GB2010969A - Mounting for Gas Turbine Jet Propulsion Engine - Google Patents

Mounting for Gas Turbine Jet Propulsion Engine

Info

Publication number
GB2010969A
GB2010969A GB7849176A GB7849176A GB2010969A GB 2010969 A GB2010969 A GB 2010969A GB 7849176 A GB7849176 A GB 7849176A GB 7849176 A GB7849176 A GB 7849176A GB 2010969 A GB2010969 A GB 2010969A
Authority
GB
United Kingdom
Prior art keywords
engine
mounting
pylon
gas turbine
pivoted
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Withdrawn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
GB7849176A
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB7849176A priority Critical patent/GB2010969A/en
Publication of GB2010969A publication Critical patent/GB2010969A/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Withdrawn legal-status Critical Current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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The engine is connected through pylon 11 to an aircraft wing by a mounting in which the engine thrust X is transmitted to the pylon by two links arranged at opposite sides of the engine and lying in a plane oblique to the engine axis D. The ends 26 of the links nearer to axis D are pivoted to engine casing 22 whilst the other ends 27 are connected to the ends of a bellcrank lever 28 itself pivoted at 28A to strut 18 pivoted to pylon 11. Bending of casing 22 in the horizontal plane places the two oblique links respectively into tension and compression and results in corresponding pivoting of lever 28. <IMAGE>
GB7849176A 1977-12-22 1978-12-19 Mounting for Gas Turbine Jet Propulsion Engine Withdrawn GB2010969A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7849176A GB2010969A (en) 1977-12-22 1978-12-19 Mounting for Gas Turbine Jet Propulsion Engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB5388377 1977-12-22
GB7849176A GB2010969A (en) 1977-12-22 1978-12-19 Mounting for Gas Turbine Jet Propulsion Engine

Publications (1)

Publication Number Publication Date
GB2010969A true GB2010969A (en) 1979-07-04

Family

ID=26267360

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7849176A Withdrawn GB2010969A (en) 1977-12-22 1978-12-19 Mounting for Gas Turbine Jet Propulsion Engine

Country Status (1)

Country Link
GB (1) GB2010969A (en)

