FR3128972B1 - CONNECTION BETWEEN A BLADE FOOT AND A TIMMING DEVICE - Google Patents
CONNECTION BETWEEN A BLADE FOOT AND A TIMMING DEVICE Download PDFInfo
- Publication number
- FR3128972B1 FR3128972B1 FR2111873A FR2111873A FR3128972B1 FR 3128972 B1 FR3128972 B1 FR 3128972B1 FR 2111873 A FR2111873 A FR 2111873A FR 2111873 A FR2111873 A FR 2111873A FR 3128972 B1 FR3128972 B1 FR 3128972B1
- Authority
- FR
- France
- Prior art keywords
- connection
- foot
- timming
- bearing surface
- blade
- 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.)
- Active
Links
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/02—Hub construction
- B64C11/04—Blade mountings
- B64C11/06—Blade mountings for variable-pitch blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Surgical Instruments (AREA)
- Wind Motors (AREA)
- Pivots And Pivotal Connections (AREA)
- Connection Of Plates (AREA)
Abstract
LIAISON ENTRE UN PIED D’AUBE ET UN DISPOSITIF DE CALAGE Un aspect de l’invention concerne un ensemble (200) comportant : une aube (30) comportant un pied (31),un support d’aube statique (40),un dispositif de calage (210) lié au support d’aube (40) caractérisée en ce qu’elle comprend :une platine (13),un mors fixe (11) comportant une première portée (12), le mors fixe (11) est solidaire de la platine (13),un mors mobile (21) comportant une deuxième portée (22), le mors fixe (11) est lié au mors mobile (21) par un moyen de fixation, le pied (31) est en contact surfacique avec : la première portée (12), la deuxième portée (22) et une surface de contact (14) de la platine (13). Figure à publier avec l’abrégé : Figure 6CONNECTION BETWEEN A BLADE FOOT AND A WEDGING DEVICE One aspect of the invention relates to an assembly (200) comprising: a blade (30) comprising a foot (31), a static blade support (40), a wedging device (210) linked to the blade support (40) characterized in that it comprises: a plate (13), a fixed jaw (11) comprising a first bearing surface (12), the fixed jaw (11) is integral with the plate (13), a movable jaw (21) comprising a second bearing surface (22), the fixed jaw (11) is linked to the movable jaw (21) by a fixing means, the foot (31) is in surface contact with: the first bearing surface (12), the second bearing surface (22) and a contact surface (14) of the plate (13). Figure to be published with the abstract: Figure 6
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR2111873A FR3128972B1 (en) | 2021-11-09 | 2021-11-09 | CONNECTION BETWEEN A BLADE FOOT AND A TIMMING DEVICE |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR2111873A FR3128972B1 (en) | 2021-11-09 | 2021-11-09 | CONNECTION BETWEEN A BLADE FOOT AND A TIMMING DEVICE |
| FR2111873 | 2021-11-09 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR3128972A1 FR3128972A1 (en) | 2023-05-12 |
| FR3128972B1 true FR3128972B1 (en) | 2025-03-14 |
Family
ID=80446617
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR2111873A Active FR3128972B1 (en) | 2021-11-09 | 2021-11-09 | CONNECTION BETWEEN A BLADE FOOT AND A TIMMING DEVICE |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR3128972B1 (en) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3151883A1 (en) * | 2023-07-31 | 2025-02-07 | Safran Aircraft Engines | Fixed turbomachine vane comprising variable pitch blades |
| FR3151882A1 (en) * | 2023-07-31 | 2025-02-07 | Safran Aircraft Engines | Fixed turbomachine vane comprising variable pitch blades |
| FR3153374A1 (en) * | 2023-09-22 | 2025-03-28 | Safran Aircraft Engines | ASSEMBLY COMPRISING A BLADE AND A BLADE HOLDING SYSTEM |
| FR3153372A1 (en) * | 2023-09-22 | 2025-03-28 | Safran Aircraft Engines | ASSEMBLY COMPRISING A BLADE AND A BLADE HOLDING SYSTEM |
| FR3153373A1 (en) | 2023-09-22 | 2025-03-28 | Safran Aircraft Engines | ASSEMBLY COMPRISING A BLADE AND A BLADE HOLDING SYSTEM |
| FR3155862B1 (en) * | 2023-11-24 | 2025-11-28 | Safran Aircraft Engines | Blade of a static turbomachine blade with improved attachment |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2996584A1 (en) | 2012-10-10 | 2014-04-11 | Snecma | FOOTBED FOR LEVELED BLADE FOOT |
| FR3021030B1 (en) * | 2014-05-14 | 2018-01-05 | Ratier Figeac | SECURED ANCHOR BLADE IN RADIAL TRANSLATION, PROPELLER, TURBOMACHINE AND AIRCRAFT |
| FR3050719B1 (en) * | 2016-04-28 | 2018-04-13 | Airbus Operations | AIRCRAFT TURBOMACHINE PROPELLER COMPRISING MEANS OF FLAME-RELIEVING BACK-UP MEANS |
| US10934862B2 (en) * | 2018-08-22 | 2021-03-02 | Rolls-Royce Plc | Turbine wheel assembly |
| FR3087830B1 (en) | 2018-10-30 | 2020-10-16 | Safran Aircraft Engines | DAWN INCLUDING A STRUCTURE IN COMPOSITE MATERIAL AND A METAL STRENGTHENING PART |
| FR3097835A1 (en) * | 2019-06-27 | 2021-01-01 | Airbus Helicopters | Advance propeller with interchangeable blades and method of mounting interchangeable blades on a propeller |
| FR3107724B1 (en) * | 2020-02-27 | 2022-06-24 | Safran Aircraft Engines | Fan rotor with variable pitch blades and turbomachine equipped with such a rotor |
-
2021
- 2021-11-09 FR FR2111873A patent/FR3128972B1/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| FR3128972A1 (en) | 2023-05-12 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PLFP | Fee payment |
Year of fee payment: 2 |
|
| PLSC | Publication of the preliminary search report |
Effective date: 20230512 |
|
| PLFP | Fee payment |
Year of fee payment: 3 |
|
| PLFP | Fee payment |
Year of fee payment: 4 |
|
| PLFP | Fee payment |
Year of fee payment: 5 |