FR88324E - Laminated connecting device working with traction and torsion, its assembly and method of manufacture, used in particular for fixing the blades to the rotating hub of a helicopter - Google Patents
Laminated connecting device working with traction and torsion, its assembly and method of manufacture, used in particular for fixing the blades to the rotating hub of a helicopterInfo
- Publication number
- FR88324E FR88324E FR12827A FR12827A FR88324E FR 88324 E FR88324 E FR 88324E FR 12827 A FR12827 A FR 12827A FR 12827 A FR12827 A FR 12827A FR 88324 E FR88324 E FR 88324E
- Authority
- FR
- France
- Prior art keywords
- helicopter
- traction
- torsion
- blades
- manufacture
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C7/00—Connecting-rods or like links pivoted at both ends; Construction of connecting-rod heads
- F16C7/02—Constructions of connecting-rods with constant length
- F16C7/026—Constructions of connecting-rods with constant length made of fibre reinforced resin
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR12827A FR88324E (en) | 1965-04-12 | 1965-04-12 | Laminated connecting device working with traction and torsion, its assembly and method of manufacture, used in particular for fixing the blades to the rotating hub of a helicopter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR12827A FR88324E (en) | 1965-04-12 | 1965-04-12 | Laminated connecting device working with traction and torsion, its assembly and method of manufacture, used in particular for fixing the blades to the rotating hub of a helicopter |
Publications (1)
Publication Number | Publication Date |
---|---|
FR88324E true FR88324E (en) | 1967-01-20 |
Family
ID=8576179
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR12827A Expired FR88324E (en) | 1965-04-12 | 1965-04-12 | Laminated connecting device working with traction and torsion, its assembly and method of manufacture, used in particular for fixing the blades to the rotating hub of a helicopter |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR88324E (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2604768A1 (en) * | 1986-10-07 | 1988-04-08 | Inst Francais Du Petrole | FITTING AND METHOD OF MANUFACTURING THE FITTING FOR A SHAFT COMPRISING A REINFORCEMENT FRAME |
-
1965
- 1965-04-12 FR FR12827A patent/FR88324E/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2604768A1 (en) * | 1986-10-07 | 1988-04-08 | Inst Francais Du Petrole | FITTING AND METHOD OF MANUFACTURING THE FITTING FOR A SHAFT COMPRISING A REINFORCEMENT FRAME |
EP0267063A1 (en) * | 1986-10-07 | 1988-05-11 | Institut Français du Pétrole | Connection element for a shaft with embedded reinforcements and manufacturing process therefor |
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