Cited By (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2451461A1 (en) * 1979-03-10 1980-10-10 Rolls Royce ASSEMBLY OF TURBOMACHINE ENGINE GROUP
FR2479902A1 (en) * 1980-04-02 1981-10-09 United Technologies Corp CARTER DEVIATION CONTROL STRUCTURE FOR AIRCRAFT GAS TURBINES
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet
EP0132214A1 (en) * 1983-07-14 1985-01-23 United Technologies Corporation Load sharing for engine nacelle
EP0147878A1 (en) * 1983-12-30 1985-07-10 The Boeing Company System for mounting a jet engine
US4560122A (en) * 1983-01-12 1985-12-24 British Aerospace Public Limited Company Power plant attachment arrangements for aircraft wings
GB2202279A (en) * 1987-03-13 1988-09-21 Gen Electric Vibration isolating aircraft engine mount
GB2220034A (en) * 1988-06-22 1989-12-28 Rolls Royce Plc Load transmission in gas turbine engines
US5028001A (en) * 1987-03-13 1991-07-02 General Electric Company Method of vibration isolating an aircraft engine
EP0564126A1 (en) * 1992-03-25 1993-10-06 General Electric Company Aircraft engine thrust mount
FR2698848A1 (en) * 1992-12-07 1994-06-10 Aerospatiale Aircraft engine thrust balance - comprises two connecting liquid chambers with pistons joined to connecting rods fixed to engine
WO1996018538A1 (en) * 1994-12-12 1996-06-20 United Technologies Corporation A mounting arrangement for a gas turbine engine
FR2732947A1 (en) * 1995-04-13 1996-10-18 Rolls Royce Plc Mounting for fixing turbofan engine on airframe
EP0805108A3 (en) * 1996-05-01 1999-01-07 The Boeing Company Aircraft engine thrust mount
WO2000017049A1 (en) * 1998-09-18 2000-03-30 Lord Corporation Multi-linkage suspension system including outboard isolators
GB2351480A (en) * 1999-06-30 2001-01-03 Seneca Tech Ltd Aircraft engine mounting
EP1031507A3 (en) * 1999-02-26 2001-02-28 The Boeing Company Tuned engine mounting system for jet aircraft
WO2007033994A1 (en) * 2005-09-26 2007-03-29 Airbus France Engine assembly for aircraft comprising an engine as well as a device for locking said engine
FR2891251A1 (en) * 2005-09-28 2007-03-30 Airbus France Sas ENGINE ATTACHING MAT FOR AN AIRCRAFT
FR2891804A1 (en) * 2005-10-12 2007-04-13 Airbus France Sas NARROW SYSTEM AND AIRCRAFT ENGINE HITTING MATERIAL COMPRISING SUCH A SYSTEM
FR2915177A1 (en) * 2007-04-20 2008-10-24 Airbus France Sa AIRCRAFT ENGINE AND AIRCRAFT ENGINE CLAMPING DEVICE COMPRISING AT LEAST ONE SUCH DEVICE
US20090056343A1 (en) * 2007-08-01 2009-03-05 Suciu Gabriel L Engine mounting configuration for a turbofan gas turbine engine
EP1627812A3 (en) * 2004-08-19 2009-03-18 Rolls-Royce Plc An engine mounting assembly
EP2062819A1 (en) * 2007-11-23 2009-05-27 Snecma Jet engine hanging from an aircraft pylon
FR2925016A1 (en) * 2007-12-12 2009-06-19 Snecma Sa Isostatic jet engine pylon suspension for aircraft, has front attachment with beam transversal with respect to axis, where plane formed by rods of front attachment and transmission rod are convergent in point on axis of motor or near axis
FR2926536A1 (en) * 2008-01-23 2009-07-24 Snecma Sa ATTACHING A PROPULSIVE SYSTEM TO A STRUCTURE ELEMENT OF AN AIRCRAFT
EP2103516A2 (en) * 2008-03-21 2009-09-23 United Technologies Corporation Mounting system for a gas turbine engine
DE102009054568A1 (en) * 2009-12-11 2011-06-16 Rolls-Royce Deutschland Ltd & Co Kg Device for suspending a jet engine on a support structure
CN101484357B (en) * 2006-07-10 2011-09-21 法国空中客车公司 Aircraft engine attachment device comprising two thrust-reacting link rods that fit together transversely
US20120012694A1 (en) * 2010-07-14 2012-01-19 Spirit Aerosystems, Inc. Fail-safe aircraft engine mounting apparatus
US8342473B2 (en) 2008-06-13 2013-01-01 Rolls-Royce Plc Thrust mounting arrangement
DE102012014108A1 (en) * 2012-07-17 2014-01-23 Rolls-Royce Deutschland Ltd & Co Kg Transport safety device of an aircraft gas turbine
US20140047850A1 (en) * 2012-08-17 2014-02-20 United Technologies Corporation Assembly for mounting a turbine engine to an airframe
US8844265B2 (en) 2007-08-01 2014-09-30 United Technologies Corporation Turbine section of high bypass turbofan
EP2639159A3 (en) * 2012-03-16 2017-04-12 The Boeing Company Engine mounting system for an aircraft
US10060357B2 (en) 2007-08-01 2018-08-28 United Technologies Corporation Turbine section of high bypass turbofan
EP3587749A1 (en) * 2018-06-28 2020-01-01 Rolls-Royce plc Gas turbine engine
US11149650B2 (en) 2007-08-01 2021-10-19 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11242805B2 (en) 2007-08-01 2022-02-08 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11273923B2 (en) 2019-07-12 2022-03-15 Spirit Aerosystems, Inc. Fail-safe engine support system
US11346289B2 (en) 2007-08-01 2022-05-31 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11486311B2 (en) 2007-08-01 2022-11-01 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US20230113400A1 (en) * 2021-09-20 2023-04-13 Airbus Operations (S.A.S.) Aircraft propulsion assembly comprising a thrust force uptake device
FR3133375A1 (en) * 2022-03-11 2023-09-15 Airbus Operations (S.A.S.) Compact electric propulsion assembly comprising an isostatic motor attachment, aircraft comprising at least one such electric propulsion assembly

