Title of Invention

A STARTER ALTERNATOR ACCESSORY DRIVE SYSTEM FOR A HYBRID VEHICLE

Abstract The invention relates to a starter alternator accessory drive system (10) for a hybrid vehicle comprising an engine (12); a crank pulley (14) operatively connected to the engine (12); an accessory drive input pulley (20) operatively connected to the crank pulley (14); an accessory (38); an accessory drive output pulley (32) operatively connected to the accessory (38); a planetary gear set (22) disposed between the accessory drive input pulley (20) and the accessory drive output pulley (32) to transfer output from the engine (12) to the accessory (36); a first motor/generator (40) operatively connected to the planetary gear set (22); and a second motor/generator (44) operatively connected to the planetary gear set (22). The first and second motor/generators (40,44) are controllable to power the accessory (38) via the planetary gear set (22) at a selectable rate independent of engine speed, and to re-start the engine (12) while simultaneously powering the accessory (38).
Full Text


FIELD OF INVENTION
The present invention pertains generally to a starter alternator accessory drive
system for a hybrid vehicle.
BACKGROUND OF THE INVENTION
Driven accessories in a hybrid vehicle may include, for example, an air
conditioning compressor, a power steering pump, and an alternator. These
accessories are generally powered by output from the engine. Some of the
accessories in a hybrid vehicle may require power while the engine is off and the
vehicle is being powered by an electric motor/generator. Traditionally, in order to
power hybrid vehicle accessories when the engine is off, it was necessary to
provide each such accessory with a separate electric motor. It is also generally
necessary to provide a device or system configured to restart the engine after it
is turned off.
Conventional automotive accessory drive systems include a drive pulley
connected to an engine output shaft. A flexible chain or belt couples the drive
pulley with a plurality of driven pulleys that are each operatively connected to an
accessory. The operating speeds of the accessories in such a conventional drive
system are directly proportional to the speed of the engine. Since the engine


operates over a wide speed range (i.e., for example, between 500 rpm and
8,000 rpm), the accessories are typically designed to provide full capacity at the
low end of the engine speed range in order to ensure that they remain
operational. Therefore, at higher engine speeds, excess energy transferred to the
accessories may be lost.
WO2005119023 (Al) describes a drive pulley for a cooling pump of an .engine
comprising an input for connection to the engine and an output comprising a
hollow cylindrical member , whose outer surface constitutes a pulley belt
engagement surface. The input and output are connected by a transmission
system comprising an epicyclic gearset including two or more first planet gears ,
which are connected to respective planet shafts to rotate about the axis thereof
and are in mesh with a first sun gear . The gearset comprises two or more
second planet gears , which are connected to rotate with respective first planet
gears and are in mesh with a second sun gear. The planet shafts are connected
to a common carrier which constitutes the input. The first sun gear is
connected to the output . The transmission system comprises, two electric
motor/generators , the rotors of which are connected to the second sun gear
and the output, respectively, and the electrical stator connections of which are
connected to a controller arranged selectively to control the flow of electrical
power between them. The transmission system is at least partially
accommodated within the hollow cylindrical member.


SUMMARY OF THE INVENTION
The present invention provides a starter alternator accessory drive
system for a hybrid vehicle. The starter alternator accessory drive system includes a
planetary gear set having a first, second, and third planetary member. An engine is
operatively connected to the first planetary member, and a first motor/generator is
operatively connected to the second planetary member. A torque transfer device
operatively connects a plurality of accessories to the third planetary member. A
second motor/generator is operatively connected to either the third planetary member
or the torque transfer device. Engine output is transferable through the planetary
gear set to drive the accessories at a selectable rate, and the first and second
motor/generators are controllable to run the accessories while the engine is off and
to re-start the engine.
According to the preferred embodiment, the first planetary member is a
ring gear member, the second planetary member is a sun gear member, and the third
planetary member is a planet carrier member.
According to an alternate embodiment, the first planetary member is a
sun gear member, the second planetary member is a planet carrier member, and the
third planetary member is a ring gear member.
According to another alternate embodiment, the first planetary member
is a ring gear member, the second planetary member is a planet carrier member, and
the third planetary member is a sun gear member.
According to another alternate embodiment, the first planetary member
is a planet carrier member, the second planetary member is a ring gear member, and
the third planetary member is a sun gear member.
According to another alternate embodiment, the first planetary member
is a planet carrier member, the second planetary member is a sun gear member, and
the third planetary member is a ring gear member.
According to another alternate embodiment, the first planetary member
is a sun gear member, the second planetary member is a ring gear member, and the
third planetary member is a planet carrier member.
The above features and advantages and other features and advantages
of the present invention are readily apparent from the following detailed description


