U.S. patent number 3,759,476 [Application Number 05/227,416] was granted by the patent office on 1973-09-18 for latching system.
This patent grant is currently assigned to McDonnell Douglas Corporation. Invention is credited to Walter H. Goodwin.
United States Patent |
3,759,476 |
Goodwin |
September 18, 1973 |
LATCHING SYSTEM
Abstract
An automatic latching system for pallets and the like including
latching devices, each arranged so a pallet can move thereover to
depress an upwardly biased star wheel until a pallet is positioned
on one or both sides of the latching device, at which time the
spokes of the upwardly extended star wheel hold and restrain the
pallets from vertical and horizontal movement.
Inventors: |
Goodwin; Walter H. (Sierra
Madre, CA) |
Assignee: |
McDonnell Douglas Corporation
(Santa Monica, CA)
|
Family
ID: |
22853028 |
Appl.
No.: |
05/227,416 |
Filed: |
February 18, 1972 |
Current U.S.
Class: |
410/69;
410/92 |
Current CPC
Class: |
B60P
7/08 (20130101); B64D 9/003 (20130101) |
Current International
Class: |
B60P
7/06 (20060101); B60P 7/08 (20060101); B64D
9/00 (20060101); B65d 019/38 () |
Field of
Search: |
;248/361R,119R
;292/DIG.46,280,216,210 ;105/366C,366D |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Allen; Edward C.
Claims
What is claimed is:
1. A latching system for pallets and the like including:
at least one latch assembly, said latch assembly having a base,
linkage means connected to said base, bias means, and a star wheel
member connected for rotation about an axis to said linkage means,
said star wheel being biased upwardly to a predetermined position
by said bias means, said star wheel having spokes which extend
radially outward from the axis at 90.degree. intervals thereabout
for engaging and latching pallets to said assembly and said linkage
means being comprised of first and second pairs of links, said
links having first and second end portions and being connected
together and to said star wheel at said first ends thereof, said
pairs of links extending away from said star wheel in generally
opposite directions, said base including means to connect said link
second ends for rotation and restricted translation to said
base.
2. The latching system defined in claim 1 including:
means to support the pallets at a predetermined distance from said
base, said predetermined support distance being related to said
star wheel predetermined position so the centerline of the pallet
edges is held further from said base than the axis of rotation of
said star wheel.
3. The latching system defined in claim 2 wherein said star wheel
is mounted for rotation substantially 90.degree. from the loading
and unloading direction of the pallets.
4. A latching system for pallets and the like including at least
one latch assembly, said latch assembly having:
a base;
linkage means connected to said base;
bias means;
a star wheel member connected for rotation about an axis to said
linkage means, said star wheel being biased upwardly to a
predetermined position by said bias means, said star wheel having
outwardly extending spokes for engaging and latching pallets to
said assembly which extend radially outward from the axis of
rotation of said star wheel at substantially 90.degree. intervals
thereabout;
means to support the pallets at a predetermined distance from said
base, said predetermined support distance being related to said
star wheel predetermined position so the centerline of the pallet
edge is held further from said base than the axis of rotation of
said star wheel, said star wheel being mounted for rotation
substantially 90.degree. from the loading and unloading direction
of the pallets; and
a locking member movable along said base and including an upwardly
facing abutment surface, said abut-ment surface being a
predetermined distance above said base and being engagable with two
of said spokes when said star wheel is in its predetermined
position, said spokes are about 45.degree. to said base and said
locking member is moved between said base and said star wheel, to
prevent substantial rotation and depression of said star wheel.
5. The latching system defined in claim 4 wherein said locking
member includes an upward facing roller for engaging a pallet
thereover to assure the pallet thereover is no closer than a
predetermined distance to said base.
6. The latching system defined in claim 4 including:
means to positively connect locking members of selected latch
assemblies so said locking members move in unison.
7. The latching system defined in claim 6 wherein said selected
latch assemblies have the axes of rotation of said star wheels
thereof in substantial alignment.
8. The latching system defined in claim 6 wherein said selected
latch assemblies are substantially aligned in the direction of
movement of the pallets.
Description
BACKGROUND OF THE INVENTION
Most of the prior art pallet latches for restraining pallets from
fore, aft, and vertical movement are not usable in automatic
powered loading systems. This is because the prior art latches must
be manually actuated to latch or unlatch the pallets in place. The
few prior art automatic latches are complicated, heavy and
expensive and include special spring and cam arms actuated by the
pallet or other power actuated means to raise and lower retention
means for the latch. In addition, such automatic latches have not
proved to be fail indicative. Therefore, even though they are
designed to work automatically, personnel must be present to assure
that the latches are operating properly. This defeats one of the
primary objects of such latches which is to reduce the manpower
required to handle cargo. Also, it makes such latches unsuitable
for use with automated systems for loading containers and pallets
in a tunnel, such as the belly of an aircraft, where no space is
available to allow a man to move past the loaded pallets for
inspection of the latches in use.
