GB8331909D0 - Silencer for high velocity gas flow - Google Patents

Silencer for high velocity gas flow

Info

Publication number
GB8331909D0
GB8331909D0 GB838331909A GB8331909A GB8331909D0 GB 8331909 D0 GB8331909 D0 GB 8331909D0 GB 838331909 A GB838331909 A GB 838331909A GB 8331909 A GB8331909 A GB 8331909A GB 8331909 D0 GB8331909 D0 GB 8331909D0
Authority
GB
United Kingdom
Prior art keywords
silencer
gas flow
high velocity
velocity gas
flow
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
GB838331909A
Other versions
GB2132269B (en
GB2132269A (en
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.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
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 UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Priority to GB08331909A priority Critical patent/GB2132269B/en
Publication of GB8331909D0 publication Critical patent/GB8331909D0/en
Publication of GB2132269A publication Critical patent/GB2132269A/en
Application granted granted Critical
Publication of GB2132269B publication Critical patent/GB2132269B/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • F02K1/34—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for attenuating noise
GB08331909A 1982-12-03 1983-11-30 Silencer for high velocity gas flow Expired GB2132269B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08331909A GB2132269B (en) 1982-12-03 1983-11-30 Silencer for high velocity gas flow

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8234633 1982-12-03
GB08331909A GB2132269B (en) 1982-12-03 1983-11-30 Silencer for high velocity gas flow

Publications (3)

Publication Number Publication Date
GB8331909D0 true GB8331909D0 (en) 1984-01-04
GB2132269A GB2132269A (en) 1984-07-04
GB2132269B GB2132269B (en) 1986-07-30

Family

ID=26284592

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08331909A Expired GB2132269B (en) 1982-12-03 1983-11-30 Silencer for high velocity gas flow

Country Status (1)

Country Link
GB (1) GB2132269B (en)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2405666A (en) * 2003-09-05 2005-03-09 Dunlop Aerospace Ltd Noise attenuator, eg for turbofan engine air bleed system
GB0505246D0 (en) 2005-03-15 2005-04-20 Rolls Royce Plc Engine noise
US7946104B2 (en) * 2006-05-12 2011-05-24 Rohr, Inc. Bleed air relief system for engines
GB0614360D0 (en) 2006-07-20 2006-08-30 Rolls Royce Plc Aeroengine bleed valve
GB0616847D0 (en) 2006-08-25 2006-10-04 Rolls Royce Plc Aeroengine bleed valve
GB2443418B (en) * 2006-11-02 2011-05-04 Rolls Royce Plc An acoustic arrangement
GB0801301D0 (en) 2008-01-25 2008-03-05 Rolls Royce Plc Aeroengine bleed valve
GB0820598D0 (en) 2008-11-11 2008-12-17 Rolls Royce Plc A noise reduction device
GB0820597D0 (en) 2008-11-11 2008-12-17 Rolls Royce Plc A noise reduction device
GB2468669C (en) * 2009-03-17 2013-11-13 Rolls Royce Plc A flow discharge device
DE102011018932B4 (en) * 2011-04-28 2018-07-12 Multivac Sepp Haggenmüller Se & Co. Kg Silencer and packaging machine with such a silencing device
WO2014134134A1 (en) * 2013-03-01 2014-09-04 United Technologies Corporation Gas turbine engine anti-surge valve discharge tube
GB201322833D0 (en) * 2013-12-23 2014-02-12 Rolls Royce Plc
EP3323726A1 (en) * 2016-11-22 2018-05-23 Airbus Defence and Space SA An aircraft with turboprop engines having active means to avoid damages caused by ice impacts
GB201806461D0 (en) * 2018-04-20 2018-06-06 Rolls Royce Plc Gas turbine engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB465071A (en) * 1935-12-04 1937-04-30 Bristol Aeroplane Co Ltd Improvements in exhaust systems for internal-combustion engines
GB477245A (en) * 1936-07-29 1937-12-24 Karl Kaup Silencer especially for damping the noise of the exhaust of internal combustion engines
GB878480A (en) * 1957-12-18 1961-10-04 Rockwell Standard Co A compacted foraminous body suitable for use as a sound attenuating device
SE359367B (en) * 1969-07-11 1973-08-27 Munters C

Also Published As

Publication number Publication date
GB2132269B (en) 1986-07-30
GB2132269A (en) 1984-07-04

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Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19961130