Stirling engine
10060388 ยท 2018-08-28
Assignee
Inventors
Cpc classification
F02G1/053
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02G1/055
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05C2251/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02G1/0435
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02G1/055
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02G1/053
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02G1/043
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A Stirling engine has a housing containing a displacer and a power piston arranged to reciprocate relatively to one another. A head is adjacent to the displacer to absorb heat, and is surrounded by a block of copper or aluminum. A substantial proportion of the block is clad with a layer of stainless steel or Inconel having a thickness of between 3 mm and 0.15 mm.
Claims
1. A Stirling engine comprising a housing containing a displacer and a power piston arranged to reciprocate relatively to one another, a head adjacent to the displacer to absorb heat, the head being surrounded by a block of copper or aluminum, a proportion of an exposed outer surface of the block being clad with a layer of stainless steel or INCONNEL (nickel alloy) having a thickness of between 3 mm and 0.15 mm.
2. An engine according to claim 1, wherein the block has a maximum distance from the outermost surface to the closest part of the housing of greater than 1 cm.
3. An engine according to claim 1, wherein the thickness of the cladding layer is 1 mm to 0.5 mm.
4. An engine according to claim 1, wherein the block has a frustoconical shape, arranged coaxially with the head and with the wider end of the block furthest from the head where it provides a circular face.
5. An engine according to claim 4, wherein only the circular face of the block at the wider end is clad.
6. An engine according to claim 5, wherein the conical face of the block is brazed with nickel.
7. An engine according to claim 1, wherein the block has a cylindrical shape arranged coaxially with the head.
8. An engine according to claim 7, wherein top and/or the side faces of the block are clad.
9. An engine according to claim 1, wherein the engine is a free piston engine.
10. An engine according to claim 1, wherein the engine is a linear engine.
11. A combination of an engine according to claim 1, with a biomass, waste heat or solar heat source arranged to supply heat to the head via the block and cladding.
Description
(1) Examples of Stirling engines in accordance with the present invention will now be described with reference to the accompanying drawings, in which:
(2)
(3)
(4) The basic design of the Stirling engine is known in the art, for example, the Microgen? 1 kW engine. The engine is a linear free piston Stirling engine with a displacer (not shown) adjacent to the head end 1 and a power piston (not shown) adjacent to the opposite end 2. Heat is applied at the head end 1. This heat is absorbed by internal fins 3 as shown in
(5) An annular flange 7 surrounds a central portion of the engine and is the means by which the engine is supported again as is known in the art.
(6) The present invention is directed to the provision of a block adjacent to the head to facilitate heat absorption for particular sources.
(7) In
(8) The block 11 is made of copper or aluminum and the circular top face is clad with a circular disc 18 of stainless steel or INCONEL (nickel alloy) having a thickness of between 3 mm and 1.5 mm. The curved face 17 of the copper block 14 and under the cladding 13 and the narrow end 12 are brazed with nickel.
(9) In use, a solar collector is provided to direct solar energy onto the circular end 13 such that this energy is absorbed into the block 11 and hence into the head 10. It will be appreciated that the relatively large size of the block and the use of copper or aluminium provides a large thermal mass which optimizes the heat absorption into the head. Secondly, the large thermal mass provides a degree of smoothing for this otherwise unpredictable heat source.
(10)
(11) The typical thermal properties of the materials used are set out below:
(12) TABLE-US-00001 Thermal Specific Conductivity1 Density Heat Material W/m K kg/m3 kJ/Kg K Copper 400 8960 0.3785 Stainless 16 to 20 8030 0.5 Steel (304) Aluminium 205 2700 0.897 Inconels (Nickel 16 8430 N/A alloys)