of the best modes for carrying out the invention when taken in connection with the
accompanying drawings.
BRIEF DESCRIPTION OF THE ACCOMPANYING DRA WINGS
FIGURE 1 is a schematic depiction of an accessory drive system for a
hybrid vehicle;
FIGURE 2 is a more detailed schematic depiction of the accessory
drive system of Figure 1 in accordance with the preferred embodiment of the present
invention;
FIGURE 3 is a more detailed schematic depiction of the accessory
drive system of Figure 1 in accordance with an alternate embodiment of the present
invention;
FIGURE 4 is a more detailed schematic depiction of the accessory
drive system of Figure 1 in accordance with an alternate embodiment of the present
invention;
FIGURE 5 is a more detailed schematic depiction of the accessory
drive system of Figure 1 in accordance with an alternate embodiment of the present
invention;
FIGURE 6 is a more detailed schematic depiction of the accessory
drive system of Figure 1 in accordance with an alternate embodiment of the present
invention;
FIGURE 7 is a more detailed schematic depiction of the accessory
drive system of Figure 1 in accordance with an alternate embodiment of the present
invention;
FIGURE 8 is a more detailed schematic depiction of the accessory
drive system of Figure 1 in accordance with an alternate embodiment of the present
invention; and
FIGURE 9 is a more detailed schematic depiction of the accessory
drive system of Figure 1 in accordance with an alternate embodiment of the present
invention.


DESCRIPTION OF THE PREFERRED EMBODIMENTS
Conventional accessory drive systems operate by transferring engine
output directly to the accessories so the accessories are driven at a speed directly
proportional to engine speed. Since the engine operates over a wide speed range
(e.g., between 500 rpm and 8,000 rpm), the accessories are typically designed to
provide full capacity at the low end of the engine speed range in order to ensure
they remain fully operational. Therefore, when the engine is operating at higher
speeds, conventional accessory drive systems transfer more energy to the
accessories than necessary to provide adequate function. The excess energy
transferred to the accessories causes inefficiency and diminishes fuel economy. The
starter alternator accessory drive (SAAD) system 10 (shown in Figure 1) of the
present invention allows the accessories to be driven at a predetermined optimal
speed independent from the speed at which the engine is running in order to
improve fuel economy.
Referring to Figure 1, a schematic representation of a SAAD system 10
for a hybrid vehicle is shown. The SAAD system 10 includes an engine 12
configured to transmit output to a crank pulley 14 via a crankshaft or output shaft 16.
A first belt or chain 18 couples the crank pulley 14 with an accessory drive input
pulley 20. The accessory drive input pulley 20 is operatively connected to a
differential transmission such as the planetary gear set 22. The planetary gear set 22
has a plurality of members including: a sun gear 24; a plurality of pinions or planet
gears 26; a ring gear 28; and a pinion carrier or planet carrier 30.
The engine 12 also transfers output via the crankshaft 16 to a
transmission 17. The transmission 17 transfers output from the engine 12 to a
plurality of wheels 19 in order to drive a hybrid vehicle. It should be appreciated that
the transmission 17 and wheels 19 may include any known configurations and are not
included as part of the SAAD system 10 of the present invention.


