TECHNICAL FIELD
[0001] The present disclosure relates to a triple gear pump with floating bearings, which
uses rotating gears to pressurize and expel fluid, and in particular to a triple gear
pump stably operative not only in a series or parallel mode but also in an unloaded
mode.
BACKGROUND ART
[0002] A gear pump is generally provided with a pair of gears mutually in mesh and a housing
accommodating the gears and, by rotating the pair of gears in a flow path defined
by the housing, pressurizes and expels fluid therein. This is used as a fuel feeder
for a reciprocating engine or a jet engine or such.
[0003] A floating bearing is often used in a gear pump. In the gear pump with the floating
bearing, the bearing supports a gear shaft as well as slightly floats in the axial
direction to come in contact with a gear side face and support it. The fluid passing
through the gear pump serves for lubrication of the bearing as well as pressure application
to the bearing onto the gear side face.
[0004] A triple gear pump has been proposed, in which one drive shaft drives two gear pumps
simultaneously. The triple gear pump realizes a relatively small flow rate when these
two gear pumps are operated in a series mode and a relatively large flow rate when
operated in a parallel mode.
[0005] The patent literatures 1, 2 disclose related arts.
Citation List
Patent Literature
SUMMARY OF THE INVENTION
PROBLEM TO BE SOLVED
[0007] The floating bearing needs to be pressurized and, to assure smooth work and prevent
fluid leakage from the gear side face, the applied pressure should be managed within
a proper range. While the pressure of the fluid around the floating bearing is subject
to fluctuations depending on operation modes, however, technical difficulty would
increase if the number of operation modes were increased.
SOLUTION TO PROBLEM
[0008] The present disclosure relates to a triple gear pump that is capable of being stably
operative not only in a series or parallel mode but also in an unloaded mode.
[0009] According to an aspect, a triple gear pump with a drive gear and first and second
idler gear respectively in mesh with the drive gear so as to respectively constitute
first and second gear pumps for expelling fluid used as a fuel, is provided with:
a housing enclosing the first gear pump and the second gear pump; a drive shaft linked
to the drive gear so as to rotate unitarily with the drive gear and led out of the
housing; a drive-shaft bearing rotatably supporting the drive shaft and being axially
floatingly movable, the drive-shaft bearing receiving pressure applied by the fluid
so as to come in contact with the drive gear; a mechanical seal interposed between
the drive shaft and the housing to prevent the fluid from leaking out of the housing;
and a seal interposed between the drive-shaft bearing and the mechanical seal to prevent
the pressure of the fluid from being transmitted to the mechanical seal.
EFFECTS OF THE INVENTION
[0010] The disclosed art provides a triple gear pump that is capable of being stably operative
not only in a series or parallel mode but also in an unloaded mode.
BRIEF DESCRIPTION OF THE DRAWINGS
[0011]
FIG. 1 is a schematic block diagram of a system for feeding fuel to an engine of an
aircraft according to an embodiment.
FIG. 2 is a sectional plan view of a triple gear pump according to the embodiment.
FIG. 3 is a schematic cross-sectional view of the triple gear pump.
FIG. 4 is a sectional plan view mainly showing a floating bearing and its surroundings
in the triple gear pump in an enlarged view.
FIG. 5 is schematic block diagrams describing a series mode, a parallel mode and an
unloaded mode.
DESCRIPTION OF EMBODIMENTS
[0012] Certain embodiments will be described hereinafter with reference to the appended
drawings. Throughout the following description and the appended claims, the terms
"axial direction" and "around the axis" are defined and used with respect to each
shaft.
[0013] Referring to FIG. 1, a triple gear pump 1 according to the present embodiment is
to be incorporated in a system for feeding fuel to an engine 10 of an airplane and
then pressurizes and expels fluid such as oil with relatively low viscosity, namely
kerosine for example.
