
pumps required entails added cost. Besides, much space is required to 
accomodate the pumps, and the system is costly and trouble-prone owing to 
its complicated structure. 
There is another known system in which at least one pivoted pendulum member 
in at least one special housing is provided, having a point of intake that 
will be immersed in the oil by gravity in every attitude of the engine to 
thus maintain the lubricant supply. While this arrangement requires only 
one oil pump, the rigging of the pendulum member likewise calls for a 
comparatively large structural and spatialoutlay, involving added cost. 
The systems mentioned moreover require additional precautions to prevent 
aspiration of air into the oil line. 
Apart from these various systems, however, it is found in practice that the 
lubricating oil present in aviation combustion engines is always acted 
upon centrifugal force in most unusual flight attitudes, with the 
exception of the upside-down attitude; even, that is in steep banks and 
oblique attitudes as well as in helical maneuvers. This means that the oil 
supply, ordinarily contained in a lower storage tank is subject to such 
minor fluctuations that the lubricant supply to such an engine is safely 
maintained in the said flight attitude. The gravitational force acting on 
the lubricant is not much modified unless the engine remains in 
upside-down position with sustained deceleration, as is possible in stunt 
flying for example. For such a rare and extreme case, the known devices 
are too elaborate and costly in design. 
SUMMARY OF THE INVENTION 
The object of the invention is to maintain the lubricant supply of an 
internal combustion engine in simple manner and with little outlay, even 
in an upside-down position. 
This object is accomplished according to the invention by providing at 
least two supply tanks one of which is intended to hold the oil supply in 
the normal attitude and the other is intended to hold the oil supply in a 
different attitude of the engine. These tanks are capable of being 
connected to the suction side of the oil pump by way of one return line 
each, with a valve responding to gravity being provided, which in one 
attitude of the engine brings the return like of the tank associated with 
the attitude into communication with the suction side of the pump and 
shuts off the return line of the other pump. 
Through this arrangement, a constant connection can be maintained between 
the lubricant pump and the oil supply, while the valve, which like the oil 
itself is acted upon by gravity and any centrifugal forces, automatically 
establishes a connection with one of the tanks according to the attitude 
of the engine, while the connection to the other tank can be shut off 
against any aspiration of air. 
The one tank, accomodating the supply in the normal attitude, may be 
arranged beneath the engine, and the other tank on the opposed side above 
the engine, and the valve may be arranged between the suction side of the 
oil pump on the one hand and the two return lines connected to the tanks 
on the other hand. Such an arrangement has the advantage that with 
comparatively small structural outlay and space requirements, the system 
will maintain the lubricant supply to the engine even in an upside-down 
position. 
The valve may consist of a slide arranged in a housing and displaceable by 
gravity between two operating positions, and at right angles to the 
longitudinal axis of the engine. In the housing, a first port communicates 
with the return line of the bottom tank, a second port communicates with 
the return line of the top tank. A third opening communicates with the 
suction side of the oil pump and may be so arranged that in the first 
operating position, corresponding to a normal attitude, the first port is 
connected with the third while the second port is closed off by the slide, 
and in the second operating position corresponding to an upside-down 
attitude the second port is connected with the third while the first port 
is closed off by the slide. By this arrangement, the proper connection 
between the two tanks and the pump can be simply and dependably controlled 
according to the attitude of the engine. 
Specifically, the valve may be constructed with the slide cylindrical and 
arranged in a cylindrical bore of the housing, with the first and second 
ports being in the wall of the cylindrical bore and the third port in the 
end of the cylindrical bore. The slide is provided with a longitudinal 
bore and lateral passage slits connecting the outer surface of the slide 
with the longitudinal bore. These slits enable a connection to be made 
either between the third and first or between the third and second ports. 
Examplary embodiments of the invention as well as other details and 
features will be further described in the following with reference to the 
drawings.

DETAILED DESCRIPTION 
Reference is made initially to FIG. 1 schematically showing the general 
arrangement of the device in accordance with this invention in a 
combustion engine 1 employed as the power plant of an aircraft. For this 
purpose, a reducing gear 2 is flanged to one end of the engine 1 to drive 
a propeller 3, only a portion of which is shown. To lubricate the engine 1 
an oil pump 4 is provided. Underneath the engine 1 a tank 5 is arranged to 
hold the oil supply in the normal attitude, and above the engine 1 on the 
opposed side another tank 6 is arranged to hold the oil supply in the 
inverted attitude of the engine, the top tank 6 consisting, for example, 
of a valve cover. In the bottom tank 5 and from intake 7 a return line 8 
leads to a valve 11 as does a return line 10 from intake 9. The two lines 
8 and 10 may be connected to the suction line 12 of the oil pump 4 by 
means of valve 11. the valve 11 is designed to respond to gravity and in 
the position shown corresponding to a normal attitude, it connects the 
suction line 12 of pump 4 by way of line 8 and intake 7 to the bottom tank 
5, while the line 10 of the top tank 6 is shut off. Thus, in this position 
the supply of oil is maintained from the tank 5 while aspiration of air 
from the top tank 6 is prevented. In an inverted position or upside-down 
attitude of the engine 1, the top tank 6 is lowermost, so that oil 
escaping from the points of lubrication of engine 1 will collect by 
gravity in tank 6. In this position, gravity acts on the valve 11, the 
suction line 12 of pump 4 is connected by way of line 10 and intake 9 to 
tank 6, while line 8 is closed to prevent air from being aspirated through 
said line 8, since in that case the suction line 7 is not immersed in oil. 
FIG. 2 shows a simplified representaton of a valve 11. It consists 
essentially of a cylindrical slide 13 arranged in a cylindrical bore 15 of 
a housing 14, displaceable lengthwise between two operating positions and 
perpendicular to the longitudinal axis 16 of the engine 1 as indicated in 
FIG. 1. In the wall of the cylindrical bore 15 is arranged a first port 17 
in the form of an annular groove to which return line 8 is connected, 
leading to the bottom tank 5 shown in FIG. 1. In the cylindrical bore 15 
and offset upwardly is a second port 18 likewise in the form of an annular 
groove, to which is connected the line 10 leading to the top tank 6. In 
the top end of bore 15, a third port 19 is provided, communicating with 
the suction line 12 leading to the pump 4. The slide 13 has a longitudinal 
bore 20 and lateral passage slits 21 connecting the outer surface of the 
slide 13 with the longitudinal bore 20. 
In the first operating position shown corresponding to a normal attitude, 
in which gravity acts in the direction indicated by the arrow S, the slide 
13 connects the first port 17 with the third port 19, while the second 
port 18 is shut off by the outer surface of the slide 13. This initially 
establishes a connection from line 8 to suction line 12 for passage of 
lubricant and secondly prevents aspiration of air from tank 6. 
As shown in FIG. 3 gravity S acts on the valve 11 in the opposed direction 
corresponding to the second operating position in upside-down attitude. 
The position of the housing 14 has been left to better illustrate the 
setting of the slide 13. In reaility, however, the port 19 of housing 14 
would point downward. In this position the slide 13 connects the second 
port 18 to the third port 19 while the outside surface of the slide 13 
shuts off the first port 17. Thus, the flow of lubricant from the other 
line 10 into the suction line 12 is released and air cannot be aspirated 
from tank 5. 
The valve 11' shown in FIG. 4 consists essentially of a cylindrical slide 
22 arranged longitudinally displaceable between two operating positions as 
in the embodiment of FIGS. 2 and 3 in a cylindrical bore 23 of a housing 
24. This valve 11' is likewise perpendicular to the longitudinal axis 16 
of the engine 1. In the wall of the cylindrical bore 23 a first port 17' 
is provided, to which is connected the line 8 of the bottom tank 5. To a 
second port 18' opening into the bore 23 is connected the return line 10 
for the top tank 6. Between ports 17' and 18' on the opposed side of the 
bore 23, a third port 19' is provided connected to the suction line 12 
leading to the pump 4. The slide 22 has an annular groove 25 by way of 
which in the first operation position shown, corresponding to a normal 
attitude the first port 17' is connected with the third port 19', 
permitting flow of lubricant from the line 8 of the bottom tank 5 through 
valve 11' to the suction line 12 of pump 4. On the other hand, the port 18 
is shielded by the outer surface of slide 22 against any aspiration of air 
from the top tank 6. 
In the valve 11' of FIG. 4 as shown in FIG. 5, gravity S acts in the 
opposed direction, bringing the slide 22 into its second operating 
position corresponding to the inverted attitude of the engine. As a result 
the annular groove 25 and ports 18' and 19' establish a connection between 
the line 10 of the top tank 6 and the suction line 12 of pump 4, while 
port 17' is shut off against any aspiration of air by the outer surface of 
slide 22. The axial equalizing passage 26 in slide 22 serves the purpose 
of permitting exchange of medium present above and below slide 22 to 
ensure ease of travel of slide 22 in the bore 23. 
FIG. 6 shows a preferred embodiment of valve 11 performing the function of 
the valve of FIGS. 2 and 3 and accordingly bears the same reference 
numerals. This embodiment is distinguished by a compact, space-saving 
construction, the intake 7 and line 8 having been incorporated in the 
housing 14. The line 10 leading to the top tank 6 passes out of the bottom 
tank 5 through a stuffing box 27. The bore 15 is closed off at the bottom 
by a cover 28 with inclusion of an oil screen 29 for the intake 7. The 
slide 13 is provided on both faces 13a with small elevations 30 preventing 
direct contact and consequent adhesion to the ends of bore 15. Also, the 
distance between the annular grooves of ports 17 and 18 is greater than 
the width of the passage slit 21 to ensure ease of travel of slide 13 in 
bore 15. Due to the geometry of the ports and slit, flow from one tank is 
positively shut off so long as there is a connection with the other tank 
via lines 8 or 10. 
Thus, the several aforenoted objects and advantages are most effectively 
attained. Although several somewhat preferred embodiments have been 
disclosed and described in detail herein, it should be understood that 
this invention is in no sense limited thereby and its scope is to be 
determined by that of the appended claims.