CH320997A - Einrichtung zum Befestigen eines Triebwerkes aussen an einem Flugzeugteil - Google Patents
Einrichtung zum Befestigen eines Triebwerkes aussen an einem FlugzeugteilInfo
- Publication number
- CH320997A CH320997A CH320997DA CH320997A CH 320997 A CH320997 A CH 320997A CH 320997D A CH320997D A CH 320997DA CH 320997 A CH320997 A CH 320997A
- Authority
- CH
- Switzerland
- Prior art keywords
- attaching
- engine
- outside
- aircraft part
- aircraft
- Prior art date
Links
Classifications
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB320997X | 1953-03-04 | ||
GB319069X | 1953-03-12 | ||
GB130753X | 1953-07-13 | ||
GB260254X | 1954-02-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH320997A true CH320997A (de) | 1957-04-15 |
Family
ID=27448178
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH320997D CH320997A (de) | 1953-03-04 | 1954-03-04 | Einrichtung zum Befestigen eines Triebwerkes aussen an einem Flugzeugteil |
Country Status (2)
Country | Link |
---|---|
CH (1) | CH320997A (de) |
GB (1) | GB743205A (de) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4422288A (en) * | 1981-03-02 | 1983-12-27 | General Electric Company | Aft mounting system for combustion transition duct members |
FR3058127B1 (fr) | 2016-10-28 | 2022-02-25 | Safran Aircraft Engines | Assemblage entre un pylone d'aeronef et une turbomachine |
-
1953
- 1953-03-04 GB GB6077/53A patent/GB743205A/en not_active Expired
-
1954
- 1954-03-04 CH CH320997D patent/CH320997A/de unknown
Also Published As
Publication number | Publication date |
---|---|
GB743205A (en) | 1956-01-11 |
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