Patent US3285764A successfully refreshed from Google Patents.
US5208735A
Expired / Lapsed
US
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Latching system for avionics line replaceable modules including a handle cam and a pivoting latch cam
Assignee: Boeing North American Inc
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Filing: 1991-12-12
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Granted: 1993-05-04
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Expires: 2011-12-12
Abstract
Abstract A system for mounting avionics line replaceable modules in an avionics rack where electrical connections are made between the back end of the LRM and connectors disposed within the rack and where the latching assembly includes two rotating cams, one at the bottom of the LRM and the other at the top of engaging spring biased latch plates and thereby securely holding the LRM in the rack.
Inventors
- 👤 Todd Twachtmann
- 👤 James B. Shumaker
- 👤 M. Duane Weltha
- 👤 Chris L. Thompson
- 👤 David M. Mick
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 10:37
CPC Classifications
H; H05; H05K; H05K7/00; H05K7/14; H05K7/1401; H05K7/1411; Y; Y10; Y10T; Y10T292/00; Y10T292/08; Y10T292/0801; Y10T292/0834; Y10T292/0836; Y10T292/0838; Y10T403/00; Y10T403/59; Y10T403/591; Y10T403/595
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
78 words
An improved mounting system for avionics equipment comprising: a rack, a carrying handle, a pivoting handle cam disposed on a first end of said carrying handle, a pivoting latch cam; a slide arm coupled with said pivoting latch cam and said carrying handle; a first spring loaded latch plate disposed on said rack for coupling with said pivoting handle cam; and, a second spring loaded latch plate disposed on said rack for coupling with said pivoting latch cam.
Claim 2
Dependent Claim
78 words
An improved mounting system for avionics equipment comprising: a rack, a carrying handle, a pivoting handle cam disposed on a first end of said carrying handle, a pivoting latch cam; a slide arm coupled with said pivoting latch cam and said carrying handle; a first spring loaded latch plate disposed on said rack for coupling with said pivoting handle cam; and, a second spring loaded latch plate disposed on said rack for coupling with said pivoting latch cam.
Claim 3
Independent Claim
160 words
An apparatus for securing aviation electronics modules in an aircraft, comprising: a rack having a front end and a back end and a plurality of voids therein, said rack being mountable inside an aircraft; an aviation electronics module having a front end and a back end, disposed within one of said plurality of voids within said rack; a first cam disposed on the module for providing a predetermined force on the module with respect to the rack; a second cam disposed on the module for providing a predetermined force on the module with respect to the rack; a first lever means coupled with and manipulating the first cam, so a predetermined force is applied to the module when the lever means is manipulated; and, a second lever means coupled with said first lever means and said second cam so a manipulation of said first lever means results in a predetermined force being applied to the module by the second cam.
Claim 4
Independent Claim
160 words
An apparatus for securing aviation electronics modules in an aircraft, comprising: a rack having a front end and a back end and a plurality of voids therein, said rack being mountable inside an aircraft; an aviation electronics module having a front end and a back end, disposed within one of said plurality of voids within said rack; a first cam disposed on the module for providing a predetermined force on the module with respect to the rack; a second cam disposed on the module for providing a predetermined force on the module with respect to the rack; a first lever means coupled with and manipulating the first cam, so a predetermined force is applied to the module when the lever means is manipulated; and, a second lever means coupled with said first lever means and said second cam so a manipulation of said first lever means results in a predetermined force being applied to the module by the second cam.
Claim 5
Dependent Claim
291 words
An avionics holddown system, comprising: a rack, for receiving modules, mountable in an aircraft, said rack having a latch end and a connector end; a module having a latch end and a connector end, said module disposed in said rack so that said latch end of said module is aligned with said latch end of said rack and said connector end of said module is aligned with said connector end of said rack; said first cam disposed on said first lever means and said second cam coupled to said first lever means; a first cam disposed on said latch end of said module for engaging said latch end of said rack; a second cam disposed on said latch end of said module for engaging said latch end of said rack; a first spring-loaded latch plate disposed on said latch end of said rack for receiving said first cam; a second spring-loaded latch plate disposed on said latch end of said rack for receiving said second cam; a latch hook disposed on said latch end of said module; a spring-loaded latch pin disposed on said first lever means for cooperating with said latch hook and thereby maintaining said first lever means in a closed position when said spring-loaded latch pin engages said latch hook; and, said first spring loaded latch plate and said second spring-loaded latch plate having springs therein with predetermined characteristics, so that a manipulation of the first lever means results in engagement of one of said cams with one of said latch plates and providing a predetermined force thereon, while permitting further manipulation of said first lever means to result in engagement of another of said cams with another of said latch-plates so that a predetermined force is applied.
Claim 6
Dependent Claim
291 words
An avionics holddown system, comprising: a rack, for receiving modules, mountable in an aircraft, said rack having a latch end and a connector end; a module having a latch end and a connector end, said module disposed in said rack so that said latch end of said module is aligned with said latch end of said rack and said connector end of said module is aligned with said connector end of said rack; said first cam disposed on said first lever means and said second cam coupled to said first lever means; a first cam disposed on said latch end of said module for engaging said latch end of said rack; a second cam disposed on said latch end of said module for engaging said latch end of said rack; a first spring-loaded latch plate disposed on said latch end of said rack for receiving said first cam; a second spring-loaded latch plate disposed on said latch end of said rack for receiving said second cam; a latch hook disposed on said latch end of said module; a spring-loaded latch pin disposed on said first lever means for cooperating with said latch hook and thereby maintaining said first lever means in a closed position when said spring-loaded latch pin engages said latch hook; and, said first spring loaded latch plate and said second spring-loaded latch plate having springs therein with predetermined characteristics, so that a manipulation of the first lever means results in engagement of one of said cams with one of said latch plates and providing a predetermined force thereon, while permitting further manipulation of said first lever means to result in engagement of another of said cams with another of said latch-plates so that a predetermined force is applied.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1996-05-03 | 1996-11-02 | 1997-05-04 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2000-05-03 | 2000-11-02 | 2001-05-04 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2004-05-03 | 2004-11-02 | 2005-05-04 | $7700.00 | Window Closed / Lapsed |