CN100376780C - A stirling engine assembly - Google Patents

A stirling engine assembly Download PDF

Info

Publication number
CN100376780C
CN100376780C CNB2005100840005A CN200510084000A CN100376780C CN 100376780 C CN100376780 C CN 100376780C CN B2005100840005 A CNB2005100840005 A CN B2005100840005A CN 200510084000 A CN200510084000 A CN 200510084000A CN 100376780 C CN100376780 C CN 100376780C
Authority
CN
China
Prior art keywords
stirling engine
spring
motor
scaffold
main shaft
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.)
Expired - Fee Related
Application number
CNB2005100840005A
Other languages
Chinese (zh)
Other versions
CN1721682A (en
Inventor
亚当·理查德·格雷戈里
大卫·安东尼·克拉克
朱莉·帕特丽夏·海德
大卫·迈克尔·热纳维
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Micron Energy Holdings
Solarate Ltd
Original Assignee
Microgen Energy Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Microgen Energy Ltd filed Critical Microgen Energy Ltd
Publication of CN1721682A publication Critical patent/CN1721682A/en
Application granted granted Critical
Publication of CN100376780C publication Critical patent/CN100376780C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02GHOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G1/00Hot gas positive-displacement engine plants
    • F02G1/04Hot gas positive-displacement engine plants of closed-cycle type
    • F02G1/043Hot gas positive-displacement engine plants of closed-cycle type the engine being operated by expansion and contraction of a mass of working gas which is heated and cooled in one of a plurality of constantly communicating expansible chambers, e.g. Stirling cycle type engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Vibration Prevention Devices (AREA)

Abstract

A Stirling engine assembly for a DCHP system. A Stirling engine (1) is suspended from a mounting frame (5) by a plurality of tension springs (6). An annular absorber mass (2) surrounds the Stirling engine and is suspended from the engine on a plurality of resilient members (3) arranged asymmetrically about the main axis. The asymmetric arrangement is provided by members of different stiffnesses, or irregular spacing of the members. The absorber mass (2) itself may be reduced adjacent to the resilient members.