[0014] The fluid is supplied from a tank through a flow path F
1 and is pressurized and expelled by the triple gear pump 1. For the purpose of starting
the system or any other purpose, another low-pressure pump 3 may be interposed on
the flow path F
1. To the low-pressure pump 3 applied is, but not limited to, a centrifugal pump.
[0015] As a power source for the triple gear pump 1, energy extracted from a turbine of
the engine 10 for example is applicable, and thus the amount of expelled fluid from
the triple gear pump 1 is proportional to, or at least depends on, the rotating speed
of the turbine. As sometimes the rotating speed is relatively high whereas the fuel
consumption is relatively small particularly when the airplane cruises at a high altitude
for example, the amount of expelled fluid does not necessarily meet the demand by
engine 10. The expelled fluid, in the amount beyond the demand, is portioned out and
fed back through a return path F
3 to the flow path F
1 so that the fluid only at the demanded amount is fed to the engine 10.
[0016] As lubricant oil L is circulated and heated in the engine 10, the expelled fluid
is used for cooling it as well. Specifically, a flow path F
5 is in fluid communication with an oil cooler 9, and the fluid cools the lubricant
oil L and in response receives heat, and thereafter the fluid is introduced through
a feeding path F
7 to a combustion chamber 7 of the engine 10, thereby serving for combustion.
[0017] The triple gear pump 1 by itself generates heat, and some part of the heat turns
back through the return path F
3 to the triple gear pump 1, and resultantly non-negligible temperature rise may occur
in fluid in the flow path F
5. Therefore a cooling capacity of the oil cooler 9 sometimes loses balance against
rise in temperature of the lubricant oil L. An air-cooling oil cooler 11 by air A
extracted from a bypass flow path or such of the engine 10 is thus used supplementally.
With increase in a load on the air-cooling oil cooler 11, which is caused by increase
of return flow through the return path F
3 and resultant rise in temperature of the expelled fluid, thermal stress on respective
portions of the system will increase and some thermal energy will be exhausted in
vain, thereby reducing energy efficiency. In a conventional triple gear pump, by enabling
both a series mode and a parallel mode, increase and decrease of the amount of expelled
fluid is enabled to minimize the amount of return flow.
[0018] The triple gear pump 1 according to the present embodiment, by enabling an unloaded
mode as well as the series and parallel modes, enables further increase and decrease
of the amount of expelled fluid and also enables improvement of energy efficiency.
Specifically, the triple gear pump 1 enables a change from the series and parallel
modes when the airplane idles on the ground and when it cruises at a high altitude
for example, to a mode in which the triple gear pump 1 is released from load and then
the fuel is mainly fed by the centrifugal pump 3 for example when it requires a great
amount of fuel at a time of takeoff or such. The problem is difficulty in pressure
control because high pressure should act on the triple gear pump 1 throughout in the
unloaded mode. Its solution will become apparent in the following descriptions.
[0019] Referring mainly to FIG. 3 in combination with FIGs. 2, 3, the triple gear pump 1
is generally provided with a drive gear 23 driven by a drive shaft 21 and first and
second idler gears 27, 31 respectively driven by the drive gear 23, where the combination
of the drive gear 23 and the first idler gear 27 constitutes a first gear pump G
1 and the combination of the drive gear 23 and the second idler gear 31 constitutes
a second gear pump G
2. The housing 41 encloses these elements and respective spaces 43, 45, 47 defined
by the gear teeth and the housing 41, as being in close contact with tooth tops of
these gears, serve to pressurize and transport fluid in accordance with gear rotation.
The housing 41 is provided with a suction port 49 and a discharge port 51 both in
fluid communication with the first gear pump G
1, and further provided with a suction port 53 and a discharge port 55 both in fluid
communication with the second gear pump G
2. When the drive gear 23 is driven by an external power source to rotate about its
axis, the first and second gear pumps G
1 and G
2 are set in operation in parallel so that fluid at a pressure P
1 is sucked through the suction port 49 is expelled under a pressure P
3 through the discharge port 51, and fluid at a pressure P
5 is sucked through the suction port 53 is expelled under a pressure P
7 through the discharge port 55. The discharge pressures P
3, P
7 are usually higher than the suction pressures P
1, P
5, whereas these pressures depend on operation modes as described below.
[0020] Referring mainly to FIG. 2, the drive shaft 21 for coupling with the power source
is led out of the housing 41 while shafts 25, 29 of the first and second idler gears
27, 31 are enclosed within the housing 41. These shafts 21, 25, 29 are respectively
rotatably supported by floating bearings 33, 35, 37 which are respectively provided
in pair. In addition, the floating bearings 33, 35, 37 respectively hold the gears
23, 27, 31 in therebetween. The floating bearings 33, 35, 37 are slightly floatingly
movable in respective axial directions and receive applied pressure, thereby coming
in contact with both sides of the gears 23, 27, 31 respectively.