SUMMARY OF THE INVENTION
The present invention solves the problems heretofore unsolved by
the prior art latches by providing a system employing automatic
latches which are lightweight, inexpensive and in the remote chance
of failure, indicate such failure so that aircraft in which they
are used are never endangered by loose pallets. The present latches
provide vertical and horizontal restraint to a pallet,
automatically lower as each pallet goes by and then rebound to
raised positions that enable the restraint of pallets forward
and/or aft of the latches.
Each latch includes a four spoke star wheel which is mounted for
rotation on an upwardly biased linkage assembly. A pallet moving
over the latch contacts a spoke of the star wheel, rotates it and
pushes the star wheel beneath the pallet. Bias means associated
with the star wheel supporting linkage assembly force two of the
spokes up against the bottom of the pallet. As the trailing edge of
the pallet travels over the latch, the bias means force the star
wheel upward to pivot about the end of the pallet and regain its
raised position. Once the star wheel has been pivoted to the raised
position, it is in proper attitude to latch the forward and aft
pallet or to again pivot out of the way as a pallet is moved
thereover. When pallets are in position on both sides of the star
wheel, it is fixed thereby to restrain the pallets. In addition,
once one or two pallets have been positioned in engagement with the
star wheel of the latch, a safety lock can be moved to assure that
the star wheel is locked in its pallet restraining position. The
safety lock can only be moved to its locking position when the star
wheel is in its proper pallet restraining position. It is
preferable that positive means are provided to connect the safety
locks of associated latches together so the failure to latch of one
or more of the latches is immediately discoverable through the
impossibility of moving the positive lock connecting means to a
predetermined locked position.
It is therefore an object of the present invention to provide an
automatic latching system for pallet assemblies in aircraft.
Another object is to eliminate the need for manual manipulation or
inspection of latches within an aircraft.
Another object is to provide an automatic latch which can be used
to restrain pallet assemblies and the like within a tunnel
configuration where access to the latch is limited once the loaded
pallet assemblies have been positioned therein.
Another object is to provide an automatic latch which is fail
indicating, economical, reliable and which is not substantially
heavier than conventional manual latches for such pallets.
These and other objects and advantages of the present invention
will become apparent after considering the following detailed
specification which covers a particular embodiment of the present
invention in conjunction with the accompanying drawings
wherein:
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a plan view of the latching device of the present latch
system invention;
FIG. 2 is a side view of the latching device of FIG. 1 in position
to receive pallet assemblies;
FIG. 3 shows the latching device of FIG. 2 with a pallet assembly
moving thereover;
FIG. 4 is a side view of the latching device of FIG. 2 with its
star wheel in the worst possible condition during the latching of
two adjacent pallet assemblies;
FIG. 5 is a side view of the latching device of FIG. 2 in a locked
condition, restraining two adjacent pallet assemblies; and
FIG. 6 is a plan view of the floor of an aircraft fuselage with a
latching system constructed according to the present invention
installed therein.
DESCRIPTION OF THE PRESENT EMBODIMENT
Referring to the drawings more particularly by reference numbers,
number 10 in FIGS. 1 and 2 denotes an automatic latching device
constructed according to the present invention installed in the
floor 12 of an aircraft. The latch 10 includes a star wheel 14
having spokes 16, 18, 20 and 22. The star wheel 14 is mounted for
rotation on an upwardly biased linkage assembly 24 by means of a
shaft 26 which is held in place by means such as spring keepers 28
and 30. The linkage assembly 24 includes link arms 32, 34, 36 and
38 which are connected together by the shaft 26 at their upper ends
40, 42, 44 and 46, respectively. The ends 40, 42, 44 and 46 of the
link arms 32, 34, 36 and 38 extend upwardly so that the arms cannot
interfere with the action of the star wheel 14 to be described
hereinafter. The opposite ends 48 and 50 of the link arms 32 and
34, respectively, are connected together by means of a shaft 52
which extends therebetween and is partially restrained in
horizontally slotted openings 54 and 56 in a bifurcated base member
58. A horizontally slotted opening 60 in an opposite base member 62
partially restrains a shaft 64 connecting the opposite ends 66 and
68 of links 36 and 38 in a similar manner. The inboard ends 69
(FIG. 3) of the slotted openings 54, 56 and 60 serve as stops to
take all fore, aft and upward loads and to position the star wheel
14 at the correct locking height. The base members 58 and 62 are
connected to the floor structure 12 and the slotted openings 54, 56
and 60, provide clearance so the link arms, 32, 34, 36 and 38 along
with their connected star wheel 14 can be depressed downwardly
against the upward biasing action of a pair of springs 70 and 72
connected about the shaft 52. Ends 74 and 76 of the springs 70 and
72 are restrained by the floor structure 12 while the other ends
thereof, 78 and 80, are connected to the link arms 32 and 34 by
means of inwardly extending rods 82 and 84.