Description

Stirling engine assembly
The application is to be that November 12, application number in 2002 are that 02812605.X, name are called the dividing an application of patent application of " Stirling engine assembly " applying date.
Technical field
The present invention relates to a kind of Stirling engine assembly.Particularly, the present invention relates to a kind of assembly that is applicable to domestic combined thermoelectricity (DCHP) unit.
Background technique
Domestic combined thermoelectric unit like this will replace plain cylindrical furnace to be used for family environment.In this case, importantly make noise and vibration keep low-down level, so that client can be accepted.
Normal conditions are to support by motor is installed on the spring, and this spring will be isolated in the vibration that produces in the motor course of normal operation.An example with Stirling engine of this structure is a U.S. Pat 4,400,941.In order to make degree of isolation the highest, need to adopt the installation system of low rigidity.But, adopt low rigidity installation system may cause instability with pressure spring.
Summary of the invention
According to the present invention, a kind of Stirling engine assembly comprises: Stirling engine; Scaffold, motor are installed on this scaffold, and like this, in use, the reciprocating member of motor is along the vertical axis to-and-fro motion, and this motor is hanging on the scaffold by a plurality of extension springs.
By by the spring suspension Stirling engine, rather than it is placed on the spring, employed spring can be the spring of low rigidity, high amount of deflection.Therefore, can eliminate in the prior art contradiction between the requirement of the requirement of stable support and low rigidity installation system.
The spring that hangs motor is particularly suitable for stoping the transmission of low-frequency vibration.In order to improve damping in bigger frequency range, preferably rubber pad and each spring are connected in series.This pad can be arranged between spring and the motor, between spring and the scaffold or in these two positions.These rubber pads are specially adapted to reduce dither.
Preferably, scaffold links to each other with lower half portion of motor.Situation required when linking to each other with motor top with scaffold is compared, and this allows to use long spring.
Has additional radial stability in order to make around the Stirling engine in the suspension structures, and in order to make the combustion zone that appropriate seal be arranged, be positioned on the motor above the dome and housing, that be used for burner can comprise the flexible annular guide on every side, this flexible annular guide is between the inboard bottom surface and motor of this housing.For example, this flexible annular guide is the round section joint ring that is applicable to the material of vibration, hot environment.This will allow to carry out certain transverse movement, and therefore, engine luggine will can not cause damage, and stop the transmission of undesirable power, and can also keep the stability of motor.Also can use the optional sealing configuration that can bear high temperature, high vibration environment.
Preferably, the free length of spring is 100-150mm, and global stiffness is between 0.6 to 0.9kg/mm.When having hung motor, the length of this spring equals the length of engine block ± 20%.
Said structure is a suspension structures particularly advantageous, that be used for Stirling engine.But, by vibration damping structure that is provided with the vibration that can minimize motor and the load that therefore reduces suspension structures, can further improve design.Therefore, preferably, damping block is suspended on below the motor by at least one elastic member, and this damping block is arranged to the power that provides anti-phase with motor.This damping block both can be suspended on below the motor, also can be ring block, thereby around this engine suspension.A kind of structure in back can advantageously provide the Stirling engine with shorter total height.
Under the annular damping block situation of symmetry, because this piece is around the combination about the rotational stiffness of same axis of the inertia of horizontal axis and spring system, the pitching frequency will overlap with vertical frequency.
The pitching degree is relevant with radial rigidity shortage symmetry properties, and the vibration damper piece departs from the spring rate center more, and energizing frequency is approaching more vertical tuned frequency and pitching frequency just.Therefore, elastic member is preferably about the asymmetric layout of the main shaft of annular element.This for example can have different-stiffness to realize by making elastic member.Preferably, be arranged in first spool the opposite side vertical symmetrically, be more preferably, also be arranged in second spool the opposite side vertical with first symmetrically with main shaft with main shaft.
Also can select, be gathered near providing dissymmetrical structure perpendicular to first of main shaft by making elastic member.For this structure, elastic member preferably is arranged to the opposite side symmetry at first.
In both cases, the quality of damping block can reduce with respect to the remaining part place of this damping block near the horizontal axis place of the highest rotational stiffness.
This asymmetric annular vibration damper piece forms an independent aspects of the present invention, and this aspect generalized definition is that a kind of Stirling engine assembly comprises: Stirling engine; Scaffold, motor is installed on this scaffold, like this, in use, reciprocating member is along the vertical axis to-and-fro motion, wherein, the annular damping block is around Stirling engine, and be suspended on the motor by a plurality of elastic members, so that the power anti-phase with motor is provided, this elastic member is arranged to about the main shaft of annular element asymmetric.
According to a first aspect of the invention, when motor passes through spring suspension, when perhaps hanging, can use this structure by some other resilient mounting.
Description of drawings
Introduce an example of Stirling engine assembly of the present invention below with reference to the accompanying drawings, in the accompanying drawing:
Fig. 1 is the schematic sectional view of assembly;
Fig. 2 A is the plan view of a part that comprises the mounting assembly of two springs;
Fig. 2 B is the side view of the structure shown in Fig. 2 A;
Fig. 3 is the schematic sectional view of the optional form of the assembly shown in Fig. 1;
Fig. 4 is the dynamics schematic representation of suspension structures;
Fig. 5 A is the view of the various vibrational modes of the annular damping block of expression;
Fig. 5 B is the view of the axle of expression damping block;
Fig. 6 is the schematic representation of expression first spring structure;
Fig. 7 is the schematic representation of expression second spring structure; And
Fig. 8 is the perspective view that is applicable to the ring block in the structure of Fig. 7.
Embodiment
Stirling engine assembly comprises Stirling engine 1, and this Stirling engine 1 is known in this field.This Stirling engine has displacer and power piston, and this displacer and power piston all are arranged to vertically to-and-fro motion.This has produced the clean vertical vibration of Stirling engine 1 self.
In order to reduce this vibration, vibration damper piece 2 by this above vibration damper piece 2 and below 3 supportings of a plurality of pressure springs.This structure is loaded in the housing 4, and this housing 4 is rigidly fixed in the bottom of Stirling engine 1.This piece 2 and spring 3 are adjusted to like this, and promptly when Stirling engine 1 was worked with normal working frequency, vibration damper piece 2 was as far as possible near vibrate with Stirling engine 1 anti-phasely.Therefore, reduced the overall vibration of Stirling engine 1 and housing 4 greatly.
Current structure is included in 8 pressure springs 3 above the vibration damper piece 2 of 10.5kg (± 10%) and 8 pressure springs 3 below this vibration damper piece 2.For example, the free length of these springs is 67mm, and rigidity is 66.25N/mm (± 10%).This vibration damper is adjusted to the vibration (vibration is minimum when 50.25Hz) that absorbs 48Hz to 52Hz frequency.
The said modules of Stirling engine 1 and housing 4 is installed on the scaffold 5, and this scaffold 5 is around the head of motor, as shown in Figure 1.Motor 1 and housing 4 are suspended on the scaffold around Stirling engine mounting assembly at interval by a plurality of, have represented a kind of such mounting assembly among Fig. 2 A and the 2B.Each mounting assembly comprises a pair of extension spring 6, and this is provided with hook 7 to extension spring 6 in their upper end, be used to be installed in scaffold 5.Second hook 8 is installed on the framework 9 bottom of each spring.
The thickness of Spring Steel Wire is chosen as the weight that is enough to supporting engine 1 and vibration damper piece 2, and the weight of this motor 1 and vibration damper piece 2 still is generally 60kg between 40 to 80kg.At this moment, Spring Steel Wire typically has a diameter from 2.4mm.
Reduce low-frequency vibration for best suspension vibration isolating effect is provided, spring needs long as far as possible, and mounting points should be far away as far as possible in the design allowed band simultaneously.At this moment, top scaffold 5 will just be positioned at the engine burner housing below, bottom motor mount ring 12 be positioned at the bottom engine flange on.At this moment, the length of the spring of elongation is approximately equal to the length (190mm usually) of the engine block of removing cooler 13, heat transfer head 14 and rear end dome 15 (as shown in Figure 1).In addition, must guarantee that the natural frequency (oscillation frequency) of spring does not overlap with operation frequency or its resonance of motor, this may cause unacceptable resonance.
In current structure, be provided with around motor one-tenth rule interval and 6 to 12 springs arranged in pairs (common 8), the free length of this spring is 100 to 150mm (127mm usually) preferably.Total spring rate is (0.75kg/mm usually) between 0.6 to 0.9kg/mm, and in this structure, the rigidity of each spring is generally 0.09kg/mm.
Rubber element 10 is arranged in each framework 9.These rubber element 10 supporting construction bolts 11, by this construction bolt 11, mounting assembly is installed on the installing ring 12 of Stirling engine 1.Therefore, any vibration of Stirling engine 1 all passes to rubber element 10, is delivered in the framework 9 by this bolt 11, passes to scaffold 5 by spring 6 then.
As a kind of possibility, or, can also be provided with rubber element at the top of each spring except the rubber element 10 of each spring bottom.
Rigidity based on each rubber element 10 of four groups of springs is for example 110N/mm.This rubber element is designed to remove high frequency content, and therefore, given rigidity is suitable, and strain remains on proper level, should be kept in mind that the performance of rubber when temperature raises reduces.
Dither will be decayed by rubber element 10, and low-frequency vibration will decay by spring 6, and like this, the vibration that scaffold 5 is subjected to can be ignored, and in the tolerance limit of DCHP unit.
Fig. 3 has represented the optional components of assembly shown in Figure 1.In this structure, housing 4 ' is mounted to around Stirling engine 1, rather than is suspended on as shown in Figure 1 below this motor 1 at this moment, and vibration damper piece 2 ' is an annular, and around Stirling engine.This embodiment requires installing ring 12 that the diameter more much bigger than Fig. 1 arranged.But, the total height of this device reduces, and therefore, this design has useful in limited time in height space.In others, this installs as shown in fig. 1, and same reference numerals is used to represent same parts.
The dynamics figure of this assembly as shown in Figure 4.In the figure, each element is expressed as follows:
M1-master motor piece,
M2-vibration damper piece 2,
The number of the rigidity * extension spring of k1-extension spring 6,
The damping value of c1-and extension spring structurally associated,
The number of the compression stiffness * rubber element of k2-rubber element 10,
The damping value that c2-is relevant with the compressing rubber element,
The number of the rigidity * pressure spring of k3-pressure spring 3 (being generally 16),
C3-is with pressure spring and around the relevant damping value of the air movement of vibration damper piece.
Introduce the version of the annular vibration damper piece of Fig. 3 below with reference to Fig. 5 to 8.
Fig. 5 A and 5B have defined the axle system of ring block.X, Y and Z axle are mutually orthogonal, and wherein X and Y-axis are the horizontal axis in the ring block plane, and they intersect at the center of ring block, and the Z axle is the vertical shaft that stretches out from the center of vibration damper piece 2 '.Intrinsic energizing frequency causes along the up-and-down movement of arrow 20 directions.But, the pitching frequency will overlap with vertical frequency, and this vertical frequency causes the pitching movement about X and Y-axis, shown in arrow 21 and 22 difference.Annular vibration damper piece is also around the rotation of Z axle, and is as shown in arrow 23.In order to reduce pitching movement around X and Y-axis, proposed to make the asymmetric layout of spring, perhaps make the inertia of vibration damper piece asymmetric.
First example of this set as shown in Figure 6.This structure is suitable for the vibration damper piece usually around the equal situation of the rotary inertia of X and Y-axis.At this moment, vibration damper piece 2 ' has uniform cross section and uniform quality.By spring is arranged to as shown in Figure 6, wherein the rigidity of four springs is K, and the rigidity of all the other four springs is 0.5K, should be understood that, this provides when opposite side symmetry in X and Y-axis of the rigidity of spring the stiffness variation around the periphery of this piece, rather than the stiffness variation of crossing this piece.This spring rate pattern can be on the vibration damper piece with below be made as consistent.In second structure, spring rate and vibration damper piece rotary inertia are all asymmetric.
Second structure as shown in Figure 7, when the rotary inertia of damper rings about X and Y-axis not simultaneously, this second structure is suitable especially.At this moment, provide equal stiffness K ' 8 springs, but they accumulate in the axle X place of high inertia, consistent with the requirement that keeps enough stable in the course of the work.At this moment, provide ring block 2 ", this ring block 2 " substantially the opposite side at it be provided with pair of notches part 25, and these 8 springs be arranged to each above the notch portion and below be installed on the mounting points 26.

