IP Library Granted Patent US 9,150,309
Granted Patent B2
US 9,150,309 · App. 13/383,322 · Granted Oct 6, 2015

Fastening system for hanging mountable overhead containers

Inventor: Holger Stierle (Weil der Stadt, DE)
Assignee: SFS intec Holding AG
B64D11/003
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Quick Facts
Patent No.
US 9,150,309
App. No.
13/383,322
Granted
Oct 6, 2015
Kind
B2
Abstract

A fastening system ( 10 ) for hanging mountable overhead containers ( 12 ) is provided. The system includes at least one pair of support lugs ( 20, 22 ) mounted on a support structure ( 14 ) or on the overhead container ( 12 ). The support lugs ( 20, 22 ) can be detachably connected to each other by a pin ( 30 ) that can be drawn back in a pin guide ( 40 ) and thereby spring-loaded in the exit direction. When the support lug ( 22 ) attached to the overhead container ( 12 ) is inserted into the support lug ( 20 ) having the pin guide ( 40 ) when installing the container, the pin ( 30 ) is unlatched in the pin guide ( 40 ) and automatically moves out into the support eye ( 22 ) attached to the overhead container ( 12 ). Using a lever joined ( 60 ) to the pin guide ( 40 ) by a hinge, the pin ( 30 ) can be moved out completely into an end position, and locked in said position. In order to remove the overhead container ( 12 ), the lever ( 60 ) must simply be pivoted back.

Claims (16)

1. A fastening system ( 10 ) for mounting hanging overhead containers ( 12 ) to an aircraft, the fastening system ( 10 ) comprising:

at least one pair of support lugs ( 20 , 22 ), wherein one support lug ( 20 ) is attached to a support structure of the aircraft while the other support lug ( 22 ) is attached to the overhead container ( 12 );

a pin ( 30 ) for interconnecting the at least one pair of support lugs ( 20 , 22 ), wherein the pin ( 30 ) is moveable between a retracted position and an extended position and comprises a recess ( 44 );

receptacle sleeves ( 26 , 86 ) for the pin ( 30 ), wherein one receptacle sleeve ( 26 ) is attached to the one support lug ( 20 ) while the other receptacle sleeve ( 86 ) is attached to the other support lug ( 22 ), and wherein the receptacle sleeves ( 26 , 86 ) are flush with each other in a mounted position of the overhead container ( 12 );

a pin guide ( 40 ) for the pin ( 30 ), wherein the pin guide ( 40 ) is attached to one of the at least one pair of support lugs ( 20 , 22 ); and

a lever ( 60 ) for manual retraction of the pin ( 30 ) into the retracted position and for manual extension of the pin ( 30 ) into the extended position;

wherein the fastening system further comprises:

a compression spring ( 34 ) arranged in the pin guide ( 40 ) for biasing the pin ( 30 ) in a direction of the extended position when the pin ( 30 ) is in the retracted position;

a locking element ( 42 ) for locking the pin ( 30 ) in the retracted position, wherein the locking element ( 42 ) is movable in a direction transverse to the pin ( 30 ), and wherein the locking element ( 42 ) engages into the recess ( 44 ) for locking the pin ( 30 ); and

a release bracket ( 46 ) that includes the locking element ( 42 ), wherein the release bracket ( 46 ) is supported for movement on one of the at least one pair of support lugs ( 20 , 22 ) and is displaced into an unlock position by the other one of the at least one pair of support lugs ( 20 , 22 ) when the receptacle sleeves ( 26 , 86 ) are flush with each other; wherein the pin ( 30 ) detachably interconnects the at least one pair of support lugs ( 20 , 22 ), and wherein the locking element ( 42 ) releases the pin ( 30 ) by disengaging from the recess ( 44 ) when the release bracket ( 46 ) is displaced into the unlock position, such that the pin ( 30 ) biased by the compression spring ( 34 ) automatically extends into the receptacle sleeve of the support lug that displaced the release bracket ( 46 ) into the unlock position.

2. Fastening system according to claim 1 , wherein the release bracket ( 46 ) is biased in a direction of the pin guide ( 40 ) and the receptacle sleeve ( 26 ) of the first support lug ( 20 ) by an additional compression spring ( 48 ).

3. Fastening system according to claim 1 , wherein the lever ( 60 ) can be locked detachably in a closed position by a securing device ( 70 ).

4. Fastening system according to claim 3 , wherein the lever ( 60 ) engages in the closed position with a free end thereof in a spring-loaded part of the securing device ( 70 ) and is held back by the spring-loaded part.

5. Fastening system according to claim 4 , wherein a spring ( 68 ) is attached to the lever ( 60 ), and the spring brings the lever ( 60 ) out of the closed position when the securing device ( 70 ) is released.

6. Fastening system according to claim 5 , wherein the lever ( 60 ) forms, with a connection element ( 62 ) hinged to the pin ( 30 ), an articulated lever for extending and retracting as well as for securing the pin ( 30 ).

7. Fastening system according to claim 1 , wherein a first pair of the support lugs ( 20 , 22 ) and a second pair of the support lugs ( 20 ′, 22 ′) are attachable one next to the other at two adjacent hanging points of two adjacent overhead containers to a multiple-compartment mounting bracket ( 100 ) attached to the support structure ( 14 ).

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 25, 2022
From: SFS INTEC HOLDING AG
To: SFS GROUP INTERNATIONAL AG
Reel/Frame 061328/0559 →
CHANGE OF NAME Recorded Jan 18, 2012
From: SFS INTEC AIRCRAFT COMPONENTS GMBH
To: SFS INTEC HOLDING AG
Reel/Frame 027550/0750 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 10, 2012
From: STIERLE, HOLGER
To: SFS INTEC AIRCRAFT COMPONENTS GMBH
Reel/Frame 027509/0834 →
Priority Claims (1)
DE 10 2009 026 250 · Jul 24, 2009 · national
Continuity (1)
Related Publication 20120145829A1 · Jun 14, 2012