Aspirated relief valve for a turbocharging system

Patent metadata

Field	Value
Publication number	US-10167971-B2
Application number	US-201715646911-A
Country	US
Kind code	B2
Filing date	Jul 11, 2017
Priority date	Jul 17, 2014
Publication date	Jan 1, 2019
Grant date	Jan 1, 2019

Abstract

Engine systems have an air induction system, a turbocharger in fluid communication with an intake manifold, an evacuator defining a Venturi gap with a suction port in fluid communication therewith, a relief valve enclosing a piston and defining an inlet and an outlet in selective fluid communication with one another, and a storage tank of high pressure air in fluid communication with the evacuator. The relief valve has a valve element connected to the piston, and the piston divides the housing into a pressurized chamber in fluid communication with the suction port of the evacuator and a bypass portion in fluid communication with the inlet, which is in fluid communication with the compressed air from the turbocharger, and the outlet, which is in fluid communication with the air induction system or atmosphere. A discharge cone of the evacuator is in fluid communication with atmosphere or the air induction system.

First claim

What is claimed is:

1. An engine system comprising:
an air induction system;
a turbocharger receiving air from the air induction system, wherein the turbocharger is in fluid communication with a throttle and an intake manifold of an engine to send compressed air thereto;
an evacuator having a motive cone, a discharge cone, and a suction port, wherein a motive outlet end of the motive cone faces a discharge inlet of the discharge cone to define a Venturi gap in fluid communication with the suction port;
a relief valve having a housing enclosing a piston, the housing defining an inlet and an outlet in selective fluid communication with one another controlled by the movement of the piston and a valve element connected to the piston, wherein the piston divides the housing into a pressurized chamber in fluid communication with the suction port of the evacuator and a bypass portion opposite the pressurized chamber, the bypass portion being in fluid communication with the inlet and the outlet of the relief valve, and wherein the inlet of the relief valve is in fluid communication with the compressed air from the turbocharger upstream of the throttle and the outlet of the relief valve is in fluid communication with the air induction system or atmosphere; and
a storage tank of high pressure air in fluid communication with the evacuator for high pressure air to flow through the evacuator from the motive cone to the discharge cone, thereby creating vacuum acting on the pressurized chamber of the relief valve to move the piston between the closed position and the open position;
wherein the discharge cone of the evacuator is in fluid communication with atmosphere or the air induction system upstream of the turbocharger.

2. The system of claim 1 , wherein the relief valve is a variable valve adjustable for an amount of bypass between the open position and the closed position to prevent compressor surge of the turbocharger.

3. The system of claim 1 , further comprising a control valve fluidly connected to the storage tank, wherein the control valve selectively allows high pressure air from the storage tank to flow through the evacuator.

4. The system of claim 3 , wherein the control valve is a solenoid valve.

5. The system of claim 3 , wherein the control valve has a normally closed position.

6. The system of claim 3 , further comprising a controller in signal communication with the control valve, wherein the controller monitors operating parameters of the system and determines when to send a control signal to open or close the control valve.

7. The system of claim 6 , wherein the relief valve further comprises a position sensor detecting a position of the piston within the housing, the position sensor being in signal communication with the controller.

8. The system of claim 1 , wherein a first end of the piston defines a surface of the pressurized chamber and the second end of the piston defines a surface of the bypass chamber, and the second end of the piston is acted upon by forces from the compressed air from the turbocharger when the relief valve is in the open position.

9. The system of claim 1 , wherein the valve element is a poppet valve.

10. The system of claim 1 , wherein the relief valve further comprises a biasing element in the pressurized chamber abutted against the piston to exert a biasing force toward the closed position.

11. The system of claim 10 , wherein the biasing element is a compression spring.

12. The system of claim 1 , further comprising a noise attenuator in fluid communication with the evacuator downstream of the evacuator.

Assignees

• Fletcher David E
• Graichen Brian M
• Miller James H
• Hampton Keith
• Gilmer Matthew C
• Dayco Ip Holdings Llc

Inventors

• Fletcher David E
• Graichen Brian M
• Miller James H
• Hampton Keith
• Gilmer Matthew C

Classifications

• F16K24/04 Primary

  for venting only (F16K24/02 takes precedence) · CPC title

• F02M35/10157

  Supercharged engines · CPC title

• F02B2037/125

  Control for avoiding pump stall or surge · CPC title

• F16K37/0033

  using a permanent magnet, e.g. in combination with a reed relays · CPC title

• F02B37/18

  by bypassing exhaust {from the inlet to the outlet of turbine or to the atmosphere} · CPC title