GB2039626A - Rotary machine - Google Patents
Rotary machine Download PDFInfo
- Publication number
- GB2039626A GB2039626A GB7942015A GB7942015A GB2039626A GB 2039626 A GB2039626 A GB 2039626A GB 7942015 A GB7942015 A GB 7942015A GB 7942015 A GB7942015 A GB 7942015A GB 2039626 A GB2039626 A GB 2039626A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- rotary machine
- vanes
- combustible material
- axis
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
- F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
- F02C3/165—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant the combustion chamber contributes to the driving force by creating reactive thrust
Abstract
A rotary machine includes a rotor 10 having a number of pairs of vanes 16 extending radially outwardly, the outer end of each vane being inclined at an angle phi to a radius which angle is greater than the angle theta at which the inner end is inclined to that radius, and means for introducing a combustible material into passages bounded by adjacent blades and two end plates. <IMAGE>
Description
SPECIFICATION
Improvements in rotary machines
The present invention relates to rotary machines.
According to the present invention a rotary machine includes a rotor having at least two pairs of vanes symmetrically disposed about an axis, each vane having an inner end and an outer end, the outer end being angled, relative to a single radial from the axis, to a greater degree than the inner end, and means for introducing a combustible material into passages bounded by adjacent blades and two end plates.
The end plates can be part of a stator, or one or both may be part of the rotor. A preferred embodiment of the invention has a circular rotor and a plurality of vanes. Preferably, the combustible material is introduced along the axis of the rotor. Suitable combustible materials include gaseous or liquid fuels mixed with air. The rotary machine might advantageously be constructed at least in part of a ceramic material.
In one form of the invention the rotor is used to drive an axle to provide a power source. In this configuration combustion gases leaving the rotor will carry a great deal of energy in the form of heat, and this energy, for efficiency, must be utilised by, for example, using the exhaust gas to drive a turbine ortosupply heat via a heat exchanger.
One embodiment of the invention will now be described, by way of example only, with reference to the accompanying diagrammatic drawings, of which,
Figure 1 is an elevation, partly in section of a rotary machine according to the invention, and
Figure 2 is a plan in section along line ll-ll of Figure 1.
A rotor 10 mounted on an axle 11 in a casing 12 has a circular front plate 13 (omitted in the sectional
part of Figure 1) and a circular backplate 14. The front plate 13 has at its centre a circular opening 15 which is aligned with a circular opening 19 in the casing 12. A plurality of vanes 16 extend between the plates 13, 14, each vane 16 making a smaller angle e to a radius of plate 14 at its radial inner end than the angle 4 at its radially outer end. Afuel supply pipe 17
is directed into the opening 15.
In operation fuel from the supply pipe 17 is ignited
by, for example, a spark plug (which is not shown)
and a stable flame zone 18 is established within the
rotor 10, air to maintain the flame being drawn
through the holes 19, 15. Hot combustion gases pass
through the passages between the plates 13, 14 and
vanes 16 and act on the angled vanes 16 to rotate the
rotor 10, providing a work output through the axle
11. The gases then exhaust through an outlet 20 in the casing 12.
The operating procedure may be assisted by
'pre-rotating' rotor 10, for example by hand, prior to
igniting the fuel. It will be appreciated that the rotor
10, which is very similar to the rotor of a centrifugal
compressor, is simple to construct. Consequently a
very cheap source of power, capable of utilising | ;,,,,,,+;,,,, The inherent cheapness (and ease of construction) make the use of ceramics for constructing the rotor 10 a viable proposition.
Certain embodiments of the invention may be used in conjunction with other machinery. For example, air may be supplied to the opening 19 from a compressor which might, for example, be driven by energy from the hot gases exhausting from the outlet 20, by means, for example, of a heat exchanger.
It will be appreciated that alternative constructions are possible. For example, the rotor 10 may include vanes 16 mounted on a backplate 14, the rotor being arranged to rotate within a stator having only a single radially extending plate with an opening 19 adjacent the edges of vanes 16 remote from the backplate 14.
1. A rotary machine including a rotor having at least two pairs of vanes symmetrically disposed about an axis, each vane having an inner end and an outer end, the outer end being angled, relative to a single radial from the axis, to a greater degree than the inner end, and means for introducing a combustible material into passages bounded by adjacent blades and two end plates.