[0021] Gaps are held respectively between both ends of the first and second idler shaft
25, 29 and the floating bearings 35, 37 and the housing 41 and are respectively in
fluid communication with the suction ports 49, 53 so that the fluid flows therein
and thus pressurize these end portions by means of the suction pressures P1, P5. These
applied pressures are used for pressing the floating bearings 35, 37 respectively
against the first and second idler gears 27, 31. To spread the fluid over these ends
and equalize pressures thereon, the first and second idler shafts 25, 29 may be hollow
for example. Further, to deliver these applied pressures to the floating bearings
33 of the drive shaft 21, a communication path 67 is interposed and establishes fluid
communication between the floating bearings 37 and the floating bearings 33.
[0022] To introduce an external pressure P
9 distinct from suction pressures P
1, P
5 and apply it to the floating bearings 35, 37, introduction tubes may be provided
on both side faces of the housing 41 for example. To receive the pressure P
9, the floating bearings 35, 37 may be tapered toward corresponding ends and have steps
on these shoulders, and internal ends of the introduction tubes may be opened to these
shoulders. The step faces can serve for receiving the pressure P
9. Any appropriate seals such as gaskets should be interposed between the ends and
the shoulders in order to prevent pressure transmission. In addition, these introduction
tubes may be made in fluid communication with either the discharge port 51 or the
discharge port 55 for example and then the pressure P
9 applied to the step faces in principle matches with the discharge pressure P
3 or P
7. To further regulate applied pressure, any pressurizing means such as springs 39
may be interposed between the shoulders and the housing 41. These are used for regulating
pressures applied to the floating bearings 35, 37.
[0023] Between the housing 41 and the drive shaft 21, seals 61, 63 are interposed to prevent
the internal fluid from leaking out. To one or both of the seals 61, 63 applicable
are mechanical seals that use repulsive force by springs, for example, to press sealing
faces against counter sealing faces. Not to apply excessive pressure to the mechanical
seal, between the aforementioned communication path 67 and the seal 61 interposed
is a seal 65 for preventing transmission of fluid pressure. To this seal 65, a labyrinth
seal is applicable for example.
[0024] The housing 41 may be further provided with another introduction path 69 in order
to retrieve fluid leaked out through the labyrinth seal and apply a proper pressure
P
11 to the mechanical seal 61. The introduction path 69 may be connected to the flow
path F
1 for example so that the fluid before being given the pressure by the triple gear
pump 1 can apply its original pressure to mechanical seal 61. Of course, instead any
other proper flow path may be connected thereto.
[0025] Referring to FIG. 4 in combination with FIG. 2, a force f
1 originated from the suction pressure P
5 acts on the upper ends of the upper floating bearings 33, 37 and therefore a down
force f
d presses the upper floating bearings 33, 37 against the drive gear 23 and the second
idler gear 31. The force originated from the suction pressure P
5 also acts on the lower floating bearing 37 and further on the lower floating bearing
33 as the communication path 67 mediates so that an up force f
u presses the lower floating bearings 33, 37 against the drive gear 23 and the second
idler gear 31. Because the common pressure acts thereon, the forces f
d, f
u are mutually in balance, thereby supporting the drive gear 23 and the second idler
gear 31 stably. Further, by using a force f
2 distinct therefrom (normally greater), the up force f
u can be regulated, thereby preventing the floating bearing 37 from departing from
the second idler gear 31.
[0026] While the aforementioned descriptions mainly relates to the second gear pump G
2, a balance among forces is similarly established in regard to the first gear pump
G
1.
[0027] The triple gear pump 1 shall be put in operation if connected to a fuel feeder system
as shown in FIG. 5. Specifically, the flow path F
1 branches off into two paths respectively connected to an inflow path F
11 and an inflow path F
17. Between the flow path F
1 and the inflow path F
11, a check or non-return valve V
1 may be interposed. The inflow paths F
11, F
17 are respectively connected to the suction ports 49, 53 of the first and second gear
pumps G
1, G
2. The discharge ports 51, 55 thereof are respectively connected to outflow paths F
13, F
19. The inflow path F
11 also branches into two paths, one of which is connected via a valve V
3 to an outflow path F
15 and is, after merging with the outflow paths F
13, F
19, connected to a flow path F
21. The flow path F
21 is connected to the flow path F
5.