The planetary gear set 22 is configured to convert the rotational speed
of the accessory drive input pulley 20 (which runs at a fixed ratio of engine speed) to
a predetermined value selected to efficiently drive the accessories 38. In other words,
the planetary gear set 22 can selectively increase or decrease the magnitude of the
rotational speed from the accessory drive input pulley 20 in order to drive the
accessories 38 at more efficient speed and thereby improve fuel economy. Output
from the planetary gear set 22 is transferred to an accessory drive output pulley 32. A
second belt or chain 34 couples the accessory drive output pulley 32 with one or more
accessory pulleys 36. The accessory pulleys 36 are each operatively connected to an
accessory 38.
The SAAD system 10 includes a first motor/generator 40 and a second
motor/generator 44. The first motor/generator 40 is configured to selectively transfer
torque to and/or receive torque from the planetary gear set 22, either directly or
through a transfer device such as, for example, a belt, chain, gear set, differential gear,
etc. The first motor/generator 40 is configured to receive power from and/or transfer
power to a storage device such as the battery 45. The second motor/generator 44 is
configured to selectively transfer torque to and/or receive torque from the planetary
gear set 22; the accessory drive output pulley 32; or one of the accessory pulleys 36,
either directly or through a torque transfer device such as, for example, a belt; chain;
gear set; differential gear; etc. The second motor/generator 44 is configured to
receive power from and/or transfer power to a storage device such as the battery 45.
The first and second motor/generators 40, 44 are configured to selectively operate as a
motor, a generator, or they can be turned off to reduce rotational resistance.
The first and second motor/generators 40, 44 are controllable to drive
the accessories 38 at a predetermined rate regardless of engine speed. As is known in
the art, by transferring a first predetermined amount of input torque from the engine
12 to one of the planetary gear set 22 members, and transferring a second
predetermined amount of input torque from one of the motor/generators 40, 44 to
another of the planetary gear set 22 members, the planetary gear set 22 can be
controlled to produce a selectable amount of output torque from yet another of its
members. Therefore, by controlling the status of the motor/generators 40, 44 (i.e.,
either "motor", "generator", or "off), and the amount of output from the


motor/generators 40, 44, the planetary gear set 22 output speed is selectable within an
operational range.
The first and second motor/generators 40, 44 are controllable to drive
the accessories 38 when the engine 12 is off. Therefore, the accessories 38 remain
operational even when the hybrid vehicle is being powered exclusively by an
alternate power source (not shown) in order to conserve fuel. When the engine 12
is off, one of the motor/generators 40, 44 is preferably run as a motor, and the other
of the motor/generators 40, 44 is preferably run as a generator; however alternate
operational modes may be envisioned. Conventional hybrid vehicle accessory drive
systems typically implement individual electric motors for each accessory in order to
power the accessories when the engine is off. The SAAD system 10 of the present
invention may reduce cost as compared to conventional systems by implementing
fewer components (i.e., two motor/generators 40, 44) to drive all the accessories
38.
The first and second motor/generators 40, 44 are also controllable to
re-start the engine 12. Advantageously, the first and second motor/generators 40,
44 can drive the accessories 38 when the engine 12 is being re-started such that
there is no interruption of accessory 38 operation. More precisely, by controlling
the first and second motor/generators 40, 44, output therefrom is transferable to the
accessories 38 such that the accessories 38 remain powered, and to the engine 12
such that the engine 12 is driven. As the engine 12 is being driven by the
motor/generators 40, 44, a controller such as the controller 42 can introduce engine
spark (not shown) to re-start the engine 12.
The engine 12, the first motor/generator 40, and the second
motor/generator 44 are operatively connected to a controller 42. The controller 42
receives input from the engine 12 indicating the current engine speed and calculates
corresponding speed and torque output values for the motor/generators 40, 44
required to produce a predetermined planetary gear set 22 output speed. As an
example, if the engine 12 is running at 4,000 rpm and the accessories 38 are
optimized to run at 1,000 rpm, the controller 42 calculates the speed and amount of
torque transfer from the motor/generators 40, 44 required to produce a planetary gear


