U.S. patent application number 12/949979 was filed with the patent office on 2012-01-12 for dual force single point actuation integrated load mechanism for securing a computer processor to a socket.
This patent application is currently assigned to INTERNATIONAL BUSINESS MACHINES CORPORATION. Invention is credited to Michael D. French, JR., Michael S. Miller, Peter A. Smith, Paul A. Wormsbecher.
Application Number | 20120009810 12/949979 |
Document ID | / |
Family ID | 43501885 |
Filed Date | 2012-01-12 |
United States Patent
Application |
20120009810 |
Kind Code |
A1 |
French, JR.; Michael D. ; et
al. |
January 12, 2012 |
DUAL FORCE SINGLE POINT ACTUATION INTEGRATED LOAD MECHANISM FOR
SECURING A COMPUTER PROCESSOR TO A SOCKET
Abstract
A dual force single point actuation integrated load mechanism
for securing a computer processor to a socket, the dual force
single point actuation integrated load mechanism including a base
mounted around the socket; and a load plate rotatably coupled to
the base and secured to the base when an activate lever and a hinge
lever are secured above the load plate.
Inventors: |
French, JR.; Michael D.;
(Raleigh, NC) ; Miller; Michael S.; (Raleigh,
NC) ; Smith; Peter A.; (Cary, NC) ;
Wormsbecher; Paul A.; (Apex, NC) |
Assignee: |
INTERNATIONAL BUSINESS MACHINES
CORPORATION
Armonk
NY
|
Family ID: |
43501885 |
Appl. No.: |
12/949979 |
Filed: |
November 19, 2010 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
|
|
12831318 |
Jul 7, 2010 |
7878838 |
|
|
12949979 |
|
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Current U.S.
Class: |
439/331 |
Current CPC
Class: |
H05K 7/1053 20130101;
H01R 12/88 20130101 |
Class at
Publication: |
439/331 |
International
Class: |
H01R 13/62 20060101
H01R013/62 |
Claims
1. A dual force single point actuation integrated load mechanism
for securing a computer processor to a socket, the dual force
single point actuation integrated load mechanism comprising: a base
mounted around the socket; and a load plate rotatably coupled to
the base and secured to the base when an activate lever and a hinge
lever are secured above the load plate, wherein securing the
activate lever secures the hinge lever.
2. The dual force single point actuation integrated load mechanism
of claim 1 wherein the activate lever applies a first force to the
load plate when the activate lever is secured and wherein the hinge
lever applies a second force to the load plate when the hinge lever
is secured.
3. The dual force single point actuation integrated load mechanism
of claim 2 wherein the magnitude of the first force and the
magnitude of the second force are within a predetermined
threshold.
4. The dual force single point actuation integrated load mechanism
of claim 1 further comprising an activate lever latch for securing
the activate lever.
5. The dual force single point actuation integrated load mechanism
of claim 1 wherein the hinge lever is secured when the activate
lever is secured by applying a hinge force to the hinge lever
through a hooked end of the activate lever that is connected to the
hinge lever.
6. The dual force single point actuation integrated load mechanism
of claim 5 wherein the hooked end of the activate lever is
connected to the hinge lever via a looped end of the hinge
lever.
7. The dual force single point actuation integrated load mechanism
of claim 1 wherein the hinge lever is not fully secured when the
activate lever is unsecured.
8. An apparatus with a computer processor securely mounted within a
socket, the apparatus comprising: a computer processor and a dual
force single point actuation integrated load mechanism for securing
the computer processor to the socket, the dual force single point
actuation integrated load mechanism comprising: a base mounted
around the socket; and a load plate rotatably coupled to the base
and secured to the base when an activate lever and a hinge lever
are secured above the load plate, wherein securing the activate
lever secures the hinge lever.
9. The apparatus of claim 8 wherein the activate lever applies a
first force to the load plate when the activate lever is secured
and wherein the hinge lever applies a second force to the load
plate when the hinge lever is secured.
10. The apparatus of claim 9 wherein the magnitude of the first
force and the magnitude of the second force are within a
predetermined threshold.
11. The apparatus of claim 8 further comprising an activate lever
latch for securing the activate lever.
12. The apparatus of claim 8 wherein the hinge lever is secured
when the activate lever is secured by applying a hinge force to the
hinge lever through a hooked end of the activate lever that is
connected to the hinge lever.
13. The apparatus of claim 12 wherein the hooked end of the
activate lever is connected to the hinge lever via a looped end of
the hinge lever.
14. The apparatus of claim 8 wherein the hinge lever is not fully
secured when the activate lever is unsecured.
15. A dual force single point actuation integrated load mechanism
for securing a computer processor to a socket, the dual force
single point actuation integrated load mechanism comprising: a base
mounted around the socket; and a load plate, the load plate secured
to the base when an activate lever and a hinge lever are secured
above the load plate, wherein securing the activate lever secures
the hinge lever.
Description
CROSS-REFERENCE TO RELATED APPLICATION
[0001] This application is a continuation application of and claims
priority from U.S. patent application Ser. No. 12/831,318, filed on
Jul. 7, 2010.
BACKGROUND OF THE INVENTION
[0002] 1. Field of the Invention
[0003] The field of the invention is data processing systems, or,
more specifically, a dual force single point actuation integrated
load mechanism for securing a computer processor to a socket and an
apparatus with a computer processor securely mounted within a
socket.
[0004] 2. Description of Related Art
[0005] Modern computing systems often include powerful computer
processors that are mounted within sockets. The sockets may be
attached to a printed circuit board (`PCB`) such as a motherboard
and be configured to house a computer processor. Modern processors
may require that a force be applied to the processor in order for
the processor to remain situated within the socket such that the
processor maintains a reliable electrical connection to the
socket.
SUMMARY OF THE INVENTION
[0006] A dual force single point actuation integrated load
mechanism for securing a computer processor to a socket is
disclosed. The dual force single point actuation integrated load
mechanism includes a base mounted around the socket. The dual force
single point actuation integrated load mechanism also includes a
load plate rotatably coupled to the base and secured to the base
when an activate lever on a first side of the base and a hinge
lever on a second side of the base are secured above the load
plate. The activate lever on the first side of the load plate is
rotatably coupled with the base and is secured when the activate
lever is fully rotated. The hinge lever on the second side of the
load plate is rotatably coupled with the base and connected to the
activate lever such that rotating the activate lever rotates the
hinge lever. The hinge lever is therefore secured when the activate
lever is secured.
[0007] The foregoing and other objects, features and advantages of
the invention will be apparent from the following more particular
descriptions of exemplary embodiments of the invention as
illustrated in the accompanying drawings wherein like reference
numbers generally represent like parts of exemplary embodiments of
the invention.
BRIEF DESCRIPTION OF THE DRAWINGS
[0008] FIG. 1 sets forth a line drawing of a dual force single
point actuation integrated load mechanism for securing a computer
processor to a socket.
[0009] FIG. 2 sets forth a line drawing of a dual force single
point actuation integrated load mechanism for securing a computer
processor to a socket.
[0010] FIG. 3 sets forth a line drawing of a dual force single
point actuation integrated load mechanism for securing a computer
processor to a socket.
[0011] FIG. 4 sets forth a line drawing of a dual force single
point actuation integrated load mechanism for securing a computer
processor to a socket.
[0012] FIG. 5 sets forth a line drawing of a dual force single
point actuation integrated load mechanism for securing a computer
processor to a socket.
[0013] FIG. 6 sets forth a line drawing of an apparatus with a
computer processor securely mounted within a socket.
DETAILED DESCRIPTION OF EXEMPLARY EMBODIMENTS
[0014] Exemplary apparatus and dual force single point actuation
integrated load mechanisms for securing a computer processor to a
socket in accordance with the present invention are described with
reference to the accompanying drawings, beginning with FIG. 1. FIG.
1 sets forth a line drawing of a dual force single point actuation
integrated load mechanism for securing a computer processor to a
socket. The dual force single point actuation integrated load
mechanism for securing a computer processor to a socket of FIG. 1
includes a base (108) mounted around the socket (not shown) for
receiving a computer processor. The socket for receiving a computer
processor may be embodied as an electrical component that is
mounted on a printed circuit board (`PCB`) and further configured
to receive and house a computer processor. The socket for receiving
a computer processor forms an electrical interface between the
computer processor and the structure, such as the PCB, that the
socket is mounted on. In the example of FIG. 1, the base (108) may
be mounted, for example, on the PCB or otherwise mounted on the
socket so as to provide a force to the computer processor, thereby
securing the computer processor to the socket. The base (108) may
also be mounted to a stiffener or back-plate underneath the PCB
such that the dual force single point actuation integrated load
mechanism can secure the computer processor to the socket.
