GB888943A - Improvements in or relating to fan units - Google Patents

Improvements in or relating to fan units

Info

Publication number
GB888943A
GB888943A GB2809759A GB2809759A GB888943A GB 888943 A GB888943 A GB 888943A GB 2809759 A GB2809759 A GB 2809759A GB 2809759 A GB2809759 A GB 2809759A GB 888943 A GB888943 A GB 888943A
Authority
GB
United Kingdom
Prior art keywords
fan
relating
aug
casing
movable
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.)
Expired
Application number
GB2809759A
Inventor
Samuel David Thomas
Maurice Ian Taylor
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 GB2809759A priority Critical patent/GB888943A/en
Priority to DE19601403584 priority patent/DE1403584C3/en
Publication of GB888943A publication Critical patent/GB888943A/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
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/006—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector within one plane only
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/005—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors the motors being fixed relative to the fuselage
    • 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
    • F02K3/062—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 aft fan

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)
  • Optical Radar Systems And Details Thereof (AREA)

Abstract

888,943. Jet propelled vertical lift aircraft. ROLLS-ROYCE Ltd. Aug. 9, 1960 [Aug. 17, 1959], No. 28097/59. Class 4. A fan unit 12, driven by a gas turbine engine 10, comprises a casing 22, through which flows the fan output, and a discharge outlet 24 which is substantially sealed to but movable with respect to casing 22 so that the fan output may be directed at an angle to the longitudinal axis of the fan unit. The discharge outlet 24 is movable about pivots 27, on which it is mounted by operation of rams 31.
GB2809759A 1959-08-17 1959-08-17 Improvements in or relating to fan units Expired GB888943A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB2809759A GB888943A (en) 1959-08-17 1959-08-17 Improvements in or relating to fan units
DE19601403584 DE1403584C3 (en) 1959-08-17 1960-08-16 Twin stream fogging

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2809759A GB888943A (en) 1959-08-17 1959-08-17 Improvements in or relating to fan units

Publications (1)

Publication Number Publication Date
GB888943A true GB888943A (en) 1962-02-07

Family

ID=10270214

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2809759A Expired GB888943A (en) 1959-08-17 1959-08-17 Improvements in or relating to fan units

Country Status (2)

Country Link
DE (1) DE1403584C3 (en)
GB (1) GB888943A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4809932A (en) * 1986-12-20 1989-03-07 Messerschmitt-Bokow-Blohm GmbH Thrust vector control for aircraft
US20190170087A1 (en) * 2017-12-06 2019-06-06 Yao-Chang Lin Thrust vector controller
CN109878702A (en) * 2017-12-06 2019-06-14 林瑤章 Thrust vector control device

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2753917A1 (en) * 1977-12-03 1979-06-07 Beck & Co Ag Dr USE OF THERMOPLASTICS FOR THE MANUFACTURE OF INSULATED WINDING WIRES IN THE EXTRUSION PROCESS

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4809932A (en) * 1986-12-20 1989-03-07 Messerschmitt-Bokow-Blohm GmbH Thrust vector control for aircraft
US20190170087A1 (en) * 2017-12-06 2019-06-06 Yao-Chang Lin Thrust vector controller
CN109878702A (en) * 2017-12-06 2019-06-14 林瑤章 Thrust vector control device

Also Published As

Publication number Publication date
DE1403584A1 (en) 1968-11-14
DE1403584C3 (en) 1973-11-15

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