set 22 output speed of 1,000 rpm. These types of calculations are well known to those
skilled in the art and therefore will not be described in detail hereinafter. After
calculating, the controller 42 commands the desired operational status and torque
outputs from the motor/generators 40, 44 such that the accessories 38 are driven in an
optimally efficient manner.
Having explained the components and functionality of the SAAD
system 10, the precise interconnection of these components will now be described in
accordance with a plurality of different embodiments. Figures 2-11 each illustrate a
separate embodiment that functions similarly to the previously described SAAD
system 10, but includes somewhat different component connections. Like reference
numbers are used in Figures 2-9 to refer to like components from Figure 1.
Additionally, the letters "a" through "h" added as a suffix to a reference numeral
identifies a similar component in a different embodiment. As an example, the engine
12 of Figure 1 functions similarly to the engines 12a-12h of Figures 2-9,
respectively. Therefore, unless specified otherwise, the components of Figures 2-9
identified with a base reference number followed by one of the letters "a" through
"h" should be considered to be identical to a respective component of Figure 1
identified with a common base reference number.
Referring to Figure 2, a SAAD system 10a is shown in accordance
with the preferred embodiment of the present invention. The accessory drive input
pulley 20a (which runs at a fixed ratio of engine speed) is operatively connected to the
ring gear 28a of the planetary gear set 22a. The first motor/generator 40a is
operatively connected to the sun gear 24a of the planetary gear set 22a. The second
motor/generator 44a is operatively connected to the planet carrier 30a of the planetary
gear set 22a. The planet carrier 30a of the planetary gear set 22a is also operatively
connected to the accessory drive output pulley 32a. Therefore, in response to input
from the engine 12a (via the ring gear 28a), the first motor/generator 40a (via the sun
gear 24a) and/or the second motor/generator 44a (via the planet carrier 30a), the
planetary gear set 22a can transfer output to the accessory drive output pulley 32a (via
the planet carrier 30a) and thereby drive the accessories 38a at a selectable rate.
When the engine 12a is off, the motor/generators 40a, 44a are controllable to transfer


torque via the sun gear 24a and the planet carrier 30a, respectively, in order to power
the accessories 38a and/or to re-start the engine 12a.
Referring to Figure 3, a SAAD system 10b is shown in accordance
with an alternate embodiment of the present invention. The accessory drive input
pulley 20b (which runs at a fixed ratio of engine speed) is operatively connected to
the sun gear 24b of the planetary gear set 22b. The first motor/generator 40b is
operatively connected to the planet carrier 30b of the planetary gear set 22b. The
second motor/generator 44b is operatively connected to the ring gear 28b. The ring
gear 28b of the planetary gear set 22b is also operatively connected to the accessory
drive output pulley 32b. Therefore, in response to input from the engine 12b (via the
sun gear 24b), the first motor/generator 40b (via the planet carrier 30b) and/or the
second motor/generator 44b (via the ring gear 28b), the planetary gear set 22b can
transfer output to the accessory drive output pulley 32b (via the ring gear 28b) and
thereby drive the accessories 38b at a selectable rate. When the engine 12b is off, the
motor/generators 40b, 44b are controllable to transfer torque via the planet carrier 30b
and the ring gear 28b, respectively, in order to power the accessories 38b and/or to re-
start the engine 12b.
Referring to Figure 4, a SAAD system 10c is shown in accordance
with an alternate embodiment of the present invention. The planetary gear set 22c of
this embodiment preferably includes a double-pinion carrier 30c configuration. The
accessory drive input pulley 20c (which runs at a fixed ratio of engine speed) is
operatively connected to the ring gear 28c of the planetary gear set 22c. The first
motor/generator 40c is operatively connected to the double-pinion carrier 30c of the
planetary gear set 22c. The second motor/generator 44c is operatively connected to
the sun gear 24c of the planetary gear set 22c. The sun gear 24c of the planetary gear
set 22c is also operatively connected to the accessory drive output pulley 32c.
Therefore, in response to input from the engine 12c (via the ring gear 28c), the first
motor/generator 40c (via the double-pinion carrier 30c) and/or the second
motor/generator 44c (via the sun gear 24c), the planetary gear set 22c can transfer
output to the accessory drive output pulley 32c (via the sun gear 24c) and thereby
drive the accessories 38c at a selectable rate. When the engine 12c is off, the
motor/generators 40c, 44c are controllable to transfer torque via the double-pinion


