GB2077855A - Reversible Pitch Bladed Rotor - Google Patents
Reversible Pitch Bladed Rotor Download PDFInfo
- Publication number
- GB2077855A GB2077855A GB8019246A GB8019246A GB2077855A GB 2077855 A GB2077855 A GB 2077855A GB 8019246 A GB8019246 A GB 8019246A GB 8019246 A GB8019246 A GB 8019246A GB 2077855 A GB2077855 A GB 2077855A
- Authority
- GB
- United Kingdom
- Prior art keywords
- machine
- setting
- vanes
- rotor
- axial
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/34—Blade mountings
- F04D29/36—Blade mountings adjustable
- F04D29/362—Blade mountings adjustable during rotation
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
An axial flow fan has means, such as hydraulic actuator 14, for pivoting the fan blades 4 during fan operation from one setting giving airflow in one direction to a second setting giving air flow in the reverse direction. <IMAGE>
Description
SPECIFICATION
Improvements in or Relating to Axial Flow
Fluid Machines especially Fans
The present invention relates to axial flow fluid machines, especially axial fans, and is particularly concerned with the provision of reverse fluid flows in a fluid flow system.
Axial flow fans find extensive application in ventilation systems, such as for example in mines, and in these systems the axial fan directs ventilating air through ducting to selected discharge locations. In some ventilating systems, particularly in mines, it is a requirement that a reverse air flow can be created in the ducting, such as for example when an outbreak of fire occurs, and it is frequently an additional requirement that the change in air flow direction is achieved promptly. One known arrangement for creating this charge involved the use of diverter flaps in the ducting but this had the disadvantage of being cumbersome (and costly), since the ducting can be of substantial cross-section.An alternative arrangement, involves reverse rotation of the fan but some disadvantages of this arrangement are the delay in effecting reverse fan operation, of obtaining adequate reverse flow and additional costly equipment will be necessary. It is an object of the present invention to obviate or mitigate these disadvantages.
According to the present invention a fluid flow machine for use in a fluid ducting system comprises a rotor adapted for connection to a drive, an annular series of axial vanes pivotally mounted on the rotor, and means for pivoting the vanes whereby the vanes can be moved during rotation of the rotor from a first setting creating a fluid flow in one direction to a second setting creating a fluid flow in a reverse direction.
Thus at the first vane setting the vanes can have a positive blade pitch angle or blade root setting (as hereinafter defined) for normal fluid flow, a 600 blade root setting would be suitable, while at the second vane setting a negative blade pitch angle would be present for reverse flow.
Preferably for the second setting, a blade root setting of up to 400 is employed and preferably not greater than --200 a preferred value being approximately --100. It may be desired however to pivot the vanes through a much greater angle e.g. up to 1 600 blade root setting for the second vane setting position.
Pivoting of the vanes can be achieved by means of a suitable lever mechanism-a preferred mechanism utilises a fluid piston cylinder and crank system.
An embodiment of the present invention will now be described by way of example with reference to the accompanying drawings wherein:
Fig. 1 shows a schematic side view of a ventilating ducting including an axial flow fan;
Fig. 2 shows a sectional side view of the fan of
Fig. 1 to a larger scale;
Fig. 3 shows a plan view of the fan blading for various blade settings;
Fig. 4 shows a blade set for normal air flow;
Fig. 5 shows the blade pivoted to a second .position for reverse air flow.
Fig. 6 shows the blade pivoted to yet a further
position for reverse air flow.
Referring to-the drawings, a ventilating system, for example for a mine, includes a ducting 1
housing an axial fan 2 which is driven by a motor
(not shown) located in central housing 3. The fan
2 has an annular series of axial blades or vanes 4
mounted on rotor 5, and the discharge from vanes
4 is guided by stationary guide vanes 6 serving to
support housing 3. 7 is the front hub, the vanes 4
are pivotally mounted in bearings 9 (see Fig. 2)
and have lower cranks 10 carrying thrust blocks
11 located between annular cheek plates 12 of
regulating disc 13. The disc 13 is secured to the
cylinder of a hydraulic piston/cylinder actuator 14
controlled by sleeve valve 1 4A, positioned in hub
7. Operation of the actuator 14 causes axial
movement of disc 13 and hence pivoting of vanes
4.
Fig. 4 shows a vanes 4 set for normal air flow
in direction of arrow A: as can be seen the vane
has a positive pitch angle (a 600 setting angle
being shown). The blade root setting angle (or
blade pitch angle) a is the angle subtended
between the lines AB and AC in Fig. 3, wherein AC is a line parallel to the root chord line D-D and passing through blade pivoted axis, and
AB is the line projection of AC on the plane containing blade pivotal axis and normal to the
axis of rotation of the rotor.
To reverse air flow in arrow direction B, the vanes 4 are rotated negatively in direction RN to
the setting shown in Fig. 5: the negative root
setting can be up to 400 but a value in range -100 to --200 may be preferred. At the 100
setting a reverse flow of approximately 65%
forward can be achieved for the same rotor speed.
Reverse flow can also be achieved by positive vane rotation in direction RP to a blade root
setting of approximately 1600 as shown in Fig. 6.
This will give equal flow rate in reverse as that of
a 550 set blade (with a pressure value reduced to 80%). However performance at some angle
ranges in the increased positive blade settings up
to 1 600 can be unstable and/or unsatisfactory.
The arrangement also enable variation in the
blade setting for normal flow discharge (arrow A),
and the catering for a negative setting of -100 (or even --200) does not require considerable
additional displacement capability of the
actuating mechanism so that a reverse flow
characteristic can be included without great
additional expense.
It is an advantageous feature of the
arrangement that pivoting of the blades 4 can be
effected during rotation of the rotor 5, and
consequently change to the reverse flow mode
can be achieved very promptly.
Modifications are of course possible. For
example, it will be appreciated that the actuating
mechanism could be of some other form than the
piston-and-crank system described. It will be understood that for different blade forms (particularly twist), the preferred blade angle settings could be different from those detailed above.
Claims (9)
1. A fluid flow machine for use in a fluid ducting system comprising a rotor adapted for connection to a drive, an annular series of axial vanes pivotally mounted on the rotor, and means for pivoting the vanes whereby the vanes can be moved during rotation of the rotor from a first setting creating a fluid flow in one direction to a second setting creating a fluid flow in a reverse direction.
2. A machine as claimed in claim 1, wherein at the second setting the axial blades are set at a negative blade pitch angle up to 400.
3. A machine as claimed in claim 2, wherein the negative angle is not greater than 200.
4. A machine as claimed in claim 3, wherein the negative angle is approximately 100.
5. A machine as claimed in claim 1 , wherein the blades are pivoted positively to a blade pitch angle of up to 1 600 for said second setting.
6. A machine as claimed in any one of the preceding claims, wherein a lever mechanism is provided for pivoting of the blades between said settings.
7. A machine as claimed in claim 6, wherein the lever mechanism is actuated by a fluid operable piston/cylinder device.
8. A machine as claimed in claim 7, wherein the axial vanes have crank form root elements carried by an axially-movable annular member mechanically coupled to the piston/cylinder device.
9. A machine as claimed in claim 8, wherein the piston/cylinder device is co-axial with the rotor.
1 0. A fluid flow machine substantially as hereinbefore described with reference to and as illustrated in the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8019246A GB2077855A (en) | 1980-06-12 | 1980-06-12 | Reversible Pitch Bladed Rotor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8019246A GB2077855A (en) | 1980-06-12 | 1980-06-12 | Reversible Pitch Bladed Rotor |
Publications (1)
Publication Number | Publication Date |
---|---|
GB2077855A true GB2077855A (en) | 1981-12-23 |
Family
ID=10514006
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8019246A Withdrawn GB2077855A (en) | 1980-06-12 | 1980-06-12 | Reversible Pitch Bladed Rotor |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2077855A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0155073A2 (en) * | 1984-03-13 | 1985-09-18 | Peabody ABC Corporation | Controllable pitch fans |
US7179054B1 (en) * | 2004-05-14 | 2007-02-20 | The United States Of America As Represented By The Secretary Of The Navy | Flow reversal system for axial fan |
EP1921325A1 (en) * | 2006-11-09 | 2008-05-14 | Snecma | Turbo-propeller comprising an assembly of blades with adjustable orientation. |
-
1980
- 1980-06-12 GB GB8019246A patent/GB2077855A/en not_active Withdrawn
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0155073A2 (en) * | 1984-03-13 | 1985-09-18 | Peabody ABC Corporation | Controllable pitch fans |
EP0155073A3 (en) * | 1984-03-13 | 1986-12-17 | Peabody ABC Corporation | Controllable pitch fans |
US7179054B1 (en) * | 2004-05-14 | 2007-02-20 | The United States Of America As Represented By The Secretary Of The Navy | Flow reversal system for axial fan |
EP1921325A1 (en) * | 2006-11-09 | 2008-05-14 | Snecma | Turbo-propeller comprising an assembly of blades with adjustable orientation. |
FR2908451A1 (en) * | 2006-11-09 | 2008-05-16 | Snecma Sa | TURBOPROPULSEUR COMPRISING AN ADJUSTABLE ORIENTATION BLADE ASSEMBLY |
US8197213B2 (en) | 2006-11-09 | 2012-06-12 | Snecma | Turboprop including a set of adjustable-pitch blades |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3313518A (en) | Turbine control | |
US4250703A (en) | Swinging door particle separator and deicing system | |
EP0606108B1 (en) | Bi-directional axial-flow blower | |
KR970044624A (en) | Variable cycle gas turbine engine | |
US3066488A (en) | Power output control for a gas turbine engine | |
US7108569B2 (en) | Axial flow pump or marine propulsion device | |
US20060230759A1 (en) | Variable geometry turbocharger | |
CA2243151A1 (en) | Variable pitch fan | |
JPH0762480B2 (en) | Variable vane turbo compressor | |
US4032254A (en) | Reversible cross flow blower | |
US2722985A (en) | Full feathering propeller | |
US2318233A (en) | Aircraft propeller | |
GB2077855A (en) | Reversible Pitch Bladed Rotor | |
GB671607A (en) | Improvements in or relating to multi-stage fans, pumps and the like | |
US3248876A (en) | Fluid and vehicle propelling device | |
JP2002031097A (en) | Axial blower | |
US4167854A (en) | Torque converter with internally reversible turbine shaft | |
GB1196588A (en) | Improvements relating to Turbo-fan Aircraft Engines | |
GB545587A (en) | Improvements in and relating to apparatus applicable to screw propellors for obtaining maximum efficiency under all conditions | |
US2523404A (en) | Cooling air exit velocity control | |
US2374342A (en) | Fan | |
KR102025886B1 (en) | Ducted fan | |
US20050150671A1 (en) | Turbine motor for pneumatic tools | |
GB1362750A (en) | Axial flow reversible turbine | |
EP0467336A2 (en) | Bi-directional axial-flow blower |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |