Systems and devices for installing an evacuation slide actuation cable in a connection box assembly of an emergency evacuation slide and overwing door actuation system interface

US9755347B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9755347-B2
Application numberUS-201514971709-A
CountryUS
Kind codeB2
Filing dateDec 16, 2015
Priority dateDec 16, 2015
Publication dateSep 5, 2017
Grant dateSep 5, 2017

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

Connection box assembly is provided for connecting evacuation slide actuation cable of evacuation slide actuation system to evacuation slide inflation system. Connection box assembly comprises connection box, connection box lid coupled thereto, electrical connector blocker coupled to connection box lid, and connection box slider disposed within connection box. Connection box lid is configured to slide between an open and closed position. Electrical connector blocker is configured to prevent electrical connection to electrical connector coupled to evacuation slide inflation system when connection box lid is in open position and to permit electrical connection to electrical connector when connection box lid is in closed position. Connection box slider is positioned to receive first cable end of evacuation slide actuation cable when connection box lid is in open position. Connection box lid in closed position closes connection box retaining and sealing connection box slider and first cable end inside connection box assembly.

First claim

Opening claim text (preview).

The invention claimed is: 1. A connection box assembly for connecting an evacuation slide actuation cable of an evacuation slide actuation system to an evacuation slide inflation system, the connection box assembly comprising: a connection box; a connection box lid coupled to the connection box and configured to slide between an open position and a closed position; an electrical connector blocker coupled to the connection box lid and configured to prevent electrical connection to an electrical connector coupled to the evacuation slide inflation system when the connection box lid is in the open position and to permit electrical connection to the electrical connector when the connection box lid is in the closed position; and a connection box slider disposed within the connection box and positioned to receive a first cable end of the evacuation slide actuation cable when the connection box lid is in the open position, wherein the connection box lid in the closed position closes the connection box to retain and seal the connection box slider and the first cable end inside the connection box assembly. 2. The connection box assembly of claim 1 , wherein the electrical connector is configured to be connected to an electrical harness from the aircraft in response to the electrical connector blocker permitting electrical connection. 3. The connection box assembly of claim 2 , wherein the electrical connector blocker permits connection of the electrical harness to the electrical connector in response to the first cable end of the evacuation slide actuation cable and the connection box slider being retained and sealed inside the connection box assembly. 4. The connection box assembly of claim 3 , Therein connection of the electrical harness to the electrical connector permits a pressure sensor reading that does not occur if the first cable end of the evacuation slide actuation cable and the connection box slider are not retained and sealed inside the connection box assembly. 5. The connection box assembly of claim 1 , wherein the electrical connector blocker has a first end coupled to the connection box lid and a second free end opposite to the first end and configured to physically block the electrical connector by covering the electrical connector when the connection box lid is in the open position and to expose the electrical connector by uncovering the electrical connector when the connection box lid is in the closed position. 6. The connection box assembly of claim 5 , wherein the electrical connector blocker comprises a rigid, non-bendable material. 7. The connection box assembly of claim 5 , wherein the second free end has an opening therein to expose the electrical connector. 8. A system for assuring connection of an evacuation slide actuation cable to an evacuation slide inflation system, the system comprising: an electrical connector coupled to the evacuation slide inflation system; and a connection box assembly comprising: a connection box; a connection box Rd coupled to the connection box and configured to slide between an open position and a closed position; a connection box slider disposed within the connection box and positioned to receive a first cable end of the evacuation slide actuation cable when the connection box lid is in the open position, wherein the connection box lid in the closed position closes the connection box to retain and seal the connection box slider and the first cable end inside the connection box assembly; and an electrical connector blocker coupled to the connection box lid for preventing electrical connection to the electrical connector prior to retaining and sealing the first cable end and the connection box slider in the connection box assembly. 9. The system of claim 8 , wherein the electrical connector blocker is configured to physically block the electrical connector when the connection box lid is in the open position and to expose the electrical connector when the connection box lid is in the closed position. 10. The system of claim 9 , wherein the electrical connector is configured to be connected to an electrical harness from the aircraft when the electrical connector is exposed. 11. The system of claim 10 , wherein the electrical connector blocker permits connection of the electrical harness to the electrical connector only after the connection box lid is in the closed position and the first cable end of the evacuation slide actuation cable and the connection box slider have been retained and sealed inside the connection box assembly. 12. The system of claim 11 , wherein connection of the electrical harness to the electrical connector permits a pressure sensor reading that does not occur if the first cable end and the connection box slider are not retained and sealed inside the connection box assembly. 13. The system of claim 8 , wherein the electrical connector blocker has a first end coupled to the connection box lid and a second free end opposite to the first end and configured to physically block the electrical connector by covering the electrical connector when the connection box lid is in the open position and to expose the electrical connector by uncovering the electrical connector when the connection box lid is in the closed position. 14. The system of claim 8 , wherein the electrical connector blocker comprises a rigid, non-bendable material. 15. The system of claim 13 , wherein the second free end has an opening therein to expose the electrical connector. 16. An installation assurance method comprising: coupling an electrical connector blocker to a connection box lid of a connection box assembly comprising: the electrical connector blocker; a connection box; the connection box lid coupled to the connection box and configured to slide between an open position and a closed position; and a connection box slider disposed within the connection box; sliding the connection box lid to the open position wherein the electrical connector blocker prevents electrical connection to an electrical connector coupled to an evacuation slide inflation system; inserting a first cable end of the evacuation slide actuation cable into the connection box and the connection box slider; and sliding the connection box lid to the closed position thereby closing the connection box to retain and seal the connection box slider and the first cable end inside the connection box assembly and permitting electrical connection to the electrical connector only after the connection box slider and the first cable end are retained and sealed inside the connection box assembly. 17. The installation assurance method of claim 16 , wherein coupling the electrical connector blocker to the connection box lid physically blocks the electrical connector when the connection box lid is in the open position and exposes the electrical connector when the connection box lid is in the closed position. 18. The installation assurance method of claim 17 , wherein coupling the electrical connector blocker to the connection box lid comprises fastening a first end of the electrical connector blocker to the connection box lid, the electrical connector blocker having a free second end for covering the electrical connector for physically blocking thereof. 19. The installation assurance method of claim 17 , wherein the electrical connector is configured to be connected to an electrical harness from the aircraft when the electrical connector is exposed, the method further comprising verifying retention and sealing of the first cable end and the

Assignees

Inventors

Classifications

  • B64D25/14Primary

    Inflatable escape chutes · CPC title

  • H01R13/447Primary

    Shutter or cover plate · CPC title

  • Sealing means between cable and housing, e.g. grommet (H01R13/5221 takes precedence) · CPC title

  • for making dustproof, splashproof, drip-proof, waterproof, or flameproof connection, coupling, or casing · CPC title

  • for manufacturing contact members, e.g. by punching and by bending · CPC title

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What does patent US9755347B2 cover?
Connection box assembly is provided for connecting evacuation slide actuation cable of evacuation slide actuation system to evacuation slide inflation system. Connection box assembly comprises connection box, connection box lid coupled thereto, electrical connector blocker coupled to connection box lid, and connection box slider disposed within connection box. Connection box lid is configured t…
Who is the assignee on this patent?
Goodrich Corp
What technology area does this patent fall under?
Primary CPC classification B64D25/14. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Sep 05 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).