FR3121477B1 - AIRCRAFT TURBOMACHINE WITH VARIABLE-PITCHED PROPELLER BLADE - Google Patents
AIRCRAFT TURBOMACHINE WITH VARIABLE-PITCHED PROPELLER BLADE Download PDFInfo
- Publication number
- FR3121477B1 FR3121477B1 FR2103263A FR2103263A FR3121477B1 FR 3121477 B1 FR3121477 B1 FR 3121477B1 FR 2103263 A FR2103263 A FR 2103263A FR 2103263 A FR2103263 A FR 2103263A FR 3121477 B1 FR3121477 B1 FR 3121477B1
- Authority
- FR
- France
- Prior art keywords
- blade
- bowl
- variable
- foot
- propeller 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
- 230000000295 complement effect Effects 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/322—Blade mountings
- F04D29/323—Blade mountings adjustable
-
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/60—Mounting; Assembling; Disassembling
- F04D29/64—Mounting; Assembling; Disassembling of axial pumps
- F04D29/644—Mounting; Assembling; Disassembling of axial pumps especially adapted for elastic fluid pumps
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
L'invention concerne un ensemble comportant une aube (10) d'hélice et son système (34) de calage angulaire de l'aube (10) comportant un bol (42) qui est délimité radialement par une paroi (44) annulaire s'étendant autour d'un axe (A) de calage de l'aube (10), le bol (42) comportant une paroi (46) de fond, une extrémité (28) inférieure libre du pied (14) étant emboîtée axialement dans un logement (56) complémentaire de la paroi (46) de fond pour lier en rotation autour de l'axe (A) de calage le bol (42) et l'aube (10), caractérisé en ce que le pied (14) de l'aube (10) comporte une première face (70A) de limitation qui coopère avec une première face (72A) de butée du bol (42) pour limiter la rotation de l'aube (10) en cas de rupture de l'extrémité (28) inférieure du pied. Figure pour l'abrégé : Figure 9The invention relates to an assembly comprising a propeller blade (10) and its system (34) for angular setting of the blade (10) comprising a bowl (42) which is delimited radially by an annular wall (44) extending around an axis (A) for wedging the blade (10), the bowl (42) comprising a bottom wall (46), a free lower end (28) of the foot (14) being fitted axially in a housing (56) complementary to the bottom wall (46) to connect in rotation around the wedging axis (A) the bowl (42) and the blade (10), characterized in that the foot (14) of the blade (10) has a first limiting face (70A) which cooperates with a first abutment face (72A) of the bowl (42) to limit the rotation of the blade (10) in the event of the tip breaking (28) lower foot. Figure for abstract: Figure 9
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2103263A FR3121477B1 (en) | 2021-03-30 | 2021-03-30 | AIRCRAFT TURBOMACHINE WITH VARIABLE-PITCHED PROPELLER BLADE |
EP21755007.8A EP4185522A1 (en) | 2020-07-24 | 2021-07-15 | Aircraft turbine engine comprising variable-pitch propeller blades |
US18/006,344 US11993365B2 (en) | 2020-07-24 | 2021-07-15 | Aircraft turbine engine comprising variable-pitch propeller blades |
CN202180051861.0A CN116097005A (en) | 2020-07-24 | 2021-07-15 | Aircraft turbine engine including variable pitch propeller blades |
PCT/FR2021/051316 WO2022018359A1 (en) | 2020-07-24 | 2021-07-15 | Aircraft turbine engine comprising variable-pitch propeller blades |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2103263A FR3121477B1 (en) | 2021-03-30 | 2021-03-30 | AIRCRAFT TURBOMACHINE WITH VARIABLE-PITCHED PROPELLER BLADE |
FR2103263 | 2021-03-30 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3121477A1 FR3121477A1 (en) | 2022-10-07 |
FR3121477B1 true FR3121477B1 (en) | 2023-02-24 |
Family
ID=75746914
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2103263A Active FR3121477B1 (en) | 2020-07-24 | 2021-03-30 | AIRCRAFT TURBOMACHINE WITH VARIABLE-PITCHED PROPELLER BLADE |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3121477B1 (en) |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB718127A (en) * | 1951-02-01 | 1954-11-10 | Paolo Terzi | Improvements in or relating to variable pitch propellers |
DE4203205C2 (en) * | 1992-02-05 | 1995-12-07 | Muehlbauer Luftfahrttechn Gmbh | Propeller blade storage |
FR3017163B1 (en) * | 2014-02-04 | 2016-02-12 | Snecma | DEVICE FOR A NON-CAREED PROPELLER HAVING A VARIABLE SHIFT OF A TURBOMACHINE |
-
2021
- 2021-03-30 FR FR2103263A patent/FR3121477B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3121477A1 (en) | 2022-10-07 |
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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: 20221007 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
|
PLFP | Fee payment |
Year of fee payment: 4 |