Claims (7)

1. a Stirling engine assembly comprises: Stirling engine; Scaffold, motor is installed on this scaffold, like this, in use, reciprocating member is characterized in that along the vertical axis to-and-fro motion, the annular damping block is around Stirling engine, and be suspended on the motor by a plurality of elastic members, so that the power anti-phase with motor is provided, these elastic members are about the asymmetric setting of the main shaft of annular element.
2. assembly according to claim 1 is characterized in that: described dissymmetrical structure provides by the elastic member of different-stiffness.
3. assembly according to claim 2 is characterized in that: these elastic members are arranged in first spool the opposite side vertical with main shaft symmetrically.
4. assembly according to claim 3 is characterized in that: these elastic members also are arranged in second spool the opposite side vertical with first with main shaft symmetrically.
5. assembly according to claim 1 is characterized in that: be gathered near providing dissymmetrical structure perpendicular to first of main shaft by making elastic member.
6. assembly according to claim 5 is characterized in that: these elastic members are arranged to the opposite side at first symmetrically.
7. according to each described assembly in the claim 1 to 6, it is characterized in that: the quality of described damping block is reducing with respect to the remaining part place at this damping block near the elastic member place.
CNB2005100840005A 2001-11-14 2002-11-12 A stirling engine assembly Expired - Fee Related CN100376780C (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GBGB0127375.4A GB0127375D0 (en) 2001-11-14 2001-11-14 A stirling engine assembly
GB0127375.4 2001-11-14
GB0203016.1 2002-02-08

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
CNB02812605XA Division CN100462542C (en) 2001-11-14 2002-11-12 Stirling engine assembly

Publications (2)

Publication Number Publication Date
CN1721682A CN1721682A (en) 2006-01-18
CN100376780C true CN100376780C (en) 2008-03-26

Family

ID=9925793

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2005100840005A Expired - Fee Related CN100376780C (en) 2001-11-14 2002-11-12 A stirling engine assembly

Country Status (6)

Country Link
KR (1) KR100964910B1 (en)
CN (1) CN100376780C (en)
AR (1) AR037375A1 (en)
AT (1) ATE422025T1 (en)
DE (1) DE60231053D1 (en)
GB (2) GB0127375D0 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019192437A1 (en) * 2018-04-02 2019-10-10 宁波华斯特林电机制造有限公司 Vibration isolation structure of linear oscillatory motor and stirling engine

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5314727B2 (en) * 2011-03-31 2013-10-16 三菱重工業株式会社 Instrumentation equipment installation device for stationary engine
KR101308149B1 (en) * 2012-01-30 2013-09-12 주식회사 경동나비엔 Hanging sensor system of sterling engine's spring
CN108397645B (en) * 2017-02-08 2024-06-04 中国电力工程顾问集团华东电力设计院有限公司 Spring shock insulation foundation of turbo generator
US20220392657A1 (en) * 2021-06-03 2022-12-08 Battelle Energy Alliance, Llc Energy production devices and associated components, and related heat transfer devices and methods

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4694650A (en) * 1986-07-28 1987-09-22 Mechanical Technology Incorporated Externally tuned vibration absorber
US4742679A (en) * 1985-11-18 1988-05-10 Matsushita Electric Industrial Co., Ltd. Stirling engine
JPS63263250A (en) * 1987-04-20 1988-10-31 Mitsubishi Electric Corp Vibration reducing device for stirling engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4400941A (en) 1981-06-05 1983-08-30 Mechanical Technology Incorporated Vibration absorber for a free piston Stirling engine
JPS5828035A (en) 1981-08-11 1983-02-18 Saiichi Okamoto Vibro-isolating track and its vibro-isolating device
US5139242A (en) 1990-11-06 1992-08-18 Yarr George A Linear suspension device
US6079698A (en) 1997-08-18 2000-06-27 Fmc Corporation Isolation system for vibratory equipment

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4742679A (en) * 1985-11-18 1988-05-10 Matsushita Electric Industrial Co., Ltd. Stirling engine
US4694650A (en) * 1986-07-28 1987-09-22 Mechanical Technology Incorporated Externally tuned vibration absorber
JPS63263250A (en) * 1987-04-20 1988-10-31 Mitsubishi Electric Corp Vibration reducing device for stirling engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019192437A1 (en) * 2018-04-02 2019-10-10 宁波华斯特林电机制造有限公司 Vibration isolation structure of linear oscillatory motor and stirling engine
US11300074B2 (en) 2018-04-02 2022-04-12 Ningbo China Stirling Engine Manufacturing Co., Ltd Vibration isolation structure of linear oscillatory motor and stirling engine

Also Published As

Publication number Publication date
AR037375A1 (en) 2004-11-03
KR100964910B1 (en) 2010-06-23
ATE422025T1 (en) 2009-02-15
GB0203016D0 (en) 2002-03-27
DE60231053D1 (en) 2009-03-19
GB0127375D0 (en) 2002-01-09
CN1721682A (en) 2006-01-18
KR20040052513A (en) 2004-06-23

Similar Documents

Publication Publication Date Title
CN100462542C (en) Stirling engine assembly
CA2245621C (en) Improved isolation system for vibratory equipment
JPH0223739B2 (en)
CN100376780C (en) A stirling engine assembly
RU2651408C1 (en) Spatial frame type vibration isolator with parallel resilient-damping elements
RU2618350C1 (en) Vibro-isolating system of kochetov for machine tools
RU2301919C1 (en) Vibration isolating rubber base
AU2002339146A1 (en) A stirling engine assembly
RU2651446C1 (en) Vibration isolator for the unbalanced equipment
RU2653940C1 (en) Vibration isolator for the unbalanced equipment
SU1634859A1 (en) Vibration damping support
RU2652294C1 (en) Cap and pin spatial vibration isolator
SU1474357A1 (en) Vibration isolator
RU2006714C1 (en) Vibration-isolating suspension intended for operation at any angle to horizon
SU1746094A1 (en) Vibration isolation support
RU2652293C1 (en) Spatial vibration isolator of frame type
RU2662336C1 (en) Spatial vibration isolator of frame type
SU1634861A1 (en) Pneumatic vibration insulator for pneumatic looms
RU2661666C2 (en) Kochetov beaded mesh vibration isolator
RU2019133837A (en) SPATIAL VIBRATION ISOLATOR FOR UNBALANCED EQUIPMENT
SU1018865A2 (en) Pneumatic resilient member of vehicle suspension
RU2185545C2 (en) All-metal vibration isolator
Ingalls et al. If You Can't Kill It, Isolate It
RU2048238C1 (en) Vibratory core sand mixture compaction unit
JPH01182647A (en) Supporting method for subvibration system in dynamic vibration reducer

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
ASS Succession or assignment of patent right

Owner name: MICROGEN ENERGY LTD.

Free format text: FORMER OWNER: SOLAR GMBH

Effective date: 20131105

Owner name: SOLAR GMBH

Free format text: FORMER OWNER: MACROKIN ENERGY LTD.

Effective date: 20131105

C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20131105

Address after: Holland ulft

Patentee after: Micron Energy Holdings

Address before: Ohio, USA

Patentee before: Solarate Ltd.

Effective date of registration: 20131105

Address after: Ohio, USA

Patentee after: Solarate Ltd.

Address before: Burke County, England

Patentee before: Microgen Energy Ltd.

CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20080326

Termination date: 20151112

EXPY Termination of patent right or utility model