Flame-out resistant fuel pumping system
AssigneeColtec Industries Inc.
InventorsBernard J. Bisson, George L. Bennett
Life of this patent
Estimating the term…
Abstract
The fuel pumping system for delivering fuel to an engine includes a fuel transfer circuit for directing fuel from a fuel supply tank to the engine, a fuel boost pump, a main fuel pump and an accumulator device positioned along the transfer circuit between the boost pump and the engine for accumulating fuel and vapor so as to provide a reserve supply of fuel to the engine while minimizing the amount of undissolved vapor delivered to the engine. The system includes a return passage communicating, at one end, with the accumulator and at an opposite end with the fuel transfer circuit upstream of the boost pump for directing fuel and vapor from the accumulator into the transfer circuit.
Claims20
A fuel pumping system for delivering fuel to an engine, comprising:
- a fuel supply tank for supplying fuel to be delivered to the engine;
- a fuel transfer circuit for directing fuel from said fuel supply tank to the engine;
- a fuel boost pump positioned along said fuel transfer circuit between said fuel supply tank and the engine for displacing fuel through said fuel transfer circuit from said fuel supply tank toward the engine, said fuel boost pump including a pump inlet and a pump discharge outlet;
- an accumulator means positioned along said fuel transfer circuit between said pump discharge outlet and the engine for accumulating vapor and fuel so as to provide a reserve supply of fuel to the engine while minimizing the amount of undissolved vapor delivered to the engine;
- and a return conduit having an inlet end communicating with said accumulator means and an outlet end communicating with said fuel transfer circuit between said fuel supply tank and said accumulator means, said return conduit operating to direct vapor or vapor and fuel from said accumulator means into said fuel transfer circuit.
A fuel pumping system for delivering fuel to an engine comprising:
- a fuel supply tank for supplying fuel to be delivered to the engine;
- a fuel transfer circuit for directing fuel from said fuel supply tank to the engine;
- a fuel boost pump positioned along said fuel transfer circuit between said fuel supply tank and the engine for displacing fuel through said fuel transfer circuit from said fuel supply tank toward the engine, said fuel boost pump being a self-priming, centrifugal-type pump capable of pumping liquid and vapor and including it pump inlet and a pump discharge outlet;
- an accumulator means positioned along said fuel transfer circuit between said pump discharge outlet and the engine for accumulating vapor and fuel so as to provide a reserve supply of fuel to the engine while minimizing the amount of undissolved vapor delivered to the engine, said accumulator means including an accumulator inlet for directing fuel and vapor into said accumulator means from said pump discharge outlet, a first accumulator outlet for discharging fuel from said accumulator means through said fuel transfer circuit to the engine, and a second accumulator outlet for allowing fuel and vapor to exit from said accumulator means;
- and
- a return passage having an inlet end communicating with said second accumulator outlet and an outlet end communicating with said fuel transfer circuit upstream of said pump discharge outlet for directing fuel and vapor from said accumulator means into said fuel transfer circuit.
A fuel pumping system for pumping fuel from a fuel-supply tank to an aircraft engine while preventing flame-out of the aircraft engine due to accumulated vapor, comprising:
- a fuel flow conduit for directing fuel from said fuel supply tank to the aircraft engine;
- a fuel boost pump positioned along said fuel flow conduit for displacing fuel from said supply tank through said fuel flow circuit toward the aircraft engine;
- an accumulator container positioned along said fuel flow conduit between said boost pump and the aircraft engine, said accumulator container including an upper vapor storage portion for accumulating vapor, a fuel storage portion below said vapor storage portion for accumulating liquid fuel during normal operation of the fuel pumping system, an accumulator inlet passage for directing liquid fuel and vapor from said boost pump into said accumulator container, a first accumulator outlet passage connected to said first storage portion for directing liquid fuel into said fuel flow conduit toward the aircraft engine, and a second accumulator outlet passage connected to said vapor storage portion for discharging fuel and vapor from said accumulator container;
- and a return passage having an inlet end connected to said second accumulator outlet passage and an outlet end communicating with said fuel flow conduit between said fuel supply tank and said accumulator inlet passage, said return passage operating to direct vapor and fuel from said accumulator container into said fuel flow conduit.
Dependencies are inferred from the claim text.