Patent EP0242626B1 successfully refreshed from Google Patents.
Patent US3973645A successfully refreshed from Google Patents.
US3973645A
Expired / Lapsed
US
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Inflatable evacuation slide
Assignee: Zodiac Acquisition Corp
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Filing: 1975-08-15
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Granted: 1976-08-10
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Expires: 1995-08-15
Abstract
Abstract Disclosed is a generally five-sided inflatable evacuation slide in which one corner of the slide is supported on the aircraft wing surfaces and the sliding surface is both banked and canted away from the elevated egress of the aircraft.
Inventors
- 👤 Earl E. Dix
- 👤 William H. Fischer
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 23:46
CPC Classifications
B; B64; B64D; B64D25/00; B64D25/08; B64D25/14
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
118 words
Inflatable slide apparatus for evacuation from an elevated egress of an aircraft to a lower surface upon which the aircraft is at rest where the egress is located near an aircraft wing, comprising: a fluid distensible beam structure generally including five beam sections in fluid communication with each other to form a generally pentagonal beam structure; a sliding surface operably affixed to the generally pentagonal fluid distensible beam structure; means to deploy the fluid distensible beam structure and sliding surface from the elevated egress to have a portion of the pentagonal beam structure supported by the aircraft wing and one of the five pentagonal beam sections disposed on the lower surface upon which the aircraft is at rest.
Claim 2
Dependent Claim
118 words
Inflatable slide apparatus for evacuation from an elevated egress of an aircraft to a lower surface upon which the aircraft is at rest where the egress is located near an aircraft wing, comprising: a fluid distensible beam structure generally including five beam sections in fluid communication with each other to form a generally pentagonal beam structure; a sliding surface operably affixed to the generally pentagonal fluid distensible beam structure; means to deploy the fluid distensible beam structure and sliding surface from the elevated egress to have a portion of the pentagonal beam structure supported by the aircraft wing and one of the five pentagonal beam sections disposed on the lower surface upon which the aircraft is at rest.
Claim 3
Dependent Claim
174 words
Inflatable slide apparatus for evacuation from an elevated egress of an aircraft to a lower surface upon which the aircraft is at rest where the egress is located near an aircraft wing, comprising: a fluid distensible beam structure generally including five beam sections in fluid communication with each other to form a generally pentagonal shaped beam structure, a first beam section disposed adjacent the elevated egress and operably connected thereto, a second beam section extending outward from the elevated egress to the aircraft wing, a third beam section disposed on the lower surface upon which the aircraft is at rest, a fourth beam section extending from the second beam section to the third beam section, and a fifth beam section extending between the first beam section and the third beam section; a sliding surface operably affixed to the generally pentagonal shaped fluid distensible beam structure; means to deploy the fluid distensible beam structure and sliding surface from the elevated egress to have a portion of the pentagonal beam structure supported by the aircraft wing.
Claim 4
Dependent Claim
174 words
Inflatable slide apparatus for evacuation from an elevated egress of an aircraft to a lower surface upon which the aircraft is at rest where the egress is located near an aircraft wing, comprising: a fluid distensible beam structure generally including five beam sections in fluid communication with each other to form a generally pentagonal shaped beam structure, a first beam section disposed adjacent the elevated egress and operably connected thereto, a second beam section extending outward from the elevated egress to the aircraft wing, a third beam section disposed on the lower surface upon which the aircraft is at rest, a fourth beam section extending from the second beam section to the third beam section, and a fifth beam section extending between the first beam section and the third beam section; a sliding surface operably affixed to the generally pentagonal shaped fluid distensible beam structure; means to deploy the fluid distensible beam structure and sliding surface from the elevated egress to have a portion of the pentagonal beam structure supported by the aircraft wing.
Claim 5
Dependent Claim
214 words
Inflatable slide apparatus for evacuation from an elevated egress of an aircraft to a lower surface upon which the aircraft is at rest where the egress is located near an aircraft wing, comprising: a fluid distensible member of a generally elongate configuration when fully inflated, disposed in an uninflated, folded configuration at the elevated egress with one end secured thereto, said member generally comprising a generally pentagonal shaped fluid distensible beam having a sliding surface operably affixed thereto, said pentagonal shaped fluid distensible beam having five beam sections in fluid communication with each other, including, when inflated, a sill beam section disposed at the elevated egress and operably secured thereto, a wing beam section extending outward from one end of the sill beam section to the aircraft wing, a bottom beam section disposed on the lower surface upon which the aircraft is at rest, an inboard longitudinal beam section extending from the other end of the sill beam section to the inboard end of the bottom beam section, and an outboard longitudinal beam section extending from the wing beam section to the outboard end of the bottom beam section; means to deploy the fluid distensible member from the elevated egress to have a portion of the pentagonal beam structure supported by the aircraft wing.