2. A rotary machine as claimed in Claim 1 wherein the end plates are part of a stator.
3. A rotary machine as claimed in Claim 1 wherein one end plate is part of a stator and the other is part of the rotor.
4. A rotary machine as claimed in Claim 1 wherein the end plates are part of the rotor.
5. A rotary machine as claimed in any one of
Claims 1 to 4 wherein the rotor is circular and has a plurality of vanes.
6. A rotary machine as claimed in any one of
Claims 1 to 5 wherein the combustible material is introduced along the axis of the rotor.
7. A rotary machine as claimed in any one of
Claims 1 to 6 including means for igniting the combustible material.
8. A rotary machine as claimed in Claim 7 connected to drive an axle.
9. A rotary machine as claimed in Claim 7 or in
Claim 8 wherein combustion gases exiting from the passages are collected and used to drive a turbine.
10. A rotary machine as claimed in Claim 7 or
Claim 8 wherein combustion gases exiting from the passages are collected and passed through a heat exchanger.
11. A rotary machine as claimed in Claim 9 wherein the turbine drives a compressor which compresses combustible material before introduction to the rotor.
12. A rotary machine substantially as herein described with reference to the accompanying drawings.
13. A rotary machine substantially as herein described.
14. A rotary machine as claimed in any one of
Claims 1 to 13 constructed at least in part of ceramic
moforinl
**WARNING** end of DESC field may overlap start of CLMS **.
Claims (14)
1. A rotary machine including a rotor having at least two pairs of vanes symmetrically disposed about an axis, each vane having an inner end and an outer end, the outer end being angled, relative to a single radial from the axis, to a greater degree than the inner end, and means for introducing a combustible material into passages bounded by adjacent blades and two end plates.
2. A rotary machine as claimed in Claim 1 wherein the end plates are part of a stator.
3. A rotary machine as claimed in Claim 1 wherein one end plate is part of a stator and the other is part of the rotor.
4. A rotary machine as claimed in Claim 1 wherein the end plates are part of the rotor.
5. A rotary machine as claimed in any one of
Claims 1 to 4 wherein the rotor is circular and has a plurality of vanes.
6. A rotary machine as claimed in any one of
Claims 1 to 5 wherein the combustible material is introduced along the axis of the rotor.
7. A rotary machine as claimed in any one of
Claims 1 to 6 including means for igniting the combustible material.
8. A rotary machine as claimed in Claim 7 connected to drive an axle.
9. A rotary machine as claimed in Claim 7 or in
Claim 8 wherein combustion gases exiting from the passages are collected and used to drive a turbine.
10. A rotary machine as claimed in Claim 7 or
Claim 8 wherein combustion gases exiting from the passages are collected and passed through a heat exchanger.
11. A rotary machine as claimed in Claim 9 wherein the turbine drives a compressor which compresses combustible material before introduction to the rotor.
12. A rotary machine substantially as herein described with reference to the accompanying drawings.
13. A rotary machine substantially as herein described.
14. A rotary machine as claimed in any one of
Claims 1 to 13 constructed at least in part of ceramic
moforinl
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7942015A GB2039626B (en) | 1978-12-19 | 1979-12-05 | Rotary machine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7849159 | 1978-12-19 | ||
GB7942015A GB2039626B (en) | 1978-12-19 | 1979-12-05 | Rotary machine |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2039626A true GB2039626A (en) | 1980-08-13 |
GB2039626B GB2039626B (en) | 1982-11-24 |
Family
ID=26270027
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7942015A Expired GB2039626B (en) | 1978-12-19 | 1979-12-05 | Rotary machine |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2039626B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1998007984A1 (en) * | 1996-08-23 | 1998-02-26 | Dragoljub Perunicic | Motor propulsion unit having improved efficiency |
WO2009009026A2 (en) | 2007-07-10 | 2009-01-15 | Ziyad Qamhiyeh | Rotary internal combustion engine |
-
1979
- 1979-12-05 GB GB7942015A patent/GB2039626B/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1998007984A1 (en) * | 1996-08-23 | 1998-02-26 | Dragoljub Perunicic | Motor propulsion unit having improved efficiency |
WO2009009026A2 (en) | 2007-07-10 | 2009-01-15 | Ziyad Qamhiyeh | Rotary internal combustion engine |
EP2167797A2 (en) * | 2007-07-10 | 2010-03-31 | Ziyad Qamhiyeh | Rotary internal combustion engine |
EP2167797A4 (en) * | 2007-07-10 | 2014-03-05 | Ziyad Qamhiyeh | Rotary internal combustion engine |
Also Published As
Publication number | Publication date |
---|---|
GB2039626B (en) | 1982-11-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |