GB201611749D0 - Unitary exhaust - Google Patents

Unitary exhaust

Info

Publication number
GB201611749D0
GB201611749D0 GBGB1611749.1A GB201611749A GB201611749D0 GB 201611749 D0 GB201611749 D0 GB 201611749D0 GB 201611749 A GB201611749 A GB 201611749A GB 201611749 D0 GB201611749 D0 GB 201611749D0
Authority
GB
United Kingdom
Prior art keywords
unitary exhaust
unitary
exhaust
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.)
Withdrawn
Application number
GBGB1611749.1A
Other versions
GB2553493A (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.)
Binns Jason K
Original Assignee
Binns Jason K
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
Publication of GB201611749D0 publication Critical patent/GB201611749D0/en
Application filed by Binns Jason K filed Critical Binns Jason K
Priority to GB1611749.1A priority Critical patent/GB2553493A/en
Publication of GB2553493A publication Critical patent/GB2553493A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/02—Plural gas-turbine plants having a common power output
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/14—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, fuselages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
GB1611749.1A 2016-09-08 2016-09-08 Unitary exhaust Withdrawn GB2553493A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1611749.1A GB2553493A (en) 2016-09-08 2016-09-08 Unitary exhaust

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1611749.1A GB2553493A (en) 2016-09-08 2016-09-08 Unitary exhaust

Publications (2)

Publication Number Publication Date
GB201611749D0 true GB201611749D0 (en) 2016-08-17
GB2553493A GB2553493A (en) 2018-03-14

Family

ID=56891086

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1611749.1A Withdrawn GB2553493A (en) 2016-09-08 2016-09-08 Unitary exhaust

Country Status (1)

Country Link
GB (1) GB2553493A (en)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB598698A (en) * 1946-03-12 1948-02-24 Bristol Aeroplane Co Ltd Improvements in or relating to gas turbine power plants, particularly for aircraft
GB2050260B (en) * 1979-05-29 1983-06-22 Rolls Royce V/stol aircraft
US7752834B2 (en) * 2006-10-25 2010-07-13 United Technologies Corporation Aircraft propulsion systems
US8015796B2 (en) * 2007-06-05 2011-09-13 United Technologies Corporation Gas turbine engine with dual fans driven about a central core axis
DE102008011643A1 (en) * 2008-02-28 2009-09-03 Rolls-Royce Deutschland Ltd & Co Kg Aircraft drive unit with multi-fan design

Also Published As

Publication number Publication date
GB2553493A (en) 2018-03-14

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Legal Events

Date Code Title Description
AAF Amended application filed

Free format text: CORRECTION: APPLICATION GB1611749.1 WAS ADVERTISED IN THE PATENTS DESIGNS JOURNAL NO. 6639 ON 17.08.2016 AS BEING ORIGINALLY FILED ON 6 JULY 2016, THIS HAS BEEN RE-DATED TO 8 SEPTEMBER 2016 FOLLOWING THE FILING OF MISSING DRAWINGS.

WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)