[0015] The dual force single point actuation integrated load
mechanism for securing a computer processor to a socket of FIG. 1
also includes a load plate (104) rotatably coupled to the base
(108) via a hinge lever (106). The load plate (104) is rotatably
coupled to the base (108) such that one side of the load plate
(104) remains coupled to the base (108) while the other three sides
of the load plate (104) may be decoupled from the base (108),
thereby allowing the load plate (104) to be disengaged from the
computer processor that the integrated load mechanism is securing
to the socket. An illustration of this concept is illustrated and
described in greater detail with reference to FIG. 4.
[0016] The load plate (104) of FIG. 1 is also secured to the base
(108) when an activate lever (102) on a first side (120) of the
base (108) and a hinge lever (106) on a second side (122) of the
base (108) are secured above the load plate (104). The activate
lever (102) and the hinge lever (106) may be coupled to, for
example, torsion springs that apply a force to each lever (102,
106) such that each lever is rotated away from the base (108) in
the absence of any other force being applied to each lever (102,
106). In the example of FIG. 1, the activate lever (102) on the
first side (120) of the base (108) and the hinge lever (106) on the
second side (122) of the base (108) are not in a secured position
above the load plate (104). Placing the activate lever (102) on the
first side (120) of the base (108) and the hinge lever (106) on the
second side (122) of the base (108) in a secured position above the
load plate (104) will be described in more detail below.
[0017] In the example of FIG. 1, the activate lever (102) on the
first side (122) of the load plate (104) is rotatably coupled with
the base (108). The activate lever (102) of FIG. 1 is secured when
the activate lever (112) is fully rotated. For example, applying an
activate force (110) to the activate lever (102) would force the
activate lever (102) towards the activate lever latch (114) of FIG.
1, given that the activate lever (102) is rotatably coupled to the
base (108). When the activate lever (102) is fully rotated, the
activate lever (102) will be held in place by the activate lever
latch (114), at which point the activate lever (102) would be in a
"secured position," as the term is used in this application.
[0018] In the example of FIG. 1, the hinge lever (106) on the
second side (122) of the load plate (104) is also rotatably coupled
with the base (108). The hinge lever (106) of FIG. 1 is also
connected to the activate lever (102) such that rotating the
activate lever (102) rotates the hinge lever (106), given that the
hinge lever (106) is rotatably coupled with the base (108). For
example, applying an activate force (110) to the activate lever
(102) forces the activate lever (102) towards the activate lever
latch (114) of FIG. 1. In the example of FIG. 1, the activate lever
(102) is a single piece metal or other rigid material that runs
under an activate lever mounting (118) and extends towards the
hinge lever (106), such that a portion (116) of the activate lever
(102) is available to apply a force (112) to the hinge lever (106).
When the activate lever (102) rotates towards the base (108) and
the activate lever latch (114), the portion (116) of the activate
lever (102) that is available to apply a force (112) to the hinge
lever (106) also rotates in the same direction, thereby exerting a
hinge force (112) on the hinge lever (106) such that the hinge
lever (106) also rotates towards the base (108). In the example of
FIG. 1, the hinge lever (106) is secured when the activate lever
(102) is secured, which occurs when the activate lever (102) has
been fully rotated and is held in place by the activate lever latch
(114).
[0019] In the example of FIG. 1, the activate lever (102) applies a
first force to the load plate (104) when the activate lever (102)
is secured. The hinge lever (106) of FIG. 1 similarly applies a
second force to the load plate (104) when the hinge lever (106) is
secured. The forces applied to the load plate (104) by the activate
lever (102) and the hinge lever (106) force the load plate (104)
down towards the base (108), thereby causing a force to be exerted
on the computer processor by the load plate (104) and helping to
secure the computer processor within the socket. In the example of
FIG. 1, the magnitude of the first force applied by the activate
lever (102) and the magnitude of the second force applied by the
hinge lever (106) may be within a predetermined threshold such as,
for example, within a predetermined percentage of each other.