Cited By (83)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2451461A1 (en) * 1979-03-10 1980-10-10 Rolls Royce ASSEMBLY OF TURBOMACHINE ENGINE GROUP
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet
FR2479902A1 (en) * 1980-04-02 1981-10-09 United Technologies Corp CARTER DEVIATION CONTROL STRUCTURE FOR AIRCRAFT GAS TURBINES
US4560122A (en) * 1983-01-12 1985-12-24 British Aerospace Public Limited Company Power plant attachment arrangements for aircraft wings
EP0132214A1 (en) * 1983-07-14 1985-01-23 United Technologies Corporation Load sharing for engine nacelle
EP0147878A1 (en) * 1983-12-30 1985-07-10 The Boeing Company System for mounting a jet engine
US5028001A (en) * 1987-03-13 1991-07-02 General Electric Company Method of vibration isolating an aircraft engine
GB2202279A (en) * 1987-03-13 1988-09-21 Gen Electric Vibration isolating aircraft engine mount
US4875655A (en) * 1987-03-13 1989-10-24 General Electric Company Vibration isolating engine mount
GB2202279B (en) * 1987-03-13 1991-11-06 Gen Electric Vibration isolating engine mount
GB2220034A (en) * 1988-06-22 1989-12-28 Rolls Royce Plc Load transmission in gas turbine engines
US4984423A (en) * 1988-06-22 1991-01-15 Rolls-Royce Plc Aerodynamic loading in gas turbine engines
GB2220034B (en) * 1988-06-22 1992-12-02 Rolls Royce Plc Aerodynamic loading in gas turbine engines
EP0564126A1 (en) * 1992-03-25 1993-10-06 General Electric Company Aircraft engine thrust mount
FR2698848A1 (en) * 1992-12-07 1994-06-10 Aerospatiale Aircraft engine thrust balance - comprises two connecting liquid chambers with pistons joined to connecting rods fixed to engine
WO1996018538A1 (en) * 1994-12-12 1996-06-20 United Technologies Corporation A mounting arrangement for a gas turbine engine
FR2732947A1 (en) * 1995-04-13 1996-10-18 Rolls Royce Plc Mounting for fixing turbofan engine on airframe
EP0805108A3 (en) * 1996-05-01 1999-01-07 The Boeing Company Aircraft engine thrust mount
WO2000017049A1 (en) * 1998-09-18 2000-03-30 Lord Corporation Multi-linkage suspension system including outboard isolators
US6328293B1 (en) 1998-09-18 2001-12-11 Lord Corporation Multi-linkage suspension system including outboard isolators
EP1031507A3 (en) * 1999-02-26 2001-02-28 The Boeing Company Tuned engine mounting system for jet aircraft
GB2351480B (en) * 1999-06-30 2002-09-25 Seneca Tech Ltd Aircraft engine mounting
GB2351480A (en) * 1999-06-30 2001-01-03 Seneca Tech Ltd Aircraft engine mounting
US7806363B2 (en) 2004-08-19 2010-10-05 Rolls-Royce Plc Engine mounting assembly
EP1627812A3 (en) * 2004-08-19 2009-03-18 Rolls-Royce Plc An engine mounting assembly
WO2007033994A1 (en) * 2005-09-26 2007-03-29 Airbus France Engine assembly for aircraft comprising an engine as well as a device for locking said engine
FR2891246A1 (en) * 2005-09-26 2007-03-30 Airbus France Sas ENGINE ASSEMBLY FOR AN AIRCRAFT COMPRISING AN ENGINE AND A DEVICE FOR HITCHING SUCH AN ENGINE
CN101263053B (en) * 2005-09-26 2012-05-30 空中客车运营简化股份公司 Engine assembly for aircraft comprising an engine as well as a device for assembling said engine
US8042342B2 (en) 2005-09-26 2011-10-25 Airbus Operations Sas Engine assembly for aircraft comprising an engine as well as a device for locking said engine