carrier 30c and the sun gear 24c, respectively, in order to power the accessories 38c
and/or to re-start the engine 12c.
Referring to Figure 5, a SAAD system lOd is shown in accordance
with an alternate embodiment of the present invention. The accessory drive input
pulley 20d (which runs at a fixed ratio of engine speed) is operatively connected to
the planet carrier 30d of the planetary gear set 22d. The first motor/generator 40d is
operatively connected to the ring gear 28d of the planetary gear set 22d. The second
motor/generator 44d is operatively connected to an accessory pulley 36d. The sun
gear 24d of the planetary gear set 22d is operatively connected to the accessory drive
output pulley 32d. Therefore, in response to input from the engine 12d (via the planet
carrier 30d), the first motor/generator 40d (via the ring gear 28d) and/or the second
motor/generator 44d (via an accessory pulley 36d), the planetary gear set 22d can
transfer output to the accessory drive output pulley 32d (via the sun gear 24d) and
thereby drive the accessories 38d at a selectable rate. When the engine 12d is off, the
motor/generators 40d, 44d are controllable to transfer torque via the ring gear 28d and
an accessory pulley 36d, respectively, in order to power the accessories 38d and/or to
re-start the engine 12d.
Referring to Figure 6, a SAAD system lOe is shown in accordance
with an alternate embodiment of the present invention. The accessory drive input
pulley 20e (which runs at a fixed ratio of engine speed) is operatively connected to the
planet carrier 30e of the planetary gear set 22e. The first motor/generator 40e is
operatively connected to the sun gear 24e of the planetary gear set 22e. The second
motor/generator 44e is operatively connected to the ring gear 28e of the planetary
gear set 22e. The ring gear 28e of the planetary gear set 22e is also operatively
connected to the accessory drive output pulley 32e. Therefore, in response to input
from the engine 12e (via the planet carrier 30e), the first motor/generator 40e (via the
sun gear 24e) and/or the second motor/generator 44e (via the ring gear 28e), the
planetary gear set 22e can transfer output to the accessory drive output pulley 32e (via
the ring gear 28e) and thereby drive the accessories 38e at a selectable rate. When the
engine 12e is off, the motor/generators 40e, 44e are controllable to transfer torque via
the sun gear 24e and the ring gear 28e, respectively, in order to power the accessories
38e and/or to re-start the engine 12e.


