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PATENTS 12 Sealing Technology February 2006 Patents Free piston with time-varying clearance seal Applicant: Praxair Technology Inc, USA This invention relates generally to free piston devices, and is particu- larly useful for a piston employed with a linear motor for providing acoustic energy to a cryocooler. Free piston devices use reciprocating pis- tons or displacers, but rely on the overall system dynamics to guaran- tee the proper motion amplitude and phase of different system com- ponents. As such, there is no natur- al constraint on piston mean posi- tion, which may drift off-center even if the dynamics are properly executed. In a reciprocating free piston device with clearance seals, the pistons will tend to drift toward the side with the greater oscillating pressure. This is understood to be due to the higher density of the gas flowing through the seal during the half-cycle where the high oscillating pressure side is high, versus the reverse flow in the other half of the cycle. The invention makes use of the discovery that hollow pistons can flex in response to a pressure difference across the piston shell, so that in the presence of oscillating pressure the shell expands during one half-cycle, thus narrowing the seal gap, and contracts during the other half-cycle, thus increasing the seal gap. In most devices with hol- low pistons, this results in increased unbalanced mass flux through the seal and increased piston drift. This invention embodies the recogni- tion that a piston can be devised that reverses the usual pressure gra- dient on the piston shell, causing the seal gap to tighten when the pressure is high in front, and vice versa. This essentially makes the piston seal itself behave like a check-valve, reducing flow in the direction that normally causes pis- ton drift/offset. Patent number: WO 2005/089328 Inventor: P.S. Spoor Publication date: 29 September 2005 Trocar seal for surgical procedures Applicant: Neosurg Technologies Inc, USA A trocar seal is described that is for use in laparoscopic surgery, particu- larly to prevent the escape of insulat- ing gas during the performance of surgical procedures. The diameter is expandable from 2 mm to about 13 mm. It is preferably fabricated from silicone and coated with paralene or another approved coating. Patent number: WO 2005/094432 Inventor: P.T. O’Heeron Publication date: 13 October 2005 Seal for gap between two adjacent components Applicant: Alstom Technology Ltd, Switzerland The invention relates to a seal for sealing a gap between adjacent components, in a turbine or turbo compressor. It is applicable to com- ponents such as guide vanes or rotor blades or a heat shield. The design is intended to maintain an effective seal during relative move- ment of the sealed components due to thermal expansion. A number of different detail designs are included in the patent. Patent number: WO 2005/095763 Inventors: S. Olmes, M. Richter and T. Zierer Publication date: 13 October 2005 Applicant: Gore Enterprise Holdings, USA This patent describes an expanded PTFE tape that is particularly intended for use on large flanges requiring a conformable gasket that will function with low sealing stress. The tape includes a layer that has low air permeability. A decrease in leak rate of about 1.5 orders of magnitude has been demonstrated. Patent number: WO 2005/103533 Inventor: K.E. Dove Publication date: 3 November 2005 Seal removal tool for aircraft air compressors Applicant: Honeywell International Inc, USA This patent describes a tool that is designed for removing the mechan- ical seal from an aircraft air cycle machine (ACM), the turbocom- pressors used for cabin air supply etc., without damaging the seal. This can help prevent unwanted debris being left within the machine. Also, as the seals are gen- erally relatively expensive to replace, if it is undamaged it is preferable for the seal not to be damaged during the removal process, so that it can be reused when the ACM is reassembled. The seal has a grooved inner surface, and the removal tool has matching grooves on retractable fingers. To remove the seal the fin- gers of the tool can be expanded to contact the seal. The method of operation and variants of the tool are covered in considerable detail. Patent number: WO 2005/097412 Inventors: J.T. Chan, J.M. Hurlbut and R.S. Stoltz Publication date: 20 October 2005 Editor’s comment: This appears to be a potentially useful technique for remov- ing seals from a location with difficult access. I am sure, like me, you will be pleased to learn how much the aero- space industry is interested in saving money by reusing dismantled seals. Free piston designed to distort in response to the pressure differential and maintain the correct pressure balance, from WO 2005/089328. Example of the seal removal tool disclosed in WO 2005/097412, showing the grooved fingers that are expanded to mate with the seal. Coil gasket utilizing expanded PTFE tape

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Page 1: Coil gasket utilizing expanded PTFE tape

PATENTS

12Sealing Technology February 2006

PatentsFree piston with time-varying clearance seal

Applicant: PraxairTechnology Inc, USA

This invention relates generally tofree piston devices, and is particu-larly useful for a piston employedwith a linear motor for providingacoustic energy to a cryocooler. Freepiston devices use reciprocating pis-tons or displacers, but rely on theoverall system dynamics to guaran-tee the proper motion amplitudeand phase of different system com-ponents. As such, there is no natur-al constraint on piston mean posi-tion, which may drift off-centereven if the dynamics are properlyexecuted. In a reciprocating freepiston device with clearance seals,the pistons will tend to drift towardthe side with the greater oscillatingpressure. This is understood to bedue to the higher density of the gasflowing through the seal during thehalf-cycle where the high oscillatingpressure side is high, versus thereverse flow in the other half of thecycle. The invention makes use of

the discovery that hollow pistonscan flex in response to a pressuredifference across the piston shell, sothat in the presence of oscillatingpressure the shell expands duringone half-cycle, thus narrowing theseal gap, and contracts during theother half-cycle, thus increasing theseal gap. In most devices with hol-low pistons, this results in increasedunbalanced mass flux through theseal and increased piston drift. Thisinvention embodies the recogni-tion that a piston can be devisedthat reverses the usual pressure gra-dient on the piston shell, causingthe seal gap to tighten when thepressure is high in front, and viceversa. This essentially makes thepiston seal itself behave like acheck-valve, reducing flow in thedirection that normally causes pis-ton drift/offset.Patent number: WO 2005/089328Inventor: P.S. SpoorPublication date:

29 September 2005

Trocar seal for surgical procedures

Applicant: NeosurgTechnologies Inc, USA

A trocar seal is described that is foruse in laparoscopic surgery, particu-larly to prevent the escape of insulat-ing gas during the performance ofsurgical procedures. The diameter is

expandable from 2 mm to about 13mm. It is preferably fabricated fromsilicone and coated with paralene oranother approved coating.Patent number: WO 2005/094432Inventor: P.T. O’HeeronPublication date: 13 October 2005

Seal for gap between two adjacent components

Applicant: Alstom TechnologyLtd, Switzerland

The invention relates to a seal forsealing a gap between adjacentcomponents, in a turbine or turbocompressor. It is applicable to com-ponents such as guide vanes orrotor blades or a heat shield. Thedesign is intended to maintain an

effective seal during relative move-ment of the sealed components dueto thermal expansion. A number ofdifferent detail designs are includedin the patent.Patent number: WO 2005/095763Inventors: S. Olmes, M. Richter

and T. ZiererPublication date: 13 October 2005

Applicant: Gore EnterpriseHoldings, USA

This patent describes an expandedPTFE tape that is particularlyintended for use on large flangesrequiring a conformable gasketthat will function with low sealingstress. The tape includes a layer

that has low air permeability. Adecrease in leak rate of about 1.5orders of magnitude has beendemonstrated.Patent number: WO 2005/103533Inventor: K.E. DovePublication date:

3 November 2005

Seal removal tool for aircraft air compressors

Applicant: HoneywellInternational Inc, USA

This patent describes a tool that isdesigned for removing the mechan-ical seal from an aircraft air cyclemachine (ACM), the turbocom-pressors used for cabin air supplyetc., without damaging the seal.This can help prevent unwanteddebris being left within themachine. Also, as the seals are gen-erally relatively expensive to replace,if it is undamaged it is preferable forthe seal not to be damaged duringthe removal process, so that it canbe reused when the ACM isreassembled. The seal has a groovedinner surface, and the removal tool

has matching grooves on retractablefingers. To remove the seal the fin-gers of the tool can be expanded tocontact the seal. The method ofoperation and variants of the toolare covered in considerable detail.Patent number: WO 2005/097412Inventors: J.T. Chan, J.M. Hurlbut

and R.S. StoltzPublication date: 20 October 2005

Editor’s comment: This appears to be apotentially useful technique for remov-ing seals from a location with difficultaccess. I am sure, like me, you will bepleased to learn how much the aero-space industry is interested in savingmoney by reusing dismantled seals.

Free piston designed to distort in response to the pressure differentialand maintain the correct pressure balance, from WO 2005/089328.

Example of the seal removal tool disclosed in WO 2005/097412, showingthe grooved fingers that are expanded to mate with the seal.

Coil gasket utilizing expanded PTFE tape