[0020] In the example of FIG. 1, and as described above, the dual
force single point actuation integrated load mechanism may also
include an activate lever latch (114) for securing the activate
lever. The activate lever latch (114) operates to hold the activate
lever (102) in a secured position so that each lever (102, 106)
continues to exert a force on the load plate (104) that is
transferred to the computer processor to keep the computer
processor securely mounted within the socket.
[0021] In the example of FIG. 1, the dual force single point
actuation integrated load mechanism includes an activate lever
(102) that includes hooked end at the portion (116) of the activate
lever that applies a force to the hinge lever (106). The hooked end
of the activate lever (102) is interlocked with the hinge lever
(106) via a looped end of the hinge lever (106). Interlocking the
hooked end of the activate lever (102) with the looped end of the
hinge lever (106) provides for a reliable and secure connection
between the activate lever (102) and the hinge lever (106) such
that the activate lever (102) can reliably control the positioning
of the hinge lever (106).
[0022] For further explanation, FIG. 2 sets forth an additional
line drawing of a dual force single point actuation integrated load
mechanism for securing a computer processor to a socket. The dual
force single point actuation integrated load mechanism of FIG. 2 is
identical to the dual force single point actuation integrated load
mechanism of FIG. 1, as it also includes the activate lever (102),
the load plate (104), the hinge lever (106), the base (108), the
activate lever latch (114), and the portion (116) of the activate
lever that applies a force to the hinge lever (106). In the example
of FIG. 2, however, the activate lever (102) and the hinge lever
(106) are in a completely unsecured position such that the activate
lever (102) and hinge lever (106) are not securing the load plate
(104). As described above, the load plate (104) is rotatably
coupled to the base (108). When the activate lever (102) and hinge
lever (106) are not securing the load plate (104), the load plate
(104) may therefore be rotated upwards such that the load plate can
be disengaged from the computer processor, allowing for removal of
the computer processor.
[0023] In the example of FIG. 2, the hooked end of the activate
lever (102), which is located at the portion (116) of the activate
lever (102) that applies a force to the hinge lever (106), and the
looped end of the hinge lever (106) are not interlocked. In this
particular configuration, the activate lever (102) is not exerting
a force on the hinge lever (106) and is not controlling the
positioning of the hinge lever (106). In such an example, the
activate lever (102) would need to be rotated towards the activate
lever latch (114), at which point the hooked end of the activate
lever (102) would engage the looped end of the hinge lever (106)
thereby enabling the activate lever (102) to exert a force on the
hinge lever (106) forcing the hinge lever (106) to be rotated
towards the base (108).
[0024] For further explanation, FIG. 3 sets forth an additional
line drawing of a dual force single point actuation integrated load
mechanism for securing a computer processor to a socket. The dual
force single point actuation integrated load mechanism of FIG. 3 is
identical to the dual force single point actuation integrated load
mechanism of FIG. 1 and FIG. 2, as it also includes the activate
lever (102), the load plate (104), the hinge lever (106), the base
(108), the activate lever latch (114), and the portion (116) of the
activate lever that applies a force to the hinge lever (106). In
fact, components of the dual force single point actuation
integrated load mechanism are positioned as in FIG. 2, but
illustrated from a different perspective.
[0025] In the example of FIG. 3, the hinge lever mounting (302) and
the portion (304) of the hinge lever (106) that limits rotation are
also labeled. The hinge lever mounting (302) is the physical
housing that is used to connect the hinge lever (106) to the base
(108). One end of the hinge lever (106) of FIG. 3 has a looped end
as described above with reference to FIG. 1 and FIG. 2. The other
end of the hinge lever (106) is shaped such that this end serves as
the portion (304) of the hinge lever (106) that limits the rotation
of the hinge lever (106). In between these two ends of the hinge
lever (106), the hinge lever is mounted within the hinge lever
mounting (302) such that the hinge lever (106) is connected to the
base (108) of the dual force single point actuation integrated load
mechanism for securing a computer processor to a socket.
[0026] In the example of FIG. 3, the hinge lever (106) operates as
a hinge for the load plate (104), which is coupled to the hinge
lever (106) at the hinge lever mounting (302) such that the load
plate (104) can rotate about the hinge lever (106). As described
above with reference to FIG. 1 and FIG. 2, the looped end of the
hinge lever (106) can receive a force from the hooked end of the
activate lever (102) such that the looped end of the hinge lever
(106) is forced down towards the base (108) of the dual force
single point actuation integrated load mechanism. When the activate
lever (102) is not exerting a force on the hinge lever (106), as
illustrated in FIG. 3, the looped end of the hinge lever (106) may
rotate away from the base (108) of the dual force single point
actuation integrated load mechanism. The range of rotation is
limited, however, by the portion (304) of the hinge lever (106)
that limits the rotation of the hinge lever (108) which comes into
contact with the base (108) as the looped end of the hinge lever
(106) rotates away from the base (108).
