GB2557264A - Multibody helmholtz resonator - Google Patents

Multibody helmholtz resonator Download PDF

Info

Publication number
GB2557264A
GB2557264A GB1620499.2A GB201620499A GB2557264A GB 2557264 A GB2557264 A GB 2557264A GB 201620499 A GB201620499 A GB 201620499A GB 2557264 A GB2557264 A GB 2557264A
Authority
GB
United Kingdom
Prior art keywords
chamber
helmholtz resonator
chambers
wall
opening
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
Application number
GB1620499.2A
Other versions
GB2557264A8 (en
GB201620499D0 (en
GB2557264B (en
Inventor
J Maclane Stephen
Hutchings Stephen
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.)
Delphi International Operations Luxembourg SARL
Original Assignee
Delphi International Operations Luxembourg SARL
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 Delphi International Operations Luxembourg SARL filed Critical Delphi International Operations Luxembourg SARL
Priority to GB1620499.2A priority Critical patent/GB2557264B/en
Publication of GB201620499D0 publication Critical patent/GB201620499D0/en
Priority to PCT/EP2017/080235 priority patent/WO2018099802A1/en
Publication of GB2557264A publication Critical patent/GB2557264A/en
Publication of GB2557264A8 publication Critical patent/GB2557264A8/en
Application granted granted Critical
Publication of GB2557264B publication Critical patent/GB2557264B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23MCASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M20/00Details of combustion chambers, not otherwise provided for, e.g. means for storing heat from flames
    • F23M20/005Noise absorbing means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M55/00Fuel-injection apparatus characterised by their fuel conduits or their venting means; Arrangements of conduits between fuel tank and pump F02M37/00
    • F02M55/04Means for damping vibrations or pressure fluctuations in injection pump inlets or outlets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23KFEEDING FUEL TO COMBUSTION APPARATUS
    • F23K5/00Feeding or distributing other fuel to combustion apparatus
    • F23K5/02Liquid fuel
    • F23K5/14Details thereof
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/31Fuel-injection apparatus having hydraulic pressure fluctuations damping elements
    • F02M2200/315Fuel-injection apparatus having hydraulic pressure fluctuations damping elements for damping fuel pressure fluctuations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00014Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

A Helmholtz resonator (26) is adapted to attenuate pressure fluctuations propagating in injection fuel equipment. The resonator includes a peripheral wall 30, 32, 34 enclosing an inner space S. An opening 36 is arranged through the peripheral wall enabling fluid communication with the inner space. The resonator has at least one partition wall 38 dividing the inner space into distinct chambers C1, C2, the partition wall having an aperture 42 creating fluid communication between the chambers. A third chamber C3 may also be provided which may be in fluid communication with the second chamber via a second aperture 44. The volume of C1 may be 20cm3 and the volume of C3 10cm3 with C2 in between. The resonator may have a damper comprising a gas filled diaphragm or may use a viscous damper comprising a slidable piston (50 fig.3), sub chambers (C31, C32 fig.3) and a spring (62 fig.3).

