FR1065631A - Improvements in aerodyne and aerodyne engine installations - Google Patents

Improvements in aerodyne and aerodyne engine installations

Info

Publication number
FR1065631A
FR1065631A FR1065631DA FR1065631A FR 1065631 A FR1065631 A FR 1065631A FR 1065631D A FR1065631D A FR 1065631DA FR 1065631 A FR1065631 A FR 1065631A
Authority
FR
France
Prior art keywords
aerodyne
engine installations
installations
engine
aerodyne engine
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
Other languages
French (fr)
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
Application granted granted Critical
Publication of FR1065631A publication Critical patent/FR1065631A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • B64C29/0091—Accessories not provided for elsewhere
    • 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
    • B64C29/0075—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 tiltable relative to the fuselage
    • 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
    • F02C7/22—Fuel supply systems
    • F02C7/228—Dividing fuel between various burners
    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • F02K1/008—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 in any rearward direction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • F23R3/48—Flame tube interconnectors, e.g. cross-over tubes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Supercharger (AREA)
FR1065631D 1951-08-16 1952-08-11 Improvements in aerodyne and aerodyne engine installations Expired FR1065631A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1939651A GB720394A (en) 1951-08-16 1951-08-16 Improvements relating to aircraft and aircraft engine installations

Publications (1)

Publication Number Publication Date
FR1065631A true FR1065631A (en) 1954-05-28

Family

ID=10128653

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1065631D Expired FR1065631A (en) 1951-08-16 1952-08-11 Improvements in aerodyne and aerodyne engine installations

Country Status (3)

Country Link
CH (1) CH308179A (en)
FR (1) FR1065631A (en)
GB (1) GB720394A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3026065A (en) * 1956-07-10 1962-03-20 Jr Raymond Prunty Holland Supersonic vertical-rising aircraft
FR2883840A1 (en) * 2005-03-31 2006-10-06 Noel Gil Propulsive unit for aircraft, has muffler, and compressed air reservoir that allows input of compressed air on impact surface via small holes pierced on cylinder and that produces one strike of compressed air per second from water hammers

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2843340A (en) * 1955-01-12 1958-07-15 Wibault Michel Henri Ma Joseph Jet aircraft
GB805128A (en) * 1955-09-28 1958-12-03 Power Jets Res & Dev Ltd Aircraft engine fuel systems
US2964264A (en) * 1956-01-27 1960-12-13 Martin Co Power flap for aircraft
US2986877A (en) * 1957-03-07 1961-06-06 Paul C Emmons Rotatable afterburners for jet aircraft
US3064923A (en) * 1958-05-02 1962-11-20 Daimler Benz Ag Gas turbine propulsion plant and an airplane equipped therewith
FR2690712B1 (en) * 1992-04-30 1994-06-17 Snecma PROPULSIVE ASSEMBLY WITH VARIABLE CYCLE ENGINES AND METHOD OF USE THEREOF.
GB0313456D0 (en) * 2003-06-11 2003-07-16 Rolls Royce Plc Propulsion arrangement
EP3998194A1 (en) * 2021-02-19 2022-05-18 Lilium eAircraft GmbH Wing assembly for an aircraft
EP4294719A1 (en) * 2021-02-19 2023-12-27 Lilium GmbH Wing assembly for an aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3026065A (en) * 1956-07-10 1962-03-20 Jr Raymond Prunty Holland Supersonic vertical-rising aircraft
FR2883840A1 (en) * 2005-03-31 2006-10-06 Noel Gil Propulsive unit for aircraft, has muffler, and compressed air reservoir that allows input of compressed air on impact surface via small holes pierced on cylinder and that produces one strike of compressed air per second from water hammers

Also Published As

Publication number Publication date
GB720394A (en) 1954-12-22
CH308179A (en) 1955-06-30

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