Referring to Figure 7, a SAAD system 10f is shown in accordance with
an alternate embodiment of the present invention. The accessory drive input pulley
20f (which runs at a fixed ratio of engine speed) is operatively connected to the sun
gear 24f of the planetary gear set 22f. The first motor/generator 40f is operatively
connected to the ring gear 28f of the planetary gear set 22f. The second
motor/generator 44f is operatively connected to the planet carrier 30f of the planetary
gear set 22f. The planet carrier 30f of the planetary gear set 22f is also operatively
connected to the accessory drive output pulley 32f. Therefore, in response to input
from the engine 12f (via the sun gear 24f), the first motor/generator 40f (via the ring
gear 24f) and/or the second motor/generator 44f (via the planet carrier 30f), the
planetary gear set 22f can transfer output to the accessory drive output pulley 32f (via
the planet carrier 30f) and thereby drive the accessories 38f at a selectable rate. When
the engine 12f is off, the motor/generators 40f, 44f are controllable to transfer torque
via the ring gear 28f and the planet carrier 30f, respectively, in order to power the
accessories 38f and/or to re-start the engine 12f.
Referring to Figure 8, a SAAD system 10g is shown in accordance
with an alternate embodiment of the present invention. The accessory drive input
pulley 20g (which runs at a fixed ratio of engine speed) is operatively connected to
the ring gear 28g of the planetary gear set 22g. A gear assembly 64g couples the first
motor/generator 40g with the planet carrier 30g of the planetary gear set 22g. The
second motor/generator 44g is operatively connected to one of the accessory pulleys
36g. The sun gear 24g of the planetary gear set 22g is operatively connected to the
accessory drive output pulley 32g. Therefore, in response to input from the engine
12g (via the ring gear 28g), the first motor/generator 40g (via the planet carrier 30g)
and/or the second motor/generator 44g (via an accessory drive pulley 36g), the
planetary gear set 22g can transfer output to the accessory drive output pulley 32g (via
the sun gear 24g) and thereby drive the accessories 38g at a selectable rate. When the
engine 12g is off, the motor/generators 40f, 44f are controllable to transfer torque via
the ring gear 28f and the planet carrier 30f, respectively, in order to power the
accessories 3 8f and/or to re-start the engine 12f.
Referring to Figure 9, a SAAD system 10h is shown in accordance
with an alternate embodiment of the present invention. The accessory drive input


pulley 20h (which runs at a fixed ratio of engine speed) is operatively connected to
the planet carrier 30h of the planetary gear set 22h. A third belt or chain 66h couples
the first motor/generator 40h and the sun gear 24h of the planetary gear set 22h. The
second motor/generator 44h is operatively connected to the ring gear 28h of the
planetary gear set 22h. The ring gear 28h of the planetary gear set 22h is also
operatively connected to the accessory drive output pulley 32h. Therefore, in
response to input from the engine 12h (via the planet carrier 30h), the first
motor/generator 40h (via the sun gear 24h) and/or the second motor/generator 44h
(via the ring gear 28h), the planetary gear set 22h can transfer output to the accessory
drive output pulley 32h (via the ring gear 28h) and thereby drive the accessories 38h
at a selectable rate. When the engine 12h is off, the motor/generators 40h, 44h are
controllable to transfer torque via the sun gear 24h and the ring gear 28h, respectively,
in order to power the accessories 38h and/or to re-start the engine 12h.
While the best modes for carrying out the invention have been
described in detail, those familiar with the art to which this invention relates will
recognize various alternative designs and embodiments for practicing the invention
within the scope of the appended claims.


Claims:
1. A starter alternator accessory drive system (10) for a hybrid vehicle
comprising:
an engine (12);
a crank pulley (14) operatively connected to the engine (12);
an accessory drive input pulley (20) operatively connected to the crank
pulley (14):
an accessory (38);
an accessory drive output pulley (32) operatively connected to the
accessory (38);
a planetary gear set (22) disposed between the accessory drive input
pulley (20) and the accessory drive output pulley (32) to transfer output
from the engine (12) to the accessory (36);
a first motor/generator (40) operatively connected to the planetary gear
set (22); and
a second motor/generator (44) operatively connected to the planetary
gear set (22);


characterized in that the first and second motor/generators (40,44) are
controllable to power the accessory (38) via the planetary gear set (22)
at a selectable rate independent of engine speed, and to re-start the
engine (12) while simultaneously powering the accessory (38).
2. The starter alternator accessory drive system as claimed in claim 1, comprising
at least one belt or chain (18) operatively connecting said accessory drives input
pulley (20) to said crank pulley (14).
3. The starter alternator accessory drive system as claimed in claim 1, comprising
a battery (45) configured to transfer power to and receive power from the first
and second motor/generators (40,44).
4. The starter alternator accessory drive system as claimed in claim 1, comprising
a controller (42) operatively connected to the engine (12), the first
motor/generator (40) and the second motor/generator (44), said controller (42)
configured to calculate required speed and output torque values for the first and
second motor/generators (40,44) in order to control the speed at which the
accessory (38) is run.


