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US3570415A Expired / Lapsed US ⏱️ 0.0 years remaining

Track supported mounting device for aircraft

Assignee: Boeing Co
•
Filing: 1968-12-13
•
Granted: 1971-03-16
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Expires: 1988-12-13
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Abstract

Abstract A device for mounting payload units on a rail in airplanes. The base structure has an integral caliper-type configuration for slidable engagement about the head portion of a rail structure. A spring mounted plunger and associated actuating means, such as an eccentric, are carried by the device and upon actuation of the eccentric, the plunger will extend into a rail cutout or detent for securing the caliper engagement and thus locking the device to the rail. Upon further actuation of the eccentric the plunger will contract and unlock the device.

Inventors

  • 👤 Robert H Drinnon
  • 👤 Leo Huttas

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-31 22:17
CPC Classifications
B; B64; B64D; B64D9/00; B64D9/003; Y; Y02; Y02T; Y02T50/00; Y02T50/40

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 218 words
An aircraft floor mounting device for releasably anchoring payload units to a rail member which is provided with a substantial round head portion and spaced intervening slots, comprising: a. a body having two pair of integrally connected legs, each said pair of legs having opposed concave inner surfaces for attachingly complementing said round head portion of said rail member when engaged thereon; b. said body provided with a substantially vertically extending bore at a location between said two pair of legs; c. a plug member connected to a shaft; d. said plug member disposed between said two pair of legs with said shaft slidably engaged within said bore; e. a spring positioned next to said plug member for biasing said plug member into said slot; and f. a horizontally positioned member with eccentric means provided on said body, said eccentric means linked to said shaft so that partly rotational actuation of said member causes a movement to said shaft in a vertical direction whereby said plug, biased by said spring, plugs said intervening slot for locking said mounting device onto said rail and whereby upon continued rotation of said member said shaft moves in a vertical direction against said biased spring so that said plug moves out of said slot, thereby unlocking said mounting device from said rail.
Claim 2
Dependent Claim 218 words
An aircraft floor mounting device for releasably anchoring payload units to a rail member which is provided with a substantial round head portion and spaced intervening slots, comprising: a. a body having two pair of integrally connected legs, each said pair of legs having opposed concave inner surfaces for attachingly complementing said round head portion of said rail member when engaged thereon; b. said body provided with a substantially vertically extending bore at a location between said two pair of legs; c. a plug member connected to a shaft; d. said plug member disposed between said two pair of legs with said shaft slidably engaged within said bore; e. a spring positioned next to said plug member for biasing said plug member into said slot; and f. a horizontally positioned member with eccentric means provided on said body, said eccentric means linked to said shaft so that partly rotational actuation of said member causes a movement to said shaft in a vertical direction whereby said plug, biased by said spring, plugs said intervening slot for locking said mounting device onto said rail and whereby upon continued rotation of said member said shaft moves in a vertical direction against said biased spring so that said plug moves out of said slot, thereby unlocking said mounting device from said rail.
Claim 3
Dependent Claim 72 words
An aircraft floor mounting device for releasably anchoring payload units to a rail member which is provided with a substantial round head portion and spaced intervening slots as claimed in claim 11; wherein said eccentric means linked to said shaft comprises an offcenter pin and slot arrangement between said member and said shaft so that a full rotation of said member causes a reciprocating movement of said shaft and thereon connected plug.

References Cited (Backward Citations)

US2735377A Cited
US2422693A Cited
US2605064A Cited
US2625118A Cited
US3187686A Cited
US3306234A Cited
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US3478995A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1974-03-15 1974-09-14 1975-03-16 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1978-03-15 1978-09-14 1979-03-16 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1982-03-15 1982-09-14 1983-03-16 $7700.00 Window Closed / Lapsed

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