Centrifugal turbo machine having stretchable and variable diffuser vane

Patent metadata

Field	Value
Publication number	US-10352188-B2
Application number	US-201715696331-A
Country	US
Kind code	B2
Filing date	Sep 6, 2017
Priority date	Mar 28, 2017
Publication date	Jul 16, 2019
Grant date	Jul 16, 2019

Abstract

The present disclosure is relates to a centrifugal turbo machine equipped with stretchable and variable diffuser vanes capable of securing further improvement of compression efficiency by reducing an angle of the vane and increasing a length of the vane using forced rotating driving of a diffuser during operation of a compressor so as to reduce frictional loss of the fluid when a flow rate of fluid is reduced.

First claim

What is claimed is:

1. A centrifugal turbo machine having stretchable and variable diffuser vanes, comprising;
an impeller including a hub and a plurality of blades and rotatably installed at a center of an interior of a casing;
a diffuser provided on an outer side of the impeller and configured to convert kinetic energy of fluid increased by rotation of the impeller into static pressure;
a rotating ring section provided on and configured to face an outer side of the diffuser in a ring shape and configured to be rotatable about the impeller;
a plurality of vanes disposed between an inlet side and an outlet side of the diffuser with respect to a flow of fluid, spaced apart from each other in a circumferential direction to define flow paths therebetween, and each configured to adjust an angle thereof to change an area of the flow path according to a moving direction of the vane; and
a power transmitting section configured to generate power and transmit the power to the rotating ring section so that the rotating ring section is rotated about the impeller,
wherein the vane comprises two hinge shafts formed at both ends thereof and a connecting portion connecting the hinge shafts, and at least a part of the connecting portion is made of a ductile material so that a length of the connecting portion elastically varies.

2. The centrifugal turbo machine of claim 1 , wherein the connecting portion has a closed loop structure that is elastically wound around the hinge shafts.

3. The centrifugal turbo machine of claim 1 , wherein the vane further comprises a spacer inserted between and fixed to opposite sides of the connecting portion to uniformly maintain a distance between the opposite sides of the connecting portion.

4. The centrifugal turbo machine of claim 1 , wherein one hinge shaft of the hinge shafts is rotatably fixed to the inlet side of the diffuser, and the other hinge shaft is rotatably fixed to the rotating ring section.

5. The centrifugal turbo machine of claim 1 , wherein the power transmitting section comprises:
a step motor;
a first element provided on a motor shaft of the step motor;
a second element installed at one side of the rotating ring section and engaged with the first element to provide the rotating ring section with rotational power through an interaction with the first element; and
a controller configured to control driving of the step motor.

6. The centrifugal turbo machine of claim 5 , wherein the first element includes a pinion gear and the second element includes a rack gear.

Assignees

• Korea Inst Sci & Tech

Inventors

• Shin You Hwan
• Park Joo Hoon
• Kim Young Soo

Classifications

• F01D17/165 Primary

  for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line (F01D17/167 takes precedence) · CPC title

• F01D5/04

  for radial-flow machines or engines · CPC title

• F01D17/24

  electrical · CPC title

• F16H19/04

  comprising a rack · CPC title

• F04D29/46

  adjustable · CPC title