Patent US3338404A successfully refreshed from Google Patents.
← Back to Patent Explorer
US3846090A Expired / Lapsed US ⏱️ 0.0 years remaining

Control of liquid dissemination

Assignee: Imperial Chemical Industries Ltd
•
Filing: 1972-05-12
•
Granted: 1974-11-05
•
Expires: 1992-05-12
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract 1. A LIQUID HYDROCARBON FUEL OF FLASH POINT AT LEAST 90* F. AND SUITABLE FOR USE IN GAS TURBINED ENGINED AIRCRAFT, HAVING A REDUCED TENDENCY TO PARTICULATE DISSEMINATION ON BEING SUBJECTED TO SHOCK THE FUEL CONTAINING DISSOLVED THEREIN POLYMER OF MOLECULAR WEIGHT GREATER THAN 10**6 (VISCOSITY AVERAGE) OR OF INTRINSIC VISCOSITY GREATER THAN 2.5 DLS./GM. IN A CONCENTRATION SUCH THAT THERE IS MOLECULAR OVERLAP OF THE POLYMER MOLECULES IN THE LIQUID THE POLYMER BEING AN ADDITION HOMOPOLYMER OF AN ALKYL STYRENE OR AN ADDITION HOMOPOLYMER OF AN ALKYL ONE OR MORE ETHYLENICALLY UNSATURATED NON-POLR MONOMERS COPOLYMERIZABLE WITH SAID ALKYL STYRENE.

Inventors

  • 👤 F Waite
  • 👤 D Osmond
  • 👤 N Smith

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 03:47
CPC Classifications
C; C10; C10L; C10L1/00; C10L1/10; C10L1/14; C10L1/146; C10L1/16; C10L1/1625; C10L1/1633; C10L1/165; C10L1/18; C10L1/192; C10L1/195; C10L1/196; C10L1/1963

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 99 words
A LIQUID HYDROCARBON FUEL OF FLASH POINT AT LEAST 90* F. AND SUITABLE FOR USE IN GAS TURBINED ENGINED AIRCRAFT, HAVING A REDUCED TENDENCY TO PARTICULATE DISSEMINATION ON BEING SUBJECTED TO SHOCK THE FUEL CONTAINING DISSOLVED THEREIN POLYMER OF MOLECULAR WEIGHT GREATER THAN 10**6 (VISCOSITY AVERAGE) OR OF INTRINSIC VISCOSITY GREATER THAN 2.5 DLS./GM. IN A CONCENTRATION SUCH THAT THERE IS MOLECULAR OVERLAP OF THE POLYMER MOLECULES IN THE LIQUID THE POLYMER BEING AN ADDITION HOMOPOLYMER OF AN ALKYL STYRENE OR AN ADDITION HOMOPOLYMER OF AN ALKYL ONE OR MORE ETHYLENICALLY UNSATURATED NON-POLR MONOMERS COPOLYMERIZABLE WITH SAID ALKYL STYRENE.
Claim 2
Dependent Claim 99 words
A LIQUID HYDROCARBON FUEL OF FLASH POINT AT LEAST 90* F. AND SUITABLE FOR USE IN GAS TURBINED ENGINED AIRCRAFT, HAVING A REDUCED TENDENCY TO PARTICULATE DISSEMINATION ON BEING SUBJECTED TO SHOCK THE FUEL CONTAINING DISSOLVED THEREIN POLYMER OF MOLECULAR WEIGHT GREATER THAN 10**6 (VISCOSITY AVERAGE) OR OF INTRINSIC VISCOSITY GREATER THAN 2.5 DLS./GM. IN A CONCENTRATION SUCH THAT THERE IS MOLECULAR OVERLAP OF THE POLYMER MOLECULES IN THE LIQUID THE POLYMER BEING AN ADDITION HOMOPOLYMER OF AN ALKYL STYRENE OR AN ADDITION HOMOPOLYMER OF AN ALKYL ONE OR MORE ETHYLENICALLY UNSATURATED NON-POLR MONOMERS COPOLYMERIZABLE WITH SAID ALKYL STYRENE.

References Cited (Backward Citations)

No citation records indexed.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1977-11-04 1978-05-06 1978-11-05 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1981-11-04 1982-05-06 1982-11-05 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1985-11-04 1986-05-06 1986-11-05 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag