Airplane container door hinge

Information

  • Patent Grant
  • 6510589
  • Patent Number
    6,510,589
  • Date Filed
    Thursday, April 4, 2002
    22 years ago
  • Date Issued
    Tuesday, January 28, 2003
    21 years ago
Abstract
A hinge for joining two adjacent panels. The hinge comprises a first piece adapted to receive a first panel, a second piece adapted to receive a second panel, and a middle piece. Each of the first and second pieces has an opening for receiving a panel and a socket defined between two spaced stopping surfaces. Portions of the middle piece are received within the sockets of the first and second hinge pieces. The configuration of the hinge pieces prevents the panels from folding in one direction while enabling the panels to fold together in the other direction.
Description




FIELD OF THE INVENTION




This invention relates to a hinge for securing two adjacent door panels of an airplane cargo container so that the panels may fold in one direction only and end up parallel to one another.




BACKGROUND OF THE INVENTION




Airplane cargo containers specifically configured to fit inside the fuselage of an airplane have been used for years. U.S. Pat. No. 4,747,504 assigned to Airborne Express, Inc. discloses one such aircraft cargo container. This patent discloses a three-panel door slidably mounted in channels to enable the door to fold in an accordion fashion and be stored above the container when not in use. An upper panel is secured to an intermediate panel with a piano-type hinge, and similarly the intermediate panel is secured to a lower panel with another piano-type hinge. The piano-type hinges are located on opposite sides of the door. The door panels may be folded upon one another in order to fully open, partially open, or close an opening at the front of the container. However, these piano-type hinges are not structurally strong enough to withstand common loads placed upon the door which may be up to 2000 pounds of pressure. Additionally, these piano-type hinges are expensive to apply to the door because they require many rivets applied to the panels of the door. Thus, to apply a piano-type hinge to a door panel is very labor intensive. Additionally, the rivets used to secure the piano-type hinges to the door panels may wear over time, causing the hinges to be easily torn off the door panels.




Consequently, it is one objective of the present invention to provide a hinge for use with container doors which will withstand large loads.




It is a further objective of the present invention to provide a hinge which enables two door panels to fold in one direction only. It is a further objective of the present invention to provide a hinge which connects two door panels without the use of rivets.




SUMMARY OF THE INVENTION




The invention of this application which accomplishes these objectives comprises a hinge for joining two adjacent door panels. The hinge may be used in many other applications and is not intended to be limited to use with airplane container door panels.




The hinge comprises a first piece adapted to receive a first door panel, a second piece adapted to receive a second door panel, and a middle piece joining the first and second pieces so that the first and second pieces, along with their respective panels, can only be folded in one direction. Each of the first and second pieces has an opening for receiving a door panel and a socket defined between two spaced stopping surfaces. The openings may be any size or configuration in order to receive panels of different thicknesses and configurations. Each of the stopping surfaces is essentially planar and extends the width of the door panel to which the piece is attached.




The middle piece has a pair of cylindrical sections at the outer ends of arms extending radially outward from a central section of the middle piece. Each of the arms has an outer surface and an inner surface. One of the cylindrical sections of the middle piece of the hinge is received within the socket of the first piece of the hinge. The other of the cylindrical sections of the middle piece of the hinge is received within the socket of the second piece of the hinge. Each of the cylindrical sections has a circular cross sectional configuration.




Interengagement of the stopping surfaces of the first and second pieces of the hinge with the arms of the middle piece of the hinge prevents the door panels from folding in one direction but enables the door panels to fold in the other direction together so that they are substantially parallel (side by side). The stopping surfaces of the first and second pieces of the hinge abut the outer surface of the arms of the middle piece of the hinge when the panels are opened, thus preventing the door panels from folding in one direction while enabling the door panels to fold in the other direction. When the door panels are closed or folded together, the stopping surfaces of the first and second pieces of the hinge abut an inner surface of the arms of the middle piece of the hinge.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a perspective view of a airplane cargo container having a three-panel door equipped with the hinge of the present invention.





FIG. 2

is an enlarged view of the encircled area


2


of FIG.


1


.





FIGS. 3A-3C

illustrate the process of opening the hinged container door of FIG.


1


.





FIG. 3A

is a view taken along the line


3


A—


3


A of

FIG. 1

, illustrating the door in a closed position.





FIG. 3B

illustrates the door in a partially closed position.





FIG. 3C

illustrates the door in an open position.





FIG. 4A

is a side view of the three-part hinge of the present invention





FIG. 4B

is a side view of the middle section of the three-part hinge of the present invention.











DETAILED DESCRIPTION OF THE INVENTION




Referring to the drawings, and particularly to

FIG. 1

, there is illustrated an airplane cargo container


10


having a door


12


. The door


12


comprises a bottom panel


14


, a middle panel


16


, and a top panel


18


, connected together with a pair of hinges


20


,


22


. The first hinge


20


connects the bottom and middle panels


14


,


16


together. The second hinge


22


connects the intermediate and top panels


16


,


18


together. The top panel


18


has a pair of latches


24


which function to lock the door in a closed position as illustrated in FIG.


1


.




Referring now to

FIG. 2

, the hinge


22


will be described in detail. The hinge


22


joins the middle panel


16


to the top panel


18


. As illustrated in

FIG. 2

, each of the panels is adapted to slide inside a track


26


in the direction of arrow


27


, as will be described in more detail below. The hinge


22


is made up of three pieces: a first piece


30


, a second piece


32


and a middle piece


34


. The middle piece


34


is sometimes referred to as a “dog bone” due to its configuration.




The first piece


30


of the hinge


22


has an opening


36


adapted to receive a portion of the middle door panel


18


. Additionally, the first piece


30


of the hinge


22


has a socket


38


defined between two spaced stopping surfaces


40


and


42


. Each stopping surface


40


,


42


is generally planar and extends the width of the first hinge piece


30


.




Similarly, the second piece


32


of the hinge


22


has an opening


44


for receiving a portion of the top panel


18


and a socket


46


defined between generally planar stopping surfaces


48


and


50


. As illustrated in

FIG. 2

, the width of the first piece


30


of the hinge


22


is greater than the width of the second piece


32


of the hinge


22


to enable the top door panel


18


to fold downwardly from the position illustrated in

FIG. 3A

to the position illustrated in FIG.


3


B. See arrow


33


of FIG.


3


A.




As best illustrated in

FIG. 4B

, the last piece of the hinge


22


is a middle piece


34


which has a central section


52


, a pair of arms


54


,


56


extending outwardly from the central section


52


, and a pair of outermost cylindrical sections


58


,


60


at the outer ends of arms


54


,


56


, respectively. Arm


54


has an outer surface


62


and an inner surface


64


. Similarly, arm


56


has an outer surface


66


and an inner surface


68


. As illustrated in

FIGS. 2 and 4A

, the cylindrical sections


60


,


58


of the middle piece


34


of the hinge


22


are received within the sockets


38


,


46


of the second and first pieces


30


,


32


of the hinge, respectively. When the door panels


16


,


18


are generally co-planar and the hinge


22


is open the stopping surface


40


of the first piece


30


of the hinge


22


abuts the outer surface


66


of the arm


56


of the middle piece


34


of the hinge


22


. Similarly, the stopping surface


48


of the second piece


32


of the hinge


22


abuts the outer surface


62


of the arm


54


of the middle piece


34


of the hinge


22


, thus preventing the door panels


16


,


18


from folding upon one another in one direction while yet enabling the two panels


16


,


18


to fold upon one another in the other direction, the direction of arrow


33


illustrated in FIG.


3


A.




As illustrated in

FIG. 3B

, the stopping surface


42


of the first piece


30


of the hinge


22


abuts the inside surface


68


of the arm


56


of the middle piece


34


of the hinge


22


when the top door panel


18


is folded downwardly into the position shown in FIG.


3


B. Similarly, the stopping surface


50


of the second piece


32


of the hinge


22


abuts the inside surface


64


of the arm


54


of the middle piece


34


of the hinge


22


.




In order for the hinge of the present invention to function properly the angles illustrated in

FIG. 4A

must be maintained.




Referring to

FIGS. 3A-3C

, the method of opening the container door


12


will be briefly described. The user first opens the latches


24


on the top panel


18


of the door and folds the top panel


18


from the position illustrated in

FIG. 3A

to the position illustrated in FIG.


3


B. The door


12


is then slide upwardly in track


26


in the direction of arrow


70


until only the bottom panel


20


is in the track


26


. Due to the opposite orientations of the hinges


20


,


22


, the top and middle panels


18


,


16


may fold together as shown in FIG.


3


C and rest on top of the container


10


.




Although a detailed description of one preferred embodiment of the present invention has been described above, those of ordinary skill in the art will appreciate changes and modifications which may be made to the present invention without departing from the spirit and scope of the present invention. It is therefore, applicant's intention to be bound only by the scope of the following claims and not to the detailed specifics provided in the above specification.



Claims
  • 1. A hinge for joining two adjacent members, said hinge comprising:a first piece adapted to receive a first member, said first piece having a socket defined between two spaced stopping surfaces, a second piece adapted to receive a second member, said second piece having a socket defined between two spaced stopping surfaces, and a middle piece having a pair of cylindrical sections at outer ends of arms extending outwardly from a central section of said middle piece, one of said cylindrical sections being received within said socket of said first piece and the other of said cylindrical sections being received within said socket of said second piece wherein interengagement of said stopping surfaces of said first and second pieces of said hinge with said middle section of said hinge prevents said adjacent members from folding in one direction while enabling said adjacent members to fold together in the other direction.
  • 2. The hinge of claim 1 wherein said hinge is aluminum.
  • 3. The hinge of claim 1 wherein said hinge is extruded.
  • 4. The hinge of claim 1 wherein said middle piece of said hinge may be removed and rotated 180 degrees causing said adjacent members to only fold in an opposite direction than the direction set forth in claim 1.
  • 5. A hinge for joining two adjacent members, said hinge comprising:a first piece adapted to receive a first member, said first piece having an opening for receiving said first member and a socket defined between two spaced stopping surfaces, a second piece adapted to receive a second member, said second piece having an opening for receiving said second member and a socket defined between two spaced planar stopping surfaces, and a middle piece having a pair of cylindrical sections at outer ends of arms extending outwardly from a central section of said middle piece, one of said cylindrical sections being received within said socket of said first piece of said hinge and the other of said cylindrical sections being received within said socket of said second piece of said hinge wherein said one of said stopping surfaces of said first and second pieces of said hinge abuts an outer surface of said arms of said middle piece of said hinge when said members are generally parallel preventing said members from folding in one direction while enabling said members to fold in the other direction.
  • 6. The hinge of claim 5 wherein said hinge pieces are made of extruded aluminum.
  • 7. The hinge of claim 5 wherein one of said stopping surfaces of said first and second pieces of said hinge abuts an inner surface of said arms of said middle piece of said hinge when said members are folded together.
CROSS REFERENCE TO RELATED APPLICATIONS

This application is a continuation application of U.S. patent application Ser. No. 09/723,923 filed Nov. 28, 2000 entitled “Airplane Container Door Hinge”, now U.S. Pat. No. 6,378,172, and claims priority of provisional application No. 60/222,364, filed Aug. 1, 2000 which is fully incorporated by reference herein.

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Foreign Referenced Citations (2)
Number Date Country
2028919 Apr 1992 CA
29721316 Jan 1998 DE
Provisional Applications (1)
Number Date Country
60/222364 Aug 2000 US
Continuations (1)
Number Date Country
Parent 09/723923 Nov 2000 US
Child 10/116226 US