US7445179B2 (en) 2005-09-28 2008-11-04 Airbus France Engine assembly for aircraft
FR2891251A1 (en) * 2005-09-28 2007-03-30 Airbus France Sas ENGINE ATTACHING MAT FOR AN AIRCRAFT
FR2891804A1 (en) * 2005-10-12 2007-04-13 Airbus France Sas NARROW SYSTEM AND AIRCRAFT ENGINE HITTING MATERIAL COMPRISING SUCH A SYSTEM
WO2007042508A1 (en) * 2005-10-12 2007-04-19 Airbus France Nut system and aircraft engine mounting structure comprising same
US8042764B2 (en) 2005-10-12 2011-10-25 Airbus Operations Sas Nut system and aircraft engine mounting structure comprising same
CN101484357B (en) * 2006-07-10 2011-09-21 法国空中客车公司 Aircraft engine attachment device comprising two thrust-reacting link rods that fit together transversely
FR2915177A1 (en) * 2007-04-20 2008-10-24 Airbus France Sa AIRCRAFT ENGINE AND AIRCRAFT ENGINE CLAMPING DEVICE COMPRISING AT LEAST ONE SUCH DEVICE
WO2008135366A1 (en) * 2007-04-20 2008-11-13 Airbus France Aircraft engine mounting device and aircraft including at least one such device
US8146856B2 (en) 2007-04-20 2012-04-03 Airbus Operations Sas Device for attaching an aircraft engine and aircraft comprising at least one such device
US9010085B2 (en) 2007-08-01 2015-04-21 United Technologies Corporation Turbine section of high bypass turbofan
US8844265B2 (en) 2007-08-01 2014-09-30 United Technologies Corporation Turbine section of high bypass turbofan
US11614036B2 (en) 2007-08-01 2023-03-28 Raytheon Technologies Corporation Turbine section of gas turbine engine
US11486311B2 (en) 2007-08-01 2022-11-01 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11480108B2 (en) 2007-08-01 2022-10-25 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11346289B2 (en) 2007-08-01 2022-05-31 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11242805B2 (en) 2007-08-01 2022-02-08 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11215123B2 (en) 2007-08-01 2022-01-04 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11149650B2 (en) 2007-08-01 2021-10-19 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US10794293B2 (en) 2007-08-01 2020-10-06 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US10662880B2 (en) 2007-08-01 2020-05-26 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US8256707B2 (en) * 2007-08-01 2012-09-04 United Technologies Corporation Engine mounting configuration for a turbofan gas turbine engine
US10371061B2 (en) 2007-08-01 2019-08-06 United Technologies Corporation Turbine section of high bypass turbofan
US10060357B2 (en) 2007-08-01 2018-08-28 United Technologies Corporation Turbine section of high bypass turbofan
US20090056343A1 (en) * 2007-08-01 2009-03-05 Suciu Gabriel L Engine mounting configuration for a turbofan gas turbine engine
US8850793B2 (en) 2007-08-01 2014-10-07 United Technologies Corporation Turbine section of high bypass turbofan
CN101469647B (en) * 2007-11-23 2012-11-28 斯奈克玛 Turbojet engine suspended from a support strut of an aircraft
EP2062819A1 (en) * 2007-11-23 2009-05-27 Snecma Jet engine hanging from an aircraft pylon
JP2009127629A (en) * 2007-11-23 2009-06-11 Snecma Turbojet suspended from aircraft mast
US8141817B2 (en) 2007-11-23 2012-03-27 Snecma Turbojet suspended from an aircraft mast
RU2487056C2 (en) * 2007-11-23 2013-07-10 Снекма Turbojet hinged to aircraft pylon
