FR1289887A - Improvements to engine mounts - Google Patents

Improvements to engine mounts

Info

Publication number
FR1289887A
FR1289887A FR862142A FR862142A FR1289887A FR 1289887 A FR1289887 A FR 1289887A FR 862142 A FR862142 A FR 862142A FR 862142 A FR862142 A FR 862142A FR 1289887 A FR1289887 A FR 1289887A
Authority
FR
France
Prior art keywords
engine mounts
mounts
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
FR862142A
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
Priority to FR862142A priority Critical patent/FR1289887A/en
Application granted granted Critical
Publication of FR1289887A publication Critical patent/FR1289887A/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
    • 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
    • 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
    • B64C29/0058—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 vertical jet

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR862142A 1961-05-17 1961-05-17 Improvements to engine mounts Expired FR1289887A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR862142A FR1289887A (en) 1961-05-17 1961-05-17 Improvements to engine mounts

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR862142A FR1289887A (en) 1961-05-17 1961-05-17 Improvements to engine mounts

Publications (1)

Publication Number Publication Date
FR1289887A true FR1289887A (en) 1962-04-06

Family

ID=8755402

Family Applications (1)

Application Number Title Priority Date Filing Date
FR862142A Expired FR1289887A (en) 1961-05-17 1961-05-17 Improvements to engine mounts

Country Status (1)

Country Link
FR (1) FR1289887A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1222320B (en) * 1962-06-28 1966-08-04 Rolls Royce Closure device for the inlet of a gas turbine jet engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1222320B (en) * 1962-06-28 1966-08-04 Rolls Royce Closure device for the inlet of a gas turbine jet engine

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