As shown in FIG. 3, the moving of a pallet 86 over the latch 10
causes engagement between the pallet 86 and one of the spokes 16.
This causes the star wheel 14 to rotate away from the pallet 86
until the adjacent spoke 18 comes in contact with the bottom
surface 88 thereof. The contact prevents the star wheel 14 from
further rotation and the weight of the pallet 86 thereafter
depresses the star wheel 14 and its connected linkage assembly 24
against the upward biasing action of the springs 70 and 72. Once
the pallet 86 has moved past the star wheel 14 as shown in FIG. 4,
the biasing action of the springs 70 and 72 causes the star wheel
14 to again assume its raised position as limited by the slotted
openings 54, 56 and 60 and the linkage means 24. As the end of the
pallet 86 passes the centerline 90 of the shaft 26, the spoke 16 is
rotated under the pallet while the adjacent spoke 18 is rotated
thereabove. If the pallet 86 is not restrained adjacent the star
wheel 14 and is moved away from the latch 10, the next pallet 92
will cause the same action of the star wheel 14. However, when the
pallet 86 is restrained adjacent the star wheel 14, as shown in
FIG. 4, the next pallet 92 strikes the spoke 20 of the star wheel
14 causing it to rotate to the position shown in FIG. 5. The upward
pointing spokes 18 and 20 thereafter restrain both pallets 86 and
92. The axial centerline 90 of the shaft 26 and star wheel 14 is
always restrained below the centerlines 94 of the pallets so that
the pallets always tend to move over the star wheel 14 and it is
never possible for a pallet to "tuck under" the shaft 26 and cause
a jammed condition.
Rollers 96 and 98 are provided on the opposite sides of the star
wheel 14. In conjunction with the floor rollers 99, they support
the pallets and further assure that the centerlines 94 of the
pallets never drop below the centerline 90 of the star wheel 14 and
shaft 26. The rollers 96 and 98 also prevent a heavy pallet from
uplifting to depress a light pallet on the other side of star wheel
14. The roller 96 is mounted for rotation to a stationary member
100 while the roller 98 is mounted for rotation to a safety locking
member 102. The locking member 102 is restrained to be slidable a
predetermined distance by suitable means which are shown as a rail
103 and a stud 104. The locking member 102 has a relatively flat
abutment surface 105 which can be slid under the star wheel 14 when
it is in the x position shown in FIG. 5. The abutment surface 105
engages with the two downward pointing spokes 16 and 22 to prevent
rotation and/or depression of the star wheel 14. This fixes the two
opposite upward pointing spokes 18 and 20 to restrain adjacent
pallets from longitudinal or upward motion no matter whether
pallets are on one or both sides of the star wheel 14. The abutment
surface 105 has only slight clearance with the spokes 16 and 22. If
the star wheel 14 is in other than the proper x position, the end
106 of the locking member 102 engages the closest out of position
spoke to restrict further motion of the locking member 102.
As shown in FIG. 6, a purality of latches 10 are installed on the
floor 12 of the aircraft to form the latch system 108. The latches
10 are positioned along the floor 12 in lateral and longitudinal
alignment. The safety locking members 102 of each set for
longitudinally aligned latches 10 are preferably connected together
by positive linkage means 110. The linkage means 110 are usually
operated by means of levers 112 or position indicating solenoids
113 to enable the locking and unlocking of each longitudinal set of
latches 10 separately or in unison. The levers 112 may be manually
operated from any suitable location which is accessible with a full
cargo load such as the doorway 114. In the alternative, the locking
members 102 may be connected by lateral acting linkage (not shown)
which allows a loading crew to leave spaces in the pallet string.
The improper latching of the star wheel 14 of any of the latches 10
is immediately discoverable through the inability to move a lever
112 to the locking position or by the inability of a solenoid 113
to move the linkage means 110.
It is usual practice to provide three or more longitudinal sets of
latches 10. Usually less than all of the longitudinal latch sets
are sufficient to hold the pallets and therefore should one latch
set fail to lock, the cargo pallets can still be secured by the
latches 10 of the other sets and no unloading operation need take
place.
Once the cargo pallets reach their destination, the latches 10 are
unlocked by moving all of the locking members 102 back to the
position shown in FIG. 1. The pallet in the doorway 114 is removed
first. As the doorway pallet moves away from the spokes of the
adjacent star wheels 14, the wheels 14 are free to rotate and
therefore the next pallet is released and can also be removed by
means such as the powered rollers 116. The latches 10 then release
the pallets one at a time in order.
Thus there has been shown and described a novel latching system
which fulfills all of the objects and advantages sought therefor.
Many changes, alterations, modifications, and other uses and
applications of the subject latching system will become apparent to
those skilled in the art after considering this specification and
the accompanying drawings. All such changes, modifications,
variations and other uses and applications which do not depart from
the spirit and scope of the invention are deemed to be covered by
the invention which is limited only by the claims that follow.
* * * * *