Patent US5669850A successfully refreshed from Google Patents.
US3592145A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Force-carrying interlock for aluminum extruded platform
Assignee: United States Department of the Air Force
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Filing: 1969-08-15
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Granted: 1971-07-13
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Expires: 1989-08-15
Abstract
Abstract An aircraft cargo delivery pallet comprising a plurality of elongated flat extruded lightweight metallic panels interlocked together along their longitudinal edges and having a plurality of spaced elongated metallic skid strips secured transversely across the bottom surfaces of the panels adjacent their interlocking edges in parallel relation to each other, holding the panels in substantially predetermined relative flat interlocking edge-toedge relation and elongated side rails secured to the panels across the opposite ends thereof.
Inventors
- 👤 Gene A Petry
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 23:43
CPC Classifications
B; B64; B64D; B64D9/00; B65; B65D; B65D19/00; B65D19/0002
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
274 words
An assembled aircraft cargo delivery pallet comprising; a plurality of identical elongated rectangular panel members; complementary interengaging coupling means formed on the opposite bottom longitudinal edges of each of said panel members for connecting the said bottom longitudinal edges of the panel members together against separation; identical abutment means formed on the opposite upper longitudinal edge portions of said panel members for abutting engagement therebetween for resisting upward angular movement between adjacent panel members in said pallet around said coupling means; a plurality of elongated skid rails extending transversely across the bottom surfaces of said panel members between the opposite ends of said pallet; means rigidly securing said skid rails to the bottom of said pallet adjacent said interengaging coupling means; and elongated side rails rigidly secured to the opposite ends of the panel members, extending between the opposite longitudinal ends of said pallet, for resisting relative longitudinal and vertical movements between said panel members, when said pallet is withdrawn and dropped to the ground from a low-flying cargo aircraft; each of said panel members comprising extruded hollow lightweight metallic material having spaced parallel top and bottom surfaces, and spaced perpendicular side portions formed with internal truss web brace members therebetween; said complementary interengaging coupling means comprising an extruded upwardly extending tongue member formed along the lower edge portion of one side of each panel member and a complementary upwardly extending longitudinal groove formed in the bottom portion of the other side of each panel member, and identical longitudinal abutment members extruded with the panel members and projecting outwardly from the top edge portions of both of the side edges of the panel members.
Claim 2
Dependent Claim
274 words
An assembled aircraft cargo delivery pallet comprising; a plurality of identical elongated rectangular panel members; complementary interengaging coupling means formed on the opposite bottom longitudinal edges of each of said panel members for connecting the said bottom longitudinal edges of the panel members together against separation; identical abutment means formed on the opposite upper longitudinal edge portions of said panel members for abutting engagement therebetween for resisting upward angular movement between adjacent panel members in said pallet around said coupling means; a plurality of elongated skid rails extending transversely across the bottom surfaces of said panel members between the opposite ends of said pallet; means rigidly securing said skid rails to the bottom of said pallet adjacent said interengaging coupling means; and elongated side rails rigidly secured to the opposite ends of the panel members, extending between the opposite longitudinal ends of said pallet, for resisting relative longitudinal and vertical movements between said panel members, when said pallet is withdrawn and dropped to the ground from a low-flying cargo aircraft; each of said panel members comprising extruded hollow lightweight metallic material having spaced parallel top and bottom surfaces, and spaced perpendicular side portions formed with internal truss web brace members therebetween; said complementary interengaging coupling means comprising an extruded upwardly extending tongue member formed along the lower edge portion of one side of each panel member and a complementary upwardly extending longitudinal groove formed in the bottom portion of the other side of each panel member, and identical longitudinal abutment members extruded with the panel members and projecting outwardly from the top edge portions of both of the side edges of the panel members.
Claim 3
Dependent Claim
176 words
An assembled aircraft cargo delivery pallet as in claim 1, in which said truss web brace members are extruded with the panel members and further extend within the panel members in uniform zigzag relation between the top and bottom panel surfaces from one longitudinal side of the panel members to the opposite side thereof; said complementary interengaging coupling means comprises a vertical upstanding longitudinal tongue located adjacent to the lower surface of each of the panel members in offset spaced relation from the panel member sidewall to leave an upwardly extending longitudinal channel between said tongue and the adjacent side of each of the panel members; said tongue-receiving groove in the bottom portion of the other side of each panel member extends upwardly above the bottom of the panel member in predetermined inwardly spaced relation from the adjacent side of the panel member to receive the tongue member therein, and includes a downwardly extending longitudinally interlocking rib dimensioned to fit between the upwardly extending tongue member and the adjacent side of each of the panel members.
Claim 4
Dependent Claim
76 words
An assembled aircraft cargo delivery pallet as in claim 2, in which each of said elongated extruded panel members includes end closure plates secured in the opposite ends of each of the panel members and extending between the opposite Sides of the said panel members, and further including interengaging means between said elongated side rails and said closure plates; and means for rigidly securing said side rails to said end closure plates in said interengaging relation.
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) | 1974-07-12 | 1975-01-11 | 1975-07-13 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1978-07-12 | 1979-01-11 | 1979-07-13 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1982-07-12 | 1983-01-11 | 1983-07-13 | $7700.00 | Window Closed / Lapsed |