Description

(71) Applicant(s):
Delphi International Operations Luxembourg S.a.r.l. Avenue de Luxembourg, Bascharage 4940, Luxembourg (72) Inventor(s):
Stephen J Maclane Stephen Hutchings (74) Agent and/or Address for Service:
DELPHI FRANCE SAS
PO Box CS 65059, Bat. Le Raspail,
ZAC Paris Nord II 22, avenue des Nations,
Roissy CDG Cedex 95972,
France (including Overseas Departments and Territori es) (51) INT CL:
F23M 20/00 (2014.01) (56) Documents Cited:
EP 3029377 A1 EP 3029376 A1
EP 2816289 A1 EP 2642204 A1
US 20160003162 A1 (58) Field of Search:
INT CL F23M, F23R, G10K Other: WPI, EPODOC.
(54) Title of the Invention: Multibody helmholtz resonator Abstract Title: Multi-chamber Helmholtz attenuator (57) A Helmholtz resonator (26) is adapted to attenuate pressure fluctuations propagating in injection fuel equipment. The resonator includes a peripheral wall 30, 32, 34 enclosing an inner space S. An opening 36 is arranged through the peripheral wall enabling fluid communication with the inner space. The resonator has at least one partition wall 38 dividing the inner space into distinct chambers C1, C2, the partition wall having an aperture 42 creating fluid communication between the chambers. A third chamber C3 may also be provided which may be in fluid communication with the second chamber via a second aperture 44. The volume of C1 may be 20cm3 and the volume of C3 10cm3 with C2 in between. The resonator may have a damper comprising a gas filled diaphragm or may use a viscous damper comprising a slidable piston (50 fig.3), sub chambers (C31, C32 fig.3) and a spring (62 fig-3).
Figure GB2557264A_D0001
/3
Figure GB2557264A_D0002
FIG. 1
2/3
Figure GB2557264A_D0003
Figure GB2557264A_D0004
3/3 t
Figure GB2557264A_D0005
FIG. 4
Multibody Helmholtz Resonator
TECHNICAL FIELD
The present invention relates to a Helmholtz resonator adapted to be arranged in the fluid circuit of a fuel injection equipment in order to attenuate pressure fluctuations propagating in said circuit.
BACKGROUND OF THE INVENTION
Pressure fluctuations within a fuel injection system are undesirable as they can lead to external leakage or starving critical components of lubricating oil. Current solution to dampen out these oscillations include gas filled capsule dampers, moving piston pressure regulators or basic Helmholtz resonators fitted at critical points within the system to maintain a more even pressure.
Capsule type and moving piston pressure regulators lack durability and, in addition these types of attenuators require moving parts tending to move with the frequency demonstrating the highest frequency this potentially letting through some lower energy frequencies that could offer additional problems.
SUMMARY OF THE INVENTION
Accordingly, it is an object of the present invention to resolve the above mentioned problems in providing a Helmholtz resonator adapted to attenuate pressure fluctuations propagating in an injection fuel equipment, said Helmholtz resonator having a peripheral wall enclosing an inner space, an opening arranged through said peripheral wall for enabling a fluid communication with said inner space.
Advantageously, the Helmholtz resonator further comprises at least one partition wall dividing said inner space in distinct chambers, said partition wall being provided with an aperture creating an internal fluid communication between said distinct chambers, the opening opening in one of the chambers.
Also, the peripheral walls comprise a cylindrical wall extending along a main axis from a first transverse end wall to a distant second transverse end wall.
Also, said at least one partition wall is substantially parallel to any one of the transverse end walls.
Also, the Helmholtz resonator comprises a first and a second chambers in fluid communication between each other’s via a first aperture arranged in a first partition wall and, a third chamber in fluid communication with the second chamber via a second aperture arranged in a second partition wall.
Also, the first and second partition walls are substantially parallel to each other’s, the second chamber being interposed between the first chamber and the third chamber.
Also, the first chamber is larger than the second chamber and, the second chamber is larger than the third chamber.
Also, the volume of the first chamber is about 20 cm3 and, the volume of the third chamber is about 10 cm3.
Also, the first aperture has across section area of about 1 mm2 and, the second aperture has across section area of about. 0.3 mm2.
Also, the Helmholtz resonator comprises more than three distinct chambers.
Also, the opening is arranged to open in the first chamber.
Also, the cross section area of the opening is about 3 mm2.
Also, the Helmholtz resonator further comprises an outlet arranged in a peripheral wall for enabling a fluid communication with said inner space.
Also, the opening and the outlet open in the same chamber.
Also, the opening and the outlet both open in the second chamber.
Also, the Helmholtz resonator further comprises a damper, arranged in one of the chambers, said damper moving as a function of the pressure fluctuations.
Also, said damper comprises a gas filled diaphragm.
Also, in another embodiment, said damper is a viscous damper comprising a slidable piston dividing the chamber in which it is arranged in a first sub-chamber and a second sub-chamber in fluid communication with each other’s via a communication passage, said viscous damper further comprising a spring arranged between said piston and a wall of said chamber in which the piston is arranged so that, the volume of the sub-chambers vary relative to each other’s as a function of the pressure fluctuations.
The invention further extends to a fuel pump of a fuel injection equipment wherein fuel entering via a pump inlet is pressurised in a compression chamber and is expelled via a pump outlet, a camshaft rotating, in use, between a front and a rear bearings urging a reciprocating piston to vary the volume of said compression chamber, the pump further comprising a Helmholtz resonator as described in the previous lines and is arranged to attenuate pressure fluctuations in said pump.
BRIEF DESCRIPTION OF THE DRAWINGS
The present invention is now described by way of example with reference to the accompanying drawings in which:
Figure 1 is a schematic diagram of a high pressure fuel pump provided with a multibody Helmholtz resonator as per the invention.
Figure 2 is an axial section of a first embodiment of the Helmholtz resonator of figure 1.
Figure 3 is a 3D view of a second embodiment of the resonator of figure 1.
Figure 4 is an alternative to the resonator of figure 3.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
A pumping system 10 of a fuel injection equipment is sketched on figure 1 specially highlighting the fuel flows. The pumping system 10 has a housing 12 (not shown) defining a cambox having an inner space in which a camshaft 14 is arranged between a front bearing 16 aligned with a rear bearing 18, said camshaft 14 cooperating with a piston sliding in a bore.
In use, the camshaft 14 rotates and urges said piston to perform a pumping cycle varying the volume of a compression chamber 20 and, fuel entering the pumping system 10 via an inlet 22 is compressed in said compression chamber 20 and is expelled via an outlet 24 wherefrom it is delivered to fuel injectors. Part of the fuel is not pressurised and lubricates the cambox, the bearings 16, 18 or the piston and bore adjustment and, the reciprocal displacements of the piston generates pressure fluctuations that propagate in said low pressure fuel. The pumping system 10 further comprises an attenuator 26 arranged to attenuate said pressure fluctuations.
The attenuator 26 is a multibody Helmholtz resonator 26, a first embodiment of which being presented in figure 2. The Helmholtz resonator 26 has a housing 28 comprising a peripheral cylindrical wall 30 extending along a main axis X from a lower, or first, transverse wall 32 to an upper, or second, transverse wall 34. Said housing 28 defines an inner space S and, an opening 36 provided in the lower transverse face 32 is adapted to be connected to low pressure areas where in the pump pressure waves propagate, said opening 36 being both an inlet and an outlet for said pressure waves. A first partition wall 38 and a second partition wall 40 arranged in the housing 28 divide the inner space S in a lower or first chamber Cl, a middle or second chamber C2 and, in an upper or third chamber C3. The lower chamber Cl is between the lower wall 32 and first partition wall 38, the middle chamber C2 is between the two partition walls 38, 40 and, the upper chamber C3 is between the second partition wall 40 and the upper transverse wall 34. The inlet opening 36 opens in the first chamber Cl, the first partition wall 38 is provided with a first aperture 42 creating a first permanent fluid communication between the first chamber Cl and the second chamber C2 and, the second partition wall 40 is provided with a second aperture 44 creating a second permanent fluid communication between the second chamber C2 and the third chamber C3.
The relative dimensions of the Helmholtz resonator 26, the volumes of the chambers, the size of the apertures is tuned as per the use and the nature of the pressure waves to attenuate and, models have been made for a vehicle diesel fuel injection equipment and tests have been conducted successfully for a resonator 26 having a circular inlet opening 36 of 2mm diameter, a circular first aperture 42 of 1mm diameter and, a circular second aperture 44 of 0.6 mm diameter, all three holes being centrally aligned about the main axis X. Also, the first chamber Cl is 20 cm3, the second chamber C2 is 15 cm3 and the third chamber is 10 cm3. Multiple alternatives can be derived from said dimensions, for instance nonaligned or non-circular openings, relative volume of the chambers, the 2mm diameter corresponding to approximately a cross section area of 3 mm2, 1 mm diameter to approximately a cross section area of lmm2 and, 0.6 mm to approximately a cross section area of 0.3 mm2.
Said first embodiment of the Helmholtz resonator 26 is typically designed to be arranged on a pump where the direction of the return fuel flow is aligned to the main axis X.
In another alternative, where said resonator is arranged so the main axis X is perpendicular to the direction of the return flow, the opening 36 can be radially arranged through the cylindrical peripheral wall 30 and open in the first chamber Cl or, as it is represented on figure 4, in the second chamber C2. Moreover, in addition to the opening 36, the resonator 26 can be provided with an outlet 37 also radially arranged through the peripheral wall 30, said outlet 37 opening either in the same chamber as the opening 36 or in another chamber.
The resonator 26 presented comprises three chambers but resonators having two chambers and consequently only one partition wall or, having more than three chambers and consequently more than two partition walls is possible.
The resonator of figure 2 further comprises a flexible damper 46 arranged in the third chamber C3 against a face of the upper transverse wall 34. Said damper 46 captures pressurised gas between said transverse wall 34 and a flexible diaphragm 48 which peripheral edge is fixed to said wall 34 and which central area balloons under the pressure of the gas. The gas pressure is typically in the order of 3 to 5 bar that is the nominal pressure for the system. In use, when a pressure waves propagates it enters the Helmholtz resonator 26 where said wave is firstly dampened in the several chambers and finally via said flexible damper 46 which varies in volume, varying consequently the volume of the third chamber C3.
In a second embodiment presented on figure 3, the resonator 26 is provided with an oscillating damper 49 comprising a sliding piston 50 and a spring 52 arranged in the third chamber C3. The piston 50 divides said third chamber C3 into a first sub-chamber C31 that is below the piston and is limited by the second partition wall 40 and, a second sub-chamber C32 above the piston and limited by the upper transverse wall 34. The piston 50 has a peripheral outer face 54 slidably guided against the inner face of the cylindrical wall 30 and is axially X limited by a lower face 56, that is the ceiling of the first sub-chamber C31 and by an upper transverse face 58 that is the floor of the second sub-chamber C32. The piston 50 is further provided with through passage 60 (two being represented) extending between the lower 56 and the upper 56 faces so that, the sub-chambers
C31, C32 are in fluid communication via said passages 60.
Alternatively to the straight passages 60 represented, the fluid communication could be provided, for instance, by a helix groove arranged on the peripheral outer face of the piston.
The piston is further provided with a spring centering device 62 that is a member centrally protruding from its upper face 58 into the second sub-chamber C32. Said device 62 enables to engage around it the last turns of the spring 52 which on the other end is fixed to the upper transverse wall 34. Thanks to the spring 52, the piston 50 is maintained in the third chamber C3 distant from both the second partition wall 40 and the second transverse wall 34 and, is able to oscillate as a function of the pressure fluctuations entering said third chamber C3.
In an alternative not represented, the spring 52 could be arranged in the first sub-chamber C31, between the lower face 56 of the piston and the second partition wall 40 or, the piston could be arranged between two springs, one in each sub-chambers.
In use, similarly to the embodiment with a flexible damper 46, the pressure fluctuation are dampened in the chambers of the resonator 26 and, finally the piston 50 changes position, varying the relative volumes of the first and the second sub-chambers.
Also the embodiment of figure 3, having an inlet opening 36 through the first transverse face 32 is suited to be arranged aligned with the low pressure flow direction in which pressure fluctuation propagate and, the embodiment of figure 4 having an opening 36 and an outlet 37 both radially opening through the cylindrical peripheral wall 30 in the second chamber C2 is suited to be arranged perpendicular to said low pressure flow direction.
The resonators 26 can be arranged as an added devices components but in alternatives arrangements, the resonator 26 can be made integral to the pump, the housing 28 of the resonator being integrally part to the housing 12 of the pump, the upper transverse wall 34 being screwed, or fixed by other means, to the cylindrical wall 30, the partition walls and dampers being arranged prior to closing the housing 28 by the upper transverse wall 34.
LIST OF REFERENCES
X main axis
S inner space
Cl first chamber
C2 second chamber
C3 third chamber
C31 first sub-chamber
C32 second sub-chamber pumping system housing camshaft front bearing rear bearing compression chamber inlet outlet attenuator - Helmholtz resonator housing of the resonator cylindrical wall lower, first, transverse wall upper, second, transverse wall opening outlet first partition wall second partition wall first aperture second aperture flexible damper diaphragm oscillating damper piston spring peripheral outer face of the piston 56 lower face of the piston upper face of the piston passage spring centring device

Claims (18)

1. Helmholtz resonator (26) adapted to attenuate pressure fluctuations propagating in an injection fuel equipment, said Helmholtz resonator (26) having a peripheral wall (30, 32, 34) enclosing an inner space (S), an opening (36) arranged through said peripheral wall (30, 32, 34) for enabling a fluid communication with said inner space (S), characterised in that the Helmholtz resonator (26) further comprises at least one partition wall (38) dividing said inner space in distinct chambers (Cl, C2), said partition wall (38) being provided with an aperture (42) creating an internal fluid communication between said distinct chambers, the opening (36) opening in one of the chambers.
2. Helmholtz resonator (26) as claimed in the preceding claim wherein the peripheral walls (30, 32, 34) comprise a cylindrical wall (30) extending along a main axis (X) from a first transverse end (32) wall to a distant second transverse end wall (34).
3. Helmholtz resonator (26) as claimed in claim 2 wherein said at least one partition wall (38) is substantially parallel to any one of the transverse end walls (32, 34).
4. Helmholtz resonator (26) as claimed in any one of the preceding claims comprising a first (Cl) and a second (C2) chambers in fluid communication between each other’s via a first aperture (42) arranged in a first partition wall (38) and, a third chamber (C3) in fluid communication with the second chamber (C2) via a second aperture (44) arranged in a second partition wall (40).
5. Helmholtz resonator (26) as claimed in claim 4 wherein the first (38) and second (40) partition walls are substantially parallel to each other’s, the second chamber (C2) being interposed between the first chamber (Cl) and the third chamber (C3).
6. Helmholtz resonator (26) as claimed in any one of the claims 4 or 5 wherein the first chamber (Cl) is larger than the second chamber (C2) and, the second chamber (C2) is larger than the third chamber (C3).
7. Helmholtz resonator (26) as claimed in any one of the claims 4 to 6 β
wherein the volume of the first chamber (Cl) is about 20 cm and, the volume of β
the third chamber (C3) is about 10 cm .
8. Helmholtz resonator (26) as claimed in any one of the claims 4 to 7 wherein the first aperture (42) has across section area of about 1 mm2 and, the second aperture (44) has across section area of about 0.3 mm2.
9. Helmholtz resonator (26) as claimed in any one of the claims 4 to 8 comprising more than three distinct chambers.
10. Helmholtz resonator (26) as claimed in any one of the claims 4 to 9 wherein the opening (36) is arranged to open in the first chamber (Cl).
11. Helmholtz resonator (26) as claimed in claim 10 wherein cross section area of the opening (36) is about 3 mm2.
12. Helmholtz resonator (26) as claimed in any one of the claims 4 to 9 further comprising an outlet (37) arranged in a peripheral wall (30) for enabling a fluid communication with said inner space (S).
13. Helmholtz resonator (26) as claimed in claim 12 wherein the opening (36) and the outlet (37) open in the same chamber.
14. Helmholtz resonator (26) as claimed in claim 13 wherein the opening (36) and the outlet (37) both open in the second chamber (C2).
15. Helmholtz resonator (26) as claimed in any one of the preceding claims further comprising a damper (46, 49) arranged in one of the chambers, said damper moving as a function of the pressure fluctuations.
5
16. Helmholtz resonator (26) as claimed in claim 15 wherein said damper (46) comprises a gas fdled diaphragm (48).
17. Helmholtz resonator (26) as claimed in claim 15 wherein said damper is a viscous damper (49) comprising a slidable piston (50) dividing the chamber in
10 which it is arranged in a first sub-chamber (C31) and a second sub-chamber (C32) in fluid communication with each other’s via a communication passage (60), said viscous damper (49) further comprising a spring (62) arranged between said piston (50) and a wall of said chamber in which the piston is arranged so that, the volume of the sub-chambers (C31, C32) vary relative to each other’s as a function
15 of the pressure fluctuations.
18. Fuel pump (10) of a fuel injection equipment wherein fuel entering via a pump inlet (22), is pressurised in a compression chamber (20) and is expelled via a pump outlet (24), a camshaft (14) rotating, in use, between a front (16) and a
20 rear (18) bearings urging a reciprocating piston to vary the volume of said compression chamber, the pump (10) further comprising a Helmholtz resonator (26) as set in any one of the preceding claims arranged to attenuate pressure fluctuations in said pump.
Intellectual
Property
Office
Application No: GB1620499.2 Examiner: Mr Tony Walbeoff
GB1620499.2A 2016-12-02 2016-12-02 Multi-Chamber Helmholtz Resonator Expired - Fee Related GB2557264B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB1620499.2A GB2557264B (en) 2016-12-02 2016-12-02 Multi-Chamber Helmholtz Resonator
PCT/EP2017/080235 WO2018099802A1 (en) 2016-12-02 2017-11-23 Multi-chamber helmholtz resonator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1620499.2A GB2557264B (en) 2016-12-02 2016-12-02 Multi-Chamber Helmholtz Resonator

Publications (4)

Publication Number Publication Date
GB201620499D0 GB201620499D0 (en) 2017-01-18
GB2557264A true GB2557264A (en) 2018-06-20
GB2557264A8 GB2557264A8 (en) 2018-07-25
GB2557264B GB2557264B (en) 2020-04-08

Family

ID=58159620

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1620499.2A Expired - Fee Related GB2557264B (en) 2016-12-02 2016-12-02 Multi-Chamber Helmholtz Resonator

Country Status (2)

Country Link
GB (1) GB2557264B (en)
WO (1) WO2018099802A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11867139B1 (en) 2022-06-17 2024-01-09 Blue Origin, Llc Multi-volume acoustic resonator for rocket engine