[0028] Referring to FIG. 5(a) in combination with FIGs. 2 through 4, when the valve V
3 is closed, the triple gear pump 1 is in operation in a series mode. Then a relatively
low pressure through the flow path F
1 is applied to both the inflow path F
11 in communication with the suction port 49 of the first gear pump G
1 and the inflow path F
17 in communication with the suction port 53 of the second gear pump G
2. As the pressures P
1, P
5 are both low then, the down and up forces f
d, f
u are mutually in balance on any of the floating bearings 33, 35, 37. The fluid pressurized
and expelled out of the discharge port 51 flows through the flow paths F
13, F
15 and the fluid expelled out of the discharge port 55 flows through the flow path F19,
and then the fluid merges together in the flow path F
21 and is then fed to the engine 10.
[0029] Referring to FIG. 5(b) in place of FIG. 5(a), when the valve V
3 is opened, the triple gear pump 1 is in operation in a parallel mode. The exit pressure
P
3 of the first gear pump G
1 acts on the inflow path F
11 through the valve V
3, and resultantly the suction pressure P
1 rises to match with the exit pressure P
3. If the check valve V
1 is interposed there, the fluid is prevented from flowing backward toward the flow
path F
1. Even then the pressure P
1 commonly acts on both the floating bearings 35, thereby balancing the down and up
forces f
d, f
u with each other. Any change in the pressure P
1 does not affect the floating bearings 33, 37. Then the first gear pump G
1 runs on idle (does no work) and only the second gear pump G
2 contributes to feeding the fluid.
[0030] To the valve V
3, not a switching valve but a regulating valve such as a variable throttle valve is
also applicable, which can continuously regulate the flow rate. In this case, while
the valve V
3 can be set in medium states as well as the totally closed state (shown in FIG. 5(a))
and the totally opened state (shown in FIG. 5(b)), force balances on the floating
bearings 33, 35, 37 would not be lost in any of the medium states.
[0031] Referring to FIG. 5(c) in place of FIG. 5(a) and FIG. 5(b), the present embodiment
enables the unloaded mode. The valve V
3 is then kept open (or may be closed) and the amount of expelled fluid from the centrifugal
pump 3 is increased. Then high-pressure made by the centrifugal pump 3 is applied
to both the gear pumps G
1, G
2. As will be understood from the above descriptions, the down and up forces f
d, f
u are mutually in balance on the floating bearing 33, let alone the floating bearings
35, 37, because the pressure reaches the floating bearing 33 of the drive shaft 21
through the communication path 67. Despite high-pressure application to the floating
bearing 33, the labyrinth seal 65 bars the pressure from acting on the mechanical
seal 61. Fluid leakage through the mechanical seal 61 does not occur, or smooth operation
of the mechanical seal 61 is not spoiled.
[0032] In the unloaded mode, both the gear pumps G
1, G
2 do no work substantially and mainly the centrifugal pump 3 alone contributes to feeding
the fluid. The centrifugal pump can, particularly when the engine 10 outputs high
power, efficiently expel a great amount of fluid. As being understood with reference
again to FIG. 1, as the triple gear pump 1 does substantially no work and the return
flow through the return path F
3 can be minimized, temperature rise of the fluid fed to the flow path F
5 can be suppressed. The cooling capacity of the oil cooler 9 can be sufficiently utilized
and in turn the load on the oil cooler 11 can be suppressed.
[0033] The present embodiment allows selection of an optimum mode in response to a state
of the airplane, for example selecting the parallel mode when the engine 10 rotates
at relatively low speed but high power is required, selecting the series mode when
the airplane cruises at a high altitude, and selecting the unloaded mode to mainly
use the centrifugal pump when a particularly high power is required at a time of takeoff.
The present embodiment can realize high energy efficiency in any of these modes.
[0034] Although certain embodiments have been described above, modifications and variations
of the embodiments described above will occur to those skilled in the art, in light
of the above teachings.
INDUSTRIAL APPLICABILITY
[0035] The disclosed art provides a triple gear pump that is capable of being stably operative
not only in a series or parallel mode but also in an unloaded mode.