Integrated turbo-compressor with variable gear ratio transmission for internal combustion engine

Patent metadata

Field	Value
Publication number	US-11060449-B2
Application number	US-201916431084-A
Country	US
Kind code	B2
Filing date	Jun 4, 2019
Priority date	Jun 4, 2019
Publication date	Jul 13, 2021
Grant date	Jul 13, 2021

Abstract

An integrated turbo-compressor includes a compressor with a compressor outlet, a turbine with a turbine inlet, the turbine operatively connected to the compressor by an interconnect shaft, and a compounding drive. The compounding drive is connected to the turbine and has a variable gear ratio and an output member, the variable gear ratio coupling the turbine to the output member to compound output of an internal combustion engine using energy recovered from an exhaust flow received from the internal combustion engine and in excess of energy required to compress combustion air provided to the internal combustion engine. Internal combustion engines, aircraft, and methods of compounding output of internal combustion engines are also described.

First claim

What is claimed is:

1. An internal combustion engine, comprising:
an engine body supporting an engine output shaft and having a combustion air intake port and an exhaust port; and
an integrated turbo-compressor, comprising:
a compressor with a compressor outlet;
a turbine with a turbine inlet,
the turbine operatively connected to the compressor by an interconnect shaft; and
a compounding drive connected to the turbine and having a variable gear ratio and an output member,
wherein the variable gear ratio couples the turbine to the output member to compound output of the internal combustion engine using energy recovered from an exhaust flow received from the internal combustion engine,

wherein the compounding drive comprises:
an input member connected to the turbine;
the output member connected to the input member; and
an intermediate member connecting the input member to the output member through an epicyclical gear arrangement and a hydraulic pump/motor set;

wherein the compressor outlet is connected to the combustion air intake port,
wherein the turbine inlet is connected to the engine exhaust port, and
wherein an electric motor and battery arrangement is operatively connected to the engine output shaft in a hybrid-electric turbo-compounded engine arrangement, and
wherein;
the hydraulic pump/motor set comprises: a fixed displacement hydraulic module, wherein the input member operably connects the turbine to the fixed displacement hydraulic module; and a variable displacement hydraulic module in fluid communication with the fixed displacement hydraulic module via a hydraulic circuit, wherein the output member is operably connected to the hydraulic pump/motor set via the variable displacement hydraulic module, and wherein the variable displacement hydraulic module applies power through the output member according to a hydraulic fluid received through the hydraulic circuit; and
a controller operably connected to the hydraulic pump/motor set via the hydraulic circuit, wherein the controller is configured to throttle flow of the hydraulic fluid through the hydraulic circuit, to present rotation resistance to the input member via the epicyclical gear arrangement so that the output member rotates at a speed of the output shaft, to thereby match a compounding drive speed to the speed of the output shaft, whereby manipulation of hydraulic fluid flow through the hydraulic circuit, in cooperation with the epicyclical gear arrangement, provides a variable gear ratio for compounding the internal combine engine utilizing the turbine.

2. The engine of claim 1 , wherein
the epicyclical gear arrangement is arranged within a housing, the epicyclical gear arrangement comprising:
a sun gear first in rotation relative to the turbine;
a ring gear extending about the sun gear;
a plurality of planetary gears intermeshed with the sun gear and the ring gear; and
a planetary gear carrier supporting each of the planetary gears for rotation independent rotation relative to one another,
the planetary gear carrier fixed in rotation relative to the output member;
wherein the sun gear, the ring gear, and the planetary gear carrier are each supported for rotation relative to the housing.

3. The engine of claim 1 , wherein
the turbine has fixed turbomachinery geometry,
wherein the compressor has fixed turbomachinery geometry.

4. The engine of claim 1 , wherein
the internal combustion engine is a constant speed turbo-compounded engine or
wherein the internal combustion engine is a variable speed turbo-compounded engine.

5. An aircraft carrying the engine of claim 1 , wherein
the turbo-compressor is operably connected to a rotor.

6. A method of compounding output from an internal combustion engine,
internal combustion engine including:
an engine body supporting an engine output shaft and having a combustion air intake port and an exhaust port; and
an integrated turbo-compressor, comprising:
a compressor with a compressor outlet;
a turbine with a turbine inlet,
the turbine operatively connected to the compressor by an interconnect shaft; and
a compounding drive connected to the turbine and having a variable gear ratio and an output member,
wherein the variable gear ratio couples the turbine to the output member to compound output of the internal combustion engine using energy recovered from an exhaust flow received from the internal combustion engine,

wherein the compounding drive comprises:
an input member connected to the turbine;
the output member connected to the input member; and
an intermediate member connecting the input member to the output member through an epicyclical gear arrangement and a hydraulic pump/motor set;

wherein the compressor outlet is connected to the combustion air intake port,
wherein the turbine inlet is connected to the engine exhaust port, and
wherein an electric motor and battery arrangement is operatively connected to the engine output shaft in a hybrid-electric turbo-compounded engine arrangement;
the hydraulic pump/motor set includes: a fixed displacement hydraulic module, wherein the input member operably connects the turbine to the fixed displacement hydraulic module; and a variable displacement hydraulic module in fluid communication with the fixed displacement hydraulic module via a hydraulic circuit, wherein the output member is operably connected to the hydraulic pump/motor set via the variable displacement hydraulic module, and wherein the variable displacement hydraulic module applies power through the output member according to a hydraulic fluid received through the hydraulic circuit; and
a controller operably connected to the hydraulic pump/motor set via the hydraulic circuit, wherein the controller is configured to throttle flow of the hydraulic fluid through the hydraulic circuit, to present rotation resistance to the input member via the epicyclical gear arrangement so that the output member rotates at a speed of the output shaft, to thereby match a compounding drive speed to the speed of the output shaft, whereby manipulation of hydraulic fluid flow through the hydraulic circuit, in cooperation with the epicyclical gear arrangement, provides a variable gear ratio for compounding the internal combine engine utilizing the turbine; the method comprising:
receiving an engine exhaust flow from the internal combustion engine at the turbine inlet;
extracting work from the engine exhaust flow with the turbine;
applying a first extracted work portion to the compressor to compress a flow of combustion air for the internal combustion engine; and
applying second extracted work portion to the internal combustion engine to compound output of the internal combustion engine,
wherein applying the second portion of the extracted work includes varying the variable gear ratio while compounding the output of the internal combustion engine.

7. The method as recited in claim 6 , further comprising
varying the variable gear ratio of the compounding drive while rotating the engine output shaft of the internal combustion engine at a fixed rotational speed.

8. The method as recited in claim 6 , further comprising
varying the variable gear ratio of the compounding drive while varying rotational speed of the engine output shaft.

Assignees

• Hamilton Sundstrand Corp
• Hamilton Sunstrand Corp

Inventors

• Spierling Todd A
• Behling David S
• Lemmers Jr Glenn C
• Thomassin Jean

Classifications

• Y02T10/12

  Improving ICE efficiencies · CPC title

• H02K7/1815

  structurally associated with reciprocating piston engines (general aspects of generating sets, e.g. housing, F02B63/04) · CPC title

• F02B39/08

  Non-mechanical drives, e.g. fluid drives having variable gear ratio · CPC title

• F02B37/166

  the auxiliary apparatus being a combustion chamber, e.g. upstream of turbine · CPC title

• F16H3/728

  with means to change ratio in the mechanical gearing · CPC title