Claim 6
Dependent Claim
214 words
Inflatable slide apparatus for evacuation from an elevated egress of an aircraft to a lower surface upon which the aircraft is at rest where the egress is located near an aircraft wing, comprising: a fluid distensible member of a generally elongate configuration when fully inflated, disposed in an uninflated, folded configuration at the elevated egress with one end secured thereto, said member generally comprising a generally pentagonal shaped fluid distensible beam having a sliding surface operably affixed thereto, said pentagonal shaped fluid distensible beam having five beam sections in fluid communication with each other, including, when inflated, a sill beam section disposed at the elevated egress and operably secured thereto, a wing beam section extending outward from one end of the sill beam section to the aircraft wing, a bottom beam section disposed on the lower surface upon which the aircraft is at rest, an inboard longitudinal beam section extending from the other end of the sill beam section to the inboard end of the bottom beam section, and an outboard longitudinal beam section extending from the wing beam section to the outboard end of the bottom beam section; means to deploy the fluid distensible member from the elevated egress to have a portion of the pentagonal beam structure supported by the aircraft wing.
Claim 7
Dependent Claim
46 words
The inflatable slide apparatus of claim 3 wherein said means to deploy the fluid distensible member from the elevated egress include means to delay the extension of the inboard and outboard longitudinal beam sections until the wing beam section is fully extended over the aircraft wing.
Claim 8
Independent Claim
89 words
A method of deploying an elongate inflatable evacuation slide from an elevated egress of an aircraft where the egress is situated near an aircraft wing, comprising the steps of: storing a generally five-sided evacuation slide in a folded, uninflated configuration at the elevated egress; attaching one end of the folded, uninflated, slide to the elevated egress; inflating the evacuation slide from the elevated egress, and providing means on the evacuation slide to sequentially unfold the slide to support a portion of the inflated evacuation slide on the aircraft wing.
Claim 9
Independent Claim
89 words
A method of deploying an elongate inflatable evacuation slide from an elevated egress of an aircraft where the egress is situated near an aircraft wing, comprising the steps of: storing a generally five-sided evacuation slide in a folded, uninflated configuration at the elevated egress; attaching one end of the folded, uninflated, slide to the elevated egress; inflating the evacuation slide from the elevated egress, and providing means on the evacuation slide to sequentially unfold the slide to support a portion of the inflated evacuation slide on the aircraft wing.
Claim 10
Independent Claim
135 words
A method of deploying an elongate inflatable evacuation slide from an elevated egress of an aircraft where the egress is situated near an aircraft wing, comprising the steps of: storing a generally pentagonal evacuation slide in a folded, uninflated configuration at the elevated egress, the evacuation slide generally comprising a fluid distensible beam having five beam sections in fluid communication with each other and a sliding surface operably affixed thereto, one section of the fluid distensible beam adapted to be disposed on the aircraft wing; attaching one end of the folded, uninflated, slide to the elevated egress; inflating the evacuation slide from the elevated egress, and providing means on the evacuation slide to restrain deployment of the other end of the slide until the one section of the slide is disposed over the aircraft wing.
Claim 11
Independent Claim
135 words
A method of deploying an elongate inflatable evacuation slide from an elevated egress of an aircraft where the egress is situated near an aircraft wing, comprising the steps of: storing a generally pentagonal evacuation slide in a folded, uninflated configuration at the elevated egress, the evacuation slide generally comprising a fluid distensible beam having five beam sections in fluid communication with each other and a sliding surface operably affixed thereto, one section of the fluid distensible beam adapted to be disposed on the aircraft wing; attaching one end of the folded, uninflated, slide to the elevated egress; inflating the evacuation slide from the elevated egress, and providing means on the evacuation slide to restrain deployment of the other end of the slide until the one section of the slide is disposed over the aircraft wing.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1979-08-10 | 1980-02-09 | 1980-08-10 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-08-10 | 1984-02-09 | 1984-08-10 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-08-10 | 1988-02-09 | 1988-08-10 | $7700.00 | Window Closed / Lapsed |