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2642204A1 (en) * 2012-03-21 2013-09-25 Alstom Technology Ltd Simultaneous broadband damping at multiple locations in a combustion chamber
EP2816289A1 (en) * 2013-05-24 2014-12-24 Alstom Technology Ltd Damper for gas turbine
US20160003162A1 (en) * 2013-02-28 2016-01-07 Siemens Aktiengesellschaft Damping device for a gas turbine, gas turbine and method for damping thermoacoustic oscillations
EP3029377A1 (en) * 2014-12-03 2016-06-08 Alstom Technology Ltd Damper for a gas turbine
EP3029376A1 (en) * 2014-12-01 2016-06-08 Alstom Technology Ltd Helmholtz damper and gas turbine with such a helmholtz damper

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3324805A1 (en) * 1983-07-09 1985-01-17 Betriebsforschungsinstitut VDEh - Institut für angewandte Forschung GmbH, 4000 Düsseldorf Device for the prevention of pressure fluctuations in combustion chambers
JP3343871B2 (en) * 1993-07-21 2002-11-11 富士重工業株式会社 Resonant silencer in the intake system of a car engine
JP3511828B2 (en) * 1996-06-24 2004-03-29 三菱自動車工業株式会社 Fuel system and fuel pump
JP2000291509A (en) * 1999-04-01 2000-10-17 Mitsubishi Electric Corp Fuel supply device for direct injection type gasoline engine
DE102005062284B4 (en) * 2005-12-24 2019-02-28 Ansaldo Energia Ip Uk Limited Combustion chamber for a gas turbine
EP2397760B1 (en) * 2010-06-16 2020-11-18 Ansaldo Energia IP UK Limited Damper Arrangement and Method for Designing Same
RU2635858C2 (en) * 2012-03-30 2017-11-16 АНСАЛДО ЭНЕРДЖИА АйПи ЮКей ЛИМИТЕД Combustion chamber sealing segments, equipped with damping devices

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2642204A1 (en) * 2012-03-21 2013-09-25 Alstom Technology Ltd Simultaneous broadband damping at multiple locations in a combustion chamber
US20160003162A1 (en) * 2013-02-28 2016-01-07 Siemens Aktiengesellschaft Damping device for a gas turbine, gas turbine and method for damping thermoacoustic oscillations
EP2816289A1 (en) * 2013-05-24 2014-12-24 Alstom Technology Ltd Damper for gas turbine
EP3029376A1 (en) * 2014-12-01 2016-06-08 Alstom Technology Ltd Helmholtz damper and gas turbine with such a helmholtz damper
EP3029377A1 (en) * 2014-12-03 2016-06-08 Alstom Technology Ltd Damper for a gas turbine

Also Published As

Publication number Publication date
GB2557264A8 (en) 2018-07-25
GB201620499D0 (en) 2017-01-18
GB2557264B (en) 2020-04-08
WO2018099802A1 (en) 2018-06-07

Similar Documents

Publication Publication Date Title
US20200088214A1 (en) Systems and methods for managing noise in compact high speed and high force hydraulic actuators
EP3048332A1 (en) Vibration-damping device
US9772003B2 (en) Vibration damping device
KR20010075241A (en) Flat tubular pressure damper for damping fluid pressure oscillations in fluid lines
EP3088767B1 (en) Vibration-damping device
US8591208B2 (en) Multi-frequency pulsation absorber at cylinder valve cap
KR20020056886A (en) Device for reducing pressure pulsations in hydraulic manifolds
GB2557264A (en) Multibody helmholtz resonator
CZ296982B6 (en) High-pressure fuel accumulator
CN109416009A (en) High-pressure fuel pump
US9951842B2 (en) Vibration-damping device
CN108138891B (en) Vibration damping support device
JP2021085526A (en) Separating element for anti-vibration hydraulic module and anti-vibration hydraulic module equipped with such separating element
US8573061B2 (en) Pressure indicator
JP2016044776A (en) Pressure buffer device
CN105765209A (en) Fuel injection system and method for operating the fuel injection system
CN105339659B (en) Pump
CN103759094B (en) A kind of pipeline for clutch system
EP1805411B1 (en) Pressure vibration dampener for an internal combustion engine fuel injection system
CN109923310B (en) Noise silencer
CN114402148B (en) Vibration isolation device
EP3112664B1 (en) Fluid pump
KR102239573B1 (en) Resonance Effect Type Fuel Rail and Common Rail System Thereof
CN108027088B (en) Pressure-control valve
US10145345B2 (en) Fluid conveyance system for a fluid

Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)

Free format text: REGISTERED BETWEEN 20190222 AND 20190227

PCNP Patent ceased through non-payment of renewal fee

Effective date: 20201202