GB888073A - Jet propulsion engines - Google Patents

Jet propulsion engines

Info

Publication number
GB888073A
GB888073A GB1908659A GB1908659A GB888073A GB 888073 A GB888073 A GB 888073A GB 1908659 A GB1908659 A GB 1908659A GB 1908659 A GB1908659 A GB 1908659A GB 888073 A GB888073 A GB 888073A
Authority
GB
United Kingdom
Prior art keywords
air compressor
jet propulsion
nozzle
flaps
compressed
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
GB1908659A
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.)
PETER MALCOLM HUGHES
Original Assignee
PETER MALCOLM HUGHES
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 PETER MALCOLM HUGHES filed Critical PETER MALCOLM HUGHES
Priority to GB1908659A priority Critical patent/GB888073A/en
Publication of GB888073A publication Critical patent/GB888073A/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
    • 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
    • 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
    • B64C29/0066—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 with horizontal jet and jet deflector
    • 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
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/105—Heating the by-pass flow
    • F02K3/11—Heating the by-pass flow by means of burners or combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

888,073. Deflecting propulsive jets. HUGHES. P. M. Aug. 23, 1960 [June 4, 1959], No. 19086/59. Class 4. [Also in Group XXVI] A jet propulsion unit comprises a duct within which is disposed a rotary air compressor and means for imparting heat to at least some of the air compressed thereby, the air compressor being driven by an engine, the driving shaft of which is not co-axial with the rotor of the air compressor. The compressed air flows into a combustion section where fuel is injected through the injector and flame-holder device 8 and the combustion gases finally discharge through a propulsion nozzle 36 which is of rectangular form. Pivoted flaps 37, 39 and 40 are associated with the nozzle 36 for causing deflection of the gas stream, the flaps being shown in a deflecting position in Fig. 2.
GB1908659A 1959-06-04 1959-06-04 Jet propulsion engines Expired GB888073A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1908659A GB888073A (en) 1959-06-04 1959-06-04 Jet propulsion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1908659A GB888073A (en) 1959-06-04 1959-06-04 Jet propulsion engines

Publications (1)

Publication Number Publication Date
GB888073A true GB888073A (en) 1962-01-24

Family

ID=10123543

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1908659A Expired GB888073A (en) 1959-06-04 1959-06-04 Jet propulsion engines

Country Status (1)

Country Link
GB (1) GB888073A (en)

Similar Documents

Publication Publication Date Title
GB973319A (en) Improvements in supersonic fuel injector
GB1069033A (en) Improvements in or relating to gas turbine jet propulsion engines
GB757496A (en) Improvements in arrangement for controlling the air-intake orifices of jet propulsion units
GB852829A (en) Improvements in or relating to gas-turbine jet propulsion engines
GB1055625A (en) Improved vehicle for launching rocket propelled vehicles
GB891064A (en) New or improved aircraft propulsion installation
US2689454A (en) Rocket engine
GB713783A (en) Gas turbine propulsion units
GB1045295A (en) Improvements in or relating to a jet noise suppression device
GB900040A (en) Exhaust nozzle with thrust deflector
GB1027415A (en) Jet propulsion engine
GB888073A (en) Jet propulsion engines
GB1073458A (en) Improvements relating to by-pass ducted for gas-turbine aircraft engines
GB905534A (en) Improvements in or relating to gas turbine engines
GB955014A (en) Turbine jet propulsion engine
GB875496A (en) Improvements in or relating to ducted-fan gas turbine jet propulsion engines
GB1003584A (en) Improvements in or relating to jet propulsion engines
GB955013A (en) Improvements in and relating to Composite Jet Engines
GB881967A (en) Improved propulsion unit for use in vertical take-off aircraft
GB705611A (en) Improved gas turbine power plant
GB743492A (en) Improvements in jet propulsion engines including a plurality of intermittently operating combustion chambers
GB1010100A (en) Improvements in or relating to vtol or stol aircraft
GB1093793A (en) Improvements in and relating to gas turbine engines
GB704606A (en) Improvements in fuel economisers using electric sparks for petrol engines and the like
GB847868A (en) Improvements relating to vertical take-off aircraft