← Back to Patent Explorer
US3938764A Expired / Lapsed US ⏱️ 0.0 years remaining

Frangible aircraft floor

Assignee: McDonnell Douglas Corp
•
Filing: 1975-05-19
•
Granted: 1976-02-17
•
Expires: 1995-05-19
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract The upper floor of a multi-deck pressurized aircraft having frangible floor panels sealing the floor during normal flight conditions yet rupturable under a predetermined environmental condition such as when a relatively high pressure differential exists between the upper cabin and lower cargo compartments. This may occur, for example, when the cargo compartment is depressurized by inflight explosion or collision. Differential pressure activates the panel destruction apparatus which strikes the frangible floor panels in such manner as to cause them to disintegrate or crumble into small pieces. Typical panels may be chemically strengthened glass, ceramics, etc.

Inventors

  • 👤 Robert G. McIntyre
  • 👤 Otto J. Minnich

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-07 17:53
CPC Classifications
B; B64; B64C; B64C1/00; B64C1/18; B64C2001/009; Y; Y10; Y10T; Y10T137/00; Y10T137/1624; Y10T137/1632; Y10T137/1692; Y10T137/1759; Y10T137/1767; Y10T428/00; Y10T428/24; Y10T428/24628; Y10T428/24661

Claims Analysis

Total Claims: 11
Claim 1
Independent Claim 30 words
A frangible aircraft floor comprising a porous floor support; a frangible panel on said support; and means responsive to a predetermined environmental condition for striking said panel to disintegrate it.
Claim 2
Dependent Claim 30 words
A frangible aircraft floor comprising a porous floor support; a frangible panel on said support; and means responsive to a predetermined environmental condition for striking said panel to disintegrate it.
Claim 3
Dependent Claim 23 words
A frangible aircraft floor as in claim 1 wherein said porous support has openings defined by webs over which said panel is supported.
Claim 4
Dependent Claim 29 words
A frangible aircraft floor as in claim 1 wherein said frangible panel is chemically strengthened to have a thin compression layer at its surface and an inner tension layer.
Claim 5
Dependent Claim 20 words
A frangible aircraft floor as in claim 1 wherein said predetermined environmental condition is a pressure differential between two compartments.
Claim 6
Dependent Claim 25 words
A frangible aircraft floor as in claim 1 wherein said predetermined environmental condition is a reduction in pressure in the cargo compartment of said aircraft.
Claim 7
Dependent Claim 19 words
A frangible aircraft floor as in claim 1 wherein said means is a differential pressure activated panel destruction apparatus.
Claim 8
Dependent Claim 28 words
A frangible aircraft floor as in claim 6 wherein said apparatus includes a spring-loaded plunger releasable by an aneroid initiator in response to an increase in differential pressure.
Claim 9
Dependent Claim 23 words
A frangible aircraft floor as in claim 1 wherein said predetermined environmental condition is a pressure differential between the sides of said panel.
Claim 10
Independent Claim 53 words
A method of equalizing pressure in an upper passenger compartment and a lower cargo compartment comprising the steps of placing a plurality of frangible floor panels on a porous support for said passenger compartment and striking the panels to disintegrate them when the differential pressure between the two compartments exceeds a predetermined amount.
Claim 11
Independent Claim 53 words
A method of equalizing pressure in an upper passenger compartment and a lower cargo compartment comprising the steps of placing a plurality of frangible floor panels on a porous support for said passenger compartment and striking the panels to disintegrate them when the differential pressure between the two compartments exceeds a predetermined amount.

References Cited (Backward Citations)

US1951897A Cited
GB428647A Cited
US2679467A Cited
DE1003851B Cited
US2942811A Cited
US3288992A Cited
US3425333A Cited
US3643899A Cited
US3729154A Cited
US3742968A Cited
US3834076A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1979-02-16 1979-08-18 1980-02-17 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1983-02-16 1983-08-18 1984-02-17 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1987-02-16 1987-08-18 1988-02-17 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag