FIELD: chemistry.
SUBSTANCE: additive represents solution of highly-molecular polyisobutylene, which has molecular weight from, approximately 3.7·106 to, approximately 4.9·106, in used hydrocarbon liquid. Hydrocarbon liquid for machines with hydraulic systems with thermo- and/or energy-strained operation conditions contains additive in amount, ensuring energy characteristics of said machines. Mainly, hydrocarbon liquid represents kerosene or aviation spirit or Diesel fuel or liquid jet fuel. Liquid hydrocarbon fuel for jet engines contains additive in amount ensuring concentration of highly-molecular polyisobutylene in liquid hydrocarbon fuel from 0.015 to 0.095 wt %.
EFFECT: improvement of operating energy characteristics of machines, efficiency of engines, pump force.
8 cl, 1 tbl, 11 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR PRODUCING ANTITURBULENT ADDITIVE FOR HYDROCARBON ROCKET PROPELLANTS | 2015 |
|
RU2612135C1 |
METHOD OF INCREASING ENERGY CHARACTERISTICS OF LIQUID ROCKET ENGINES | 2013 |
|
RU2527918C1 |
UNIT FOR HYDROCARBON ROCKET FUEL RESEARCH | 2018 |
|
RU2664443C1 |
NANO-COMPONENT ENERGY SUPPLEMENT AND LIQUID HYDROCARBON FUEL | 2013 |
|
RU2529035C1 |
METHOD OF TRANSPORTATION OF NON-NEWTONIAN PARAFFIN-CONTAINING HYDROCARBON FLUID VIA PIPE LINE | 1998 |
|
RU2124160C1 |
OPERATION OF OXYGEN-KEROSENE LIQUID ROCKET ENGINE AND ROCKET ENGINE PLANT | 2013 |
|
RU2542623C1 |
LIQUID HYDROCARBON FUEL COMPOSITION AND METHOD OF MODIFYING LIQUID HYDROCARBON FUELS | 1997 |
|
RU2165446C2 |
METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE AT TURBOPUMP DELIVERY OF OXYGEN-METHANE PROPELLANT | 1999 |
|
RU2166661C1 |
ANTI-TURBULENT ADDITIVE AND METHOD OF REDUCING PIPE FRICTION LOSSES | 2014 |
|
RU2562611C2 |
ANTITURBULENT ADDITIVES FOR REDUCING HYDRODYNAMIC DRAG OF HYDROCARBON LIQUIDS IN PIPELINES AND METHOD FOR THEIR PRODUCING | 2015 |
|
RU2639301C2 |
Authors
Dates
2009-01-10—Published
2006-08-15—Filed