Patent AT17085B successfully refreshed from Google Patents.
← Back to Patent Explorer
US4012012A Expired / Lapsed US ⏱️ 0.0 years remaining

Supplemental oil system for engines

Assignee: Lockheed Martin Corp
•
Filing: 1975-10-30
•
Granted: 1977-03-15
•
Expires: 1995-10-30
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract An oil replenishment system provides a remote reserve oil tank and the plumbing necessary to fill the main oil tank or tanks of engines, especially aircraft engines during flight. This system includes apparatus to determine the quantity of oil pumped to any one engine so that a quantity gauge is not required on the engine. A selector valve located on the reserve tank which may be remotely controlled directs replenishment oil to the selected engine tank. The system is designed to be powered from the existing on board hydraulic power system.

Inventors

  • 👤 George E. Ligler

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-25 13:09
CPC Classifications
B; B64; B64D; B64D33/00; F; F16; F16N; F16N7/00; F16N7/38; F16N7/385

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 149 words
The combination with an airplane having a wing with multiple turbo-jet engines and each having an associated main oil tank mounted thereon, of a supplemental oil system to replenish oil in each main oil tank, said system comprising: a reserve tank of oil located internally of said airplane; a pipeline connecting said reserve tank to each said main tank; a container having a measured capacity less than that of said reserve tank located in said pipeline; valving in said pipeline operable to permit the flow of oil from said reserve tank to said container and a distribution valve to control the flow of oil from said container to a selected one of said main tanks; and a force pump to assure the flow of oil from said reserve tank to said container and to each said main tank when free to do so upon the operation of said valving.
Claim 2
Dependent Claim 149 words
The combination with an airplane having a wing with multiple turbo-jet engines and each having an associated main oil tank mounted thereon, of a supplemental oil system to replenish oil in each main oil tank, said system comprising: a reserve tank of oil located internally of said airplane; a pipeline connecting said reserve tank to each said main tank; a container having a measured capacity less than that of said reserve tank located in said pipeline; valving in said pipeline operable to permit the flow of oil from said reserve tank to said container and a distribution valve to control the flow of oil from said container to a selected one of said main tanks; and a force pump to assure the flow of oil from said reserve tank to said container and to each said main tank when free to do so upon the operation of said valving.
Claim 3
Dependent Claim 22 words
The supplemental oil system of claim 1 wherein said reserve tank has a filler opening accessible from the interior of said airplane.
Claim 4
Dependent Claim 33 words
The supplemental oil system of claim 1 including a control panel located proximate said reserve tank and connections between said panel and said valving for the operation of the latter from the former.
Claim 5
Dependent Claim 32 words
The supplemental oil system of claim 1 wherein said container is a cylinder and said force pump is a piston operable in said cylinder under the power of a reciprocating differential motor.
Claim 6
Dependent Claim 29 words
The supplemental oil system of claim 4 wherein said reciprocating differential motor is a hydraulic cylinder controlled by valve means located between it and a source of fluid pressure.
Claim 7
Dependent Claim 34 words
The supplemental oil system of claim 4 including a signal generating contact at opposite ends of said cylinder engageable by said piston to thereby indicate the location of said piston at each cylinder end.

References Cited (Backward Citations)

US2509426A Cited
US2557438A Cited
US2617495A Cited
US3052317A Cited
US3076478A Cited
US3096043A Cited
US3096788A Cited
DE1506114A1 Cited
US3500962A Cited
US3838624A Cited
US3876037A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-03-14 1980-09-13 1981-03-15 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-03-14 1984-09-13 1985-03-15 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-03-14 1988-09-13 1989-03-15 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag