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US4520424A Expired / Lapsed US ⏱️ 0.0 years remaining

Ventilated instrument panel support rail

Assignee: Boeing Co
•
Filing: 1983-06-13
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Granted: 1985-05-28
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Expires: 2003-06-13
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Abstract

Abstract A support rail structure which provides cooling air for removing heat from instruments. The support rail structures provide uniform cooling along each support rail regardless of instrument orientation within the instrument panel assembly. A system which includes the combination of instrument panel support rail and cooling manifold discharges a continuous flow of forced convection air along the base of the support rail. Valves are shown which provide flow-through cooling for cathode ray tube instruments. The instrument panel support rail structures enable a method of supplying conditioned air when concentration of instrument panels dictate that the air conditioning system be integrated within the panels.

Inventors

  • 👤 Paul E. Carpenter
  • 👤 Charles B. Fisher
  • 👤 Douglas E. Peash

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 17:42
CPC Classifications
H; H05; H05K; H05K7/00; H05K7/20; H05K7/20009; H05K7/20136; H05K7/20154

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 156 words
In combination in the flight deck panel region of an aircraft: an instrument panel; a plurality of dripshields disposed between the aircraft skin and a plurality of instrument modules distributed in spaced apart relationship between said instrument panel and said plurality of dripshields; a plurality of instrument panel support rail assemblies, each of said plurality of instrument panel support rail assemblies disposed between said instrument modules; each of said plurality of instrument panel support rail assemblies including a distribution manifold, and a support rail for retaining said instrument modules in said distributed spaced apart relationship; said distribution manifold including coupling means disposed between air supply ducting and said support rail; said coupling means comprising a plurality of air passages distributed along said manifold adjacent said support rail for dispersing cooling air to said instrument modules; and, wherein said cooling air source manifold includes a pressurization valve assembly for providing flow-through cooling of cathode ray tube instruments.
Claim 2
Dependent Claim 156 words
In combination in the flight deck panel region of an aircraft: an instrument panel; a plurality of dripshields disposed between the aircraft skin and a plurality of instrument modules distributed in spaced apart relationship between said instrument panel and said plurality of dripshields; a plurality of instrument panel support rail assemblies, each of said plurality of instrument panel support rail assemblies disposed between said instrument modules; each of said plurality of instrument panel support rail assemblies including a distribution manifold, and a support rail for retaining said instrument modules in said distributed spaced apart relationship; said distribution manifold including coupling means disposed between air supply ducting and said support rail; said coupling means comprising a plurality of air passages distributed along said manifold adjacent said support rail for dispersing cooling air to said instrument modules; and, wherein said cooling air source manifold includes a pressurization valve assembly for providing flow-through cooling of cathode ray tube instruments.

References Cited (Backward Citations)

US3541395A Cited
US3662667A Cited
US3701928A Cited
US4044515A Cited
US3956673A Cited
US4089040A Cited
DE2613366A1 Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1988-05-27 1988-11-26 1989-05-28 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1992-05-27 1992-11-26 1993-05-28 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1996-05-27 1996-11-26 1997-05-28 $7700.00 Window Closed / Lapsed

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