5. The starter alternator accessory drive system as claimed in claim 1, wherein
the planetary gear set having a first (28), second (24), and third planetary
member (30), wherein the first planetary member (28) is operatively connected
to an accessory drive input pulley (20), and the third planetary member (30) is
operatively connected to an accessory drive output pulley (32), wherein the first
motor/generator (40) operatively connected to the second planetary member,
wherein the second motor/generator (44) operatively connected to the
accessory drive output pulley (32), and wherein engine output is transferable
through the planetary gear set (22) to drive the plurality of accessories (38) at a
selectable rate.
6. The starter alternator accessory drive system as claimed in claim 1 or 5,
wherein the first planetary member is a ring gear member, the second planetary
member is a sun gear member, and the third planetary member is a planet
carrier member.


7. The starter alternator accessory drive system as claimed in claim 1 or 5,
wherein the first planetary member is a sun gear member, the second planetary
member is a planet carrier member, and the third planetary member is a ring
gear member.
8. The starter alternator accessory drive system as claimed in claim 1 or 5,
wherein the first planetary member is a ring gear member, the second planetary
member is a planet carrier member, and the third planetary member is a sun
gear member.
9. The starter alternator accessory drive system as claimed in claim 1 or 5,
wherein the first planetary member is a planet carrier member, the second
planetary member is a ring gear member, and the third planetary member is a
sun gear member.
10. The starter alternator accessory drive system as claimed in claim 1 or 5,
wherein the first planetary member is a planet carrier member, the second
planetary member is a sun gear member, and the third planetary member is a
ring gear member.


11. The starter alternator accessory drive system as claimed in claim 1 or 5,
wherein the first planetary member is a sun gear member, the second planetary
member is a ring gear member, and the third planetary member is a planet
carrier member.
12. The starter alternator accessory drive system as claimed in claim 1 or 5,
comprising a gear assembly operatively connecting the first motor/generator to
the second planetary member.
13. The starter alternator accessory drive system as claimed in claim 1 or 5,
comprising a belt operatively connecting the first motor/generator to the second
planetary member.
14. A starter alternator accessory drive system for a hybrid vehicle comprising:
a planetary gear set having a first, second, the third planetary member;
one of plurality of pulleys connected by a belt member and a plurality of
sprockets connected by a chain member operatively connecting an engine
with the first planetary member;

a first motor/generator operatively connected to the second planetary
member;
one of a plurality of pulleys connected by a belt member and a plurality of
sprockets connected by a chain member operatively connecting a plurality
of accessories to the third planetary member; and
a second motor/generator operatively connected to one of the third
planetary member and the second torque transfer device;
wherein engine output is transferable through the planetary gear set to
drive the plurality of accessories at a selectable rate, and the first and
second motor/generators are controllable to run the plurality of
accessories while the engine is off and to re-start the engine.
15. The starter alternator accessory drive system as claimed in claim 14, wherein
the planetary gear set comprises a single-pinion carrier.
16. The starter alternator accessory drive system as claimed in claim 14,
wherein the planetary gear set comprises a double-pinion carrier.



ABSTRACT


TITLE: " A STARTER ALTERNATOR ACCESSORY DRIVE SYSTEM FOR A HYBRID
VEHICLE"
The invention relates to a starter alternator accessory drive system (10) for a
hybrid vehicle comprising an engine (12); a crank pulley (14) operatively
connected to the engine (12); an accessory drive input pulley (20) operatively
connected to the crank pulley (14); an accessory (38); an accessory drive output
pulley (32) operatively connected to the accessory (38); a planetary gear set
(22) disposed between the accessory drive input pulley (20) and the accessory
drive output pulley (32) to transfer output from the engine (12) to the accessory
(36); a first motor/generator (40) operatively connected to the planetary gear
set (22); and a second motor/generator (44) operatively connected to the
planetary gear set (22). The first and second motor/generators (40,44) are
controllable to power the accessory (38) via the planetary gear set (22) at a
selectable rate independent of engine speed, and to re-start the engine (12)
while simultaneously powering the accessory (38).

