FR2127472A6 - - Google Patents

Info

Publication number
FR2127472A6
FR2127472A6 FR7116844A FR7116844A FR2127472A6 FR 2127472 A6 FR2127472 A6 FR 2127472A6 FR 7116844 A FR7116844 A FR 7116844A FR 7116844 A FR7116844 A FR 7116844A FR 2127472 A6 FR2127472 A6 FR 2127472A6
Authority
FR
France
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
FR7116844A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Application granted granted Critical
Publication of FR2127472A6 publication Critical patent/FR2127472A6/fr
Expired legal-status Critical Current

Links

Classifications

    • A—HUMAN NECESSITIES
    • A62—LIFE-SAVING; FIRE-FIGHTING
    • A62C—FIRE-FIGHTING
    • A62C3/00—Fire prevention, containment or extinguishing specially adapted for particular objects or places
    • A62C3/06—Fire prevention, containment or extinguishing specially adapted for particular objects or places of highly inflammable material, e.g. light metals, petroleum products
    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • 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
    • F02C7/24—Heat or noise insulation
    • F02C7/25—Fire protection or prevention
    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D2045/009—Fire detection or protection; Erosion protection, e.g. from airborne particles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Mechanical Engineering (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Health & Medical Sciences (AREA)
  • Public Health (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Measuring Fluid Pressure (AREA)
  • Laminated Bodies (AREA)
FR7116844A 1971-02-25 1971-05-10 Expired FR2127472A6 (cg-RX-API-DMAC10.html)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11889271A 1971-02-25 1971-02-25

Publications (1)

Publication Number Publication Date
FR2127472A6 true FR2127472A6 (cg-RX-API-DMAC10.html) 1972-10-13

Family

ID=22381379

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7116844A Expired FR2127472A6 (cg-RX-API-DMAC10.html) 1971-02-25 1971-05-10

Country Status (4)

Country Link
CA (1) CA950991A (cg-RX-API-DMAC10.html)
DE (2) DE2122116A1 (cg-RX-API-DMAC10.html)
FR (1) FR2127472A6 (cg-RX-API-DMAC10.html)
GB (1) GB1358300A (cg-RX-API-DMAC10.html)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3015431A1 (fr) * 2013-12-19 2015-06-26 Airbus Operations Sas Structure primaire de mat d'accrochage renforcee.
US9862497B2 (en) 2013-12-17 2018-01-09 Airbus Operations (S.A.S.) Assembly for an aircraft, comprising an engine attachment body partially produced in one piece with an internal stiffening rib of an attachment pylon box section
US9889943B2 (en) 2013-12-17 2018-02-13 Airbus Operations (S.A.S.) Assembly for an aircraft, comprising an engine attachment body equipped with at least one shackle support fitting that passes into the box section of the attachment pylon
US10336458B2 (en) 2013-12-23 2019-07-02 Airbus Operations (S.A.S.) Aircraft assembly comprising a mounting strut built into the nacelle and arranged at the rear section of the fuselage

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BR112015016935B1 (pt) * 2013-01-15 2022-01-11 United Technologies Corporation Motor de turbina a gás, e, método para fornecer proteção contra fogo para uma unidade de potência auxiliar
US12071858B2 (en) * 2021-10-13 2024-08-27 General Electric Company Fire retardant engine casing apparatus

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9862497B2 (en) 2013-12-17 2018-01-09 Airbus Operations (S.A.S.) Assembly for an aircraft, comprising an engine attachment body partially produced in one piece with an internal stiffening rib of an attachment pylon box section
US9889943B2 (en) 2013-12-17 2018-02-13 Airbus Operations (S.A.S.) Assembly for an aircraft, comprising an engine attachment body equipped with at least one shackle support fitting that passes into the box section of the attachment pylon
FR3015431A1 (fr) * 2013-12-19 2015-06-26 Airbus Operations Sas Structure primaire de mat d'accrochage renforcee.
US9868545B2 (en) 2013-12-19 2018-01-16 Airbus Operations (S.A.S.) Primary structure for an attachment pylon with firewall and thermal layers
US10336458B2 (en) 2013-12-23 2019-07-02 Airbus Operations (S.A.S.) Aircraft assembly comprising a mounting strut built into the nacelle and arranged at the rear section of the fuselage

Also Published As

Publication number Publication date
CA950991A (en) 1974-07-09
DE2122116A1 (de) 1972-09-07
DE2166833B2 (de) 1979-12-20
GB1358300A (en) 1974-07-03
DE2166833A1 (de) 1976-01-22
DE2166833C3 (de) 1980-08-21

Similar Documents

Publication Publication Date Title
ATA136472A (cg-RX-API-DMAC10.html)
AR196074A1 (cg-RX-API-DMAC10.html)
AU2658571A (cg-RX-API-DMAC10.html)
AU2691671A (cg-RX-API-DMAC10.html)
AU2742671A (cg-RX-API-DMAC10.html)
AU2941471A (cg-RX-API-DMAC10.html)
AU2485671A (cg-RX-API-DMAC10.html)
AU2726271A (cg-RX-API-DMAC10.html)
AU2952271A (cg-RX-API-DMAC10.html)
AU2684071A (cg-RX-API-DMAC10.html)
AU3005371A (cg-RX-API-DMAC10.html)
AU2894671A (cg-RX-API-DMAC10.html)
AU2564071A (cg-RX-API-DMAC10.html)
AU2473671A (cg-RX-API-DMAC10.html)
AU2836771A (cg-RX-API-DMAC10.html)
AU3038671A (cg-RX-API-DMAC10.html)
AU2503871A (cg-RX-API-DMAC10.html)
AU2880771A (cg-RX-API-DMAC10.html)
AU2577671A (cg-RX-API-DMAC10.html)
AU2588771A (cg-RX-API-DMAC10.html)
AU2654071A (cg-RX-API-DMAC10.html)
AU2456871A (cg-RX-API-DMAC10.html)
AU2669471A (cg-RX-API-DMAC10.html)
AU2455871A (cg-RX-API-DMAC10.html)
AU2684171A (cg-RX-API-DMAC10.html)