# US 8,465,260 B2 · Combination fan propeller structure

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- Number: US 8,465,260 B2
- Document ID: US8465260B2
- Status: Granted
- Kind: B2
- Application number: 12/710,313
- Filed: 2010-02-22
- Published: 2011-08-25
- Granted: 2013-06-18
- Earliest claimed: 2010-02-22
- Assignees: Beijing AVC Technology Research Center Co., Ltd.
- Applicants: Jen-Chieh Wu; Chiang-Han Chen
- Inventors: Jen-Chieh Wu; Chiang-Han Chen
- Web page: https://patentgrep.com/patent/US8465260B2

## CPC

- F04D 29/34: Blade mountings {(for axial flow compressors F04D29/322)}
- F04D 25/0613: {the electric motor being of the inside-out type, i.e. the rotor is arranged radially outside a central stator}
- F04D 29/329: {Details of the hub}
- F04D: NON-POSITIVE-DISPLACEMENT PUMPS (engine fuel-injection pumps F02M; ion pumps H01J41/12; electrodynamic pumps H02K44/02)

## Abstract

A combination fan propeller structure including a hub and at least one first blade assembly. The hub includes a top section and an annular section extending from the top section. The annular section has a free end distal from the top section. The first blade assembly has at least one connection section for connecting with the free end to form the fan propeller structure.

## Claims

### Claim 1

A combination fan propeller structure comprising:
a hub including a top section and an annular section extending from the top section, the annular section having a free end distal from the top section; and
at least one first blade assembly having at least one connection section, the connection section having a U-shaped channel in which the free end is complementarily inserted and received, wherein inner sides of the channel are complementarily fixedly connected with inner and outer sides of the free end for connecting with the free end to integrate the hub.

### Claim 2 (depends on 1)

The combination fan propeller structure as claimed in claim 1, wherein the first blade assembly includes a first wind guide section and a first extension section, the first extension section extending from the first wind guide section to connect with the connection section and conformably attach to the annular section.

### Claim 3 (depends on 2)

The combination fan propeller structure as claimed in claim 2, wherein the first wind guide section has two faces as two first wind guide faces, the first wind guide faces of each two adjacent first wind guide sections being positioned at different heights in an overlapping pattern.

### Claim 4 (depends on 1)

The combination fan propeller structure as claimed in claim 1, wherein the free end has at least one protrusion corresponding to the connection section for connecting with the connection section by means of insertion.

### Claim 5 (depends on 1)

The combination fan propeller structure as claimed in claim 1, wherein the channel has at least one protrusion extending from an inner side of the channel toward a center thereof for abutting against and fixing the free end.

### Claim 6 (depends on 5)

The combination fan propeller structure as claimed in claim 5, wherein the protrusions are symmetrically or asymmetrically arranged on an inner side of the channel.

### Claim 7 (depends on 6)

The combination fan propeller structure as claimed in claim 6, wherein the free end has at least one fixing hole formed on an inner circumference of the annular section, the protrusion of the channel being complementarily fixedly inserted in the fixing hole.

### Claim 8 (depends on 1)

The combination fan propeller structure as claimed in claim 1, wherein the connection section is complementarily connected with the free end by way of engagement, adhesion, insertion or tight fit.

### Claim 9 (depends on 1)

The combination fan propeller structure as claimed in claim 1, wherein the hub further includes multiple second blade assemblies extending from the free end of the annular section and arranged around the annular section, the first blade assembly being disposed between each two adjacent second blade assemblies to overlap the second blade assemblies.

### Claim 10 (depends on 9)

The combination fan propeller structure as claimed in claim 9, wherein the hub and the first and second blade assemblies are made of metal material.