FR2924094A1 (en) * 2007-11-23 2009-05-29 Snecma Sa TURBOREACTOR SUSPENDED ON AN AIRCRAFT PYLON
FR2925016A1 (en) * 2007-12-12 2009-06-19 Snecma Sa Isostatic jet engine pylon suspension for aircraft, has front attachment with beam transversal with respect to axis, where plane formed by rods of front attachment and transmission rod are convergent in point on axis of motor or near axis
FR2926536A1 (en) * 2008-01-23 2009-07-24 Snecma Sa ATTACHING A PROPULSIVE SYSTEM TO A STRUCTURE ELEMENT OF AN AIRCRAFT
EP2082960A1 (en) * 2008-01-23 2009-07-29 Snecma Attachment of a propulsion system to an aircraft structural element
US8827203B2 (en) 2008-01-23 2014-09-09 Snecma Connecting a propulsion system to a structural element of an aircraft
EP2103516B1 (en) * 2008-03-21 2016-05-04 United Technologies Corporation Mounting system for a gas turbine engine
EP2103516A2 (en) * 2008-03-21 2009-09-23 United Technologies Corporation Mounting system for a gas turbine engine
US8342473B2 (en) 2008-06-13 2013-01-01 Rolls-Royce Plc Thrust mounting arrangement
US8561940B2 (en) 2009-12-11 2013-10-22 Rolls-Royce Deutschland Ltd & Co Kg Arrangement for the suspension of a jet engine to a supporting structure
DE102009054568A1 (en) * 2009-12-11 2011-06-16 Rolls-Royce Deutschland Ltd & Co Kg Device for suspending a jet engine on a support structure
US20120012694A1 (en) * 2010-07-14 2012-01-19 Spirit Aerosystems, Inc. Fail-safe aircraft engine mounting apparatus
US8348191B2 (en) * 2010-07-14 2013-01-08 Spirit Aerosystems, Inc. Fail-safe aircraft engine mounting apparatus
EP2639159A3 (en) * 2012-03-16 2017-04-12 The Boeing Company Engine mounting system for an aircraft
US9027902B2 (en) 2012-07-17 2015-05-12 Rolls-Royce Deutschland Ltd & Co Kg Transport securing device of an aircraft gas turbine
DE102012014108B4 (en) * 2012-07-17 2015-11-05 Rolls-Royce Deutschland Ltd & Co Kg Transport safety device of an aircraft gas turbine
DE102012014108A1 (en) * 2012-07-17 2014-01-23 Rolls-Royce Deutschland Ltd & Co Kg Transport safety device of an aircraft gas turbine
US10436063B2 (en) * 2012-08-17 2019-10-08 United Technologies Corporation Assembly for mounting a turbine engine to an airframe
US20140047850A1 (en) * 2012-08-17 2014-02-20 United Technologies Corporation Assembly for mounting a turbine engine to an airframe
EP3587749A1 (en) * 2018-06-28 2020-01-01 Rolls-Royce plc Gas turbine engine
US11273923B2 (en) 2019-07-12 2022-03-15 Spirit Aerosystems, Inc. Fail-safe engine support system
US20230113400A1 (en) * 2021-09-20 2023-04-13 Airbus Operations (S.A.S.) Aircraft propulsion assembly comprising a thrust force uptake device
US11807374B2 (en) * 2021-09-20 2023-11-07 Airbus Operations (S.A.S.) Aircraft propulsion assembly comprising a thrust force uptake device
FR3133375A1 (en) * 2022-03-11 2023-09-15 Airbus Operations (S.A.S.) Compact electric propulsion assembly comprising an isostatic motor attachment, aircraft comprising at least one such electric propulsion assembly
EP4253247A1 (en) * 2022-03-11 2023-10-04 Airbus Operations (S.A.S.) Compact electric propulsion assembly comprising an isostatic motor attachment, aircraft comprising at least one such electric propulsion assembly

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Legal Events

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