[0027] For further explanation, FIG. 4 sets forth an additional
line drawing of a dual force single point actuation integrated load
mechanism for securing a computer processor to a socket. The dual
force single point actuation integrated load mechanism of FIG. 4 is
similar to the dual force single point actuation integrated load
mechanism described in FIGS. 1-3, as it includes a base (408), a
load plate (404), an activate lever (402), and a hinge lever (406)
that is controlled by a portion (410) of the activate lever (402)
that applies a force to the hinge lever (406).
[0028] The dual force single point actuation integrated load
mechanism of FIG. 4, however, differs from the dual force single
point actuation integrated load mechanism illustrated in FIG. 1-3
in that the hinge lever (406) does not include a looped end that is
interlocked with the hooked end of the activate lever (102).
Instead, the hinge lever (406) also has a hooked end. In the
example of FIG. 4, the positioning of the hinge lever (406) is
controlled by a hooked end of an activate lever (402) that limits
the movement of the hinge lever (406). For example, when the
activate lever (402) is in a secured position and restricted by the
activate lever latch (412), the design of the hooked end is such
that the hinge lever (406) is also in a secured position so that
both levers are exerting forces on the load plate (404), thereby
securing the computer processor in the socket. When the activate
lever (402) in rotated away from the base (408) into an unsecured
position, as illustrated in FIG. 4, the hooked end of the activate
lever (402), by virtue of its physical design, moves within a slot
formed by the hooked end of the hinge lever (406) such that the
hinge lever (406) rotates away from the base (408).
[0029] For further explanation, FIG. 5 sets forth an additional
line drawing of a dual force single point actuation integrated load
mechanism for securing a computer processor to a socket. The dual
force single point actuation integrated load mechanism of FIG. 5 is
identical to the dual force single point actuation integrated load
mechanism of FIG. 4, as it also includes the activate lever (402),
the load plate (404), the hinge lever (406), the base (408), the
activate lever latch (412), and the portion (410) of the activate
lever (402) that applies a force to the hinge lever (406). In the
example of FIG. 5, the activate lever (402) and the hinge lever
(406) are in a completely secured position such that the activate
lever (402) and hinge lever (406) are securing the load plate
(404).
[0030] For further explanation, FIG. 6 sets forth a line drawing of
an apparatus with a computer processor (606) securely mounted
within a socket (604). The apparatus of FIG. 6 also includes a dual
force single point actuation integrated load mechanism (608) for
securing the computer processor (606) to the socket (604) as
described above with reference to FIGS. 1-5. The apparatus of FIG.
6 may also include a PCB (602) upon which the socket (604) is
mounted. The apparatus of FIG. 6 may be embodied, for example, as a
personal computer, a blade in a blade server, or any other
computing device as will occur to those of skill in the art.
[0031] The dual force single point actuation integrated load
mechanism (608) for securing the computer processor to the socket
may be embodied as described above with reference to FIGS. 1-5. In
the example of FIG. 6, the dual force single point actuation
integrated load mechanism (608) may include a base mounted around
the socket (604) and a load plate rotatably coupled to the base and
secured to the base when an activate lever on a first side of the
base and a hinge lever on a second side of the base are secured
above the load plate. In the example of FIG. 6, the activate lever
on the first side of the load plate is rotatably coupled with the
base and is secured when the activate lever is fully rotated. In
the example of FIG. 6, the hinge lever on the second side of the
load plate is rotatably coupled with the base and connected to the
activate lever such that rotating the activate lever rotates the
hinge lever. The hinge lever of FIG. 6 is secured when the activate
lever is secured.
[0032] It will be understood from the foregoing description that
modifications and changes may be made in various embodiments of the
present invention without departing from its true spirit. The
descriptions in this specification are for purposes of illustration
only and are not to be construed in a limiting sense. The scope of
the present invention is limited only by the language of the
following claims.
* * * * *