Documents:

00927-kol-2007-abstract.pdf

00927-kol-2007-assignment.pdf

00927-kol-2007-claims.pdf

00927-kol-2007-correspondence others 1.1.pdf

00927-kol-2007-correspondence others 1.3.pdf

00927-kol-2007-correspondence others 1.4.pdf

00927-kol-2007-correspondence others.pdf

00927-kol-2007-description complete.pdf

00927-kol-2007-drawings.pdf

00927-kol-2007-form 1.pdf

00927-kol-2007-form 18.pdf

00927-kol-2007-form 2.pdf

00927-kol-2007-form 3.pdf

00927-kol-2007-form 5.pdf

00927-kol-2007-gpa.pdf

927-KOL-2007-(02-08-2012)-CORRESPONDENCE.pdf

927-KOL-2007-(22-02-2013)-ABSTRACT.pdf

927-KOL-2007-(22-02-2013)-AMANDED PAGES OF SPECIFICATION.pdf

927-KOL-2007-(22-02-2013)-CLAIMS.pdf

927-KOL-2007-(22-02-2013)-CORRESPONDENCE.pdf

927-KOL-2007-ABSTRACT.pdf

927-KOL-2007-AMANDED CLAIMS.pdf

927-KOL-2007-ASSIGNMENT.pdf

927-KOL-2007-CANCELLED PAGES.pdf

927-kol-2007-correspondence others 1.2.pdf

927-KOL-2007-CORRESPONDENCE.pdf

927-KOL-2007-DESCRIPTION (COMPLETE).pdf

927-KOL-2007-DRAWINGS.pdf

927-KOL-2007-EXAMINATION REPORT REPLY RECIEVED.pdf

927-KOL-2007-EXAMINATION REPORT.pdf

927-KOL-2007-FORM 1.pdf

927-KOL-2007-FORM 2.pdf

927-KOL-2007-FORM 26.pdf

927-KOL-2007-FORM 3.pdf

927-kol-2007-form 5.pdf

927-KOL-2007-GRANTED-ABSTRACT.pdf

927-KOL-2007-GRANTED-CLAIMS.pdf

927-KOL-2007-GRANTED-DESCRIPTION (COMPLETE).pdf

927-KOL-2007-GRANTED-DRAWINGS.pdf

927-KOL-2007-GRANTED-FORM 1.pdf

927-KOL-2007-GRANTED-FORM 2.pdf

927-KOL-2007-GRANTED-FORM 3.pdf

927-KOL-2007-GRANTED-FORM 5.pdf

927-KOL-2007-GRANTED-SPECIFICATION-COMPLETE.pdf

927-KOL-2007-OTHERS.pdf

927-KOL-2007-PETITION UNDER RULE 137.pdf

927-kol-2007-priority document.pdf

927-KOL-2007-REPLY TO EXAMINATION REPORT.pdf

927-KOL-2007-TRANSLATED COPY OF PRIORITY DOCUMENT.pdf


Patent Number 255752
Indian Patent Application Number 927/KOL/2007
PG Journal Number 12/2013
Publication Date 22-Mar-2013
Grant Date 20-Mar-2013
Date of Filing 28-Jun-2007
Name of Patentee GM GLOBAL TECHNOLOGY OPERATIONS, INC
Applicant Address 300 GM RENAISSANCE CENTER, DETROIT, MICHIGAN
Inventors:
# Inventor's Name Inventor's Address
1 PATRICK B. USORO 6748 PINE WAY DRIVE, TROY, MICHIGAN 48098
PCT International Classification Number F16H7/00; F16H7/00
PCT International Application Number N/A
PCT International Filing date
PCT Conventions:
# PCT Application Number Date of Convention Priority Country
1 11/464271 2006-08-14 U.S.A.