FR2984848B1 - Pale d'helice avec caissons et longerons de renfort et helice comprenant au moins une telle pale - Google Patents

Pale d'helice avec caissons et longerons de renfort et helice comprenant au moins une telle pale

Info

Publication number
FR2984848B1
FR2984848B1 FR1104086A FR1104086A FR2984848B1 FR 2984848 B1 FR2984848 B1 FR 2984848B1 FR 1104086 A FR1104086 A FR 1104086A FR 1104086 A FR1104086 A FR 1104086A FR 2984848 B1 FR2984848 B1 FR 2984848B1
Authority
FR
France
Prior art keywords
propeller
blade
housings
lengths
reinforcing
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
Application number
FR1104086A
Other languages
English (en)
Other versions
FR2984848A1 (fr
Inventor
Stanislas Tutaj
Bruno Petellaz
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.)
Ratier Figeac SAS
Original Assignee
Ratier Figeac SAS
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 Ratier Figeac SAS filed Critical Ratier Figeac SAS
Priority to FR1104086A priority Critical patent/FR2984848B1/fr
Priority to GB1222809.4A priority patent/GB2498076B/en
Priority to US13/721,727 priority patent/US9365285B2/en
Publication of FR2984848A1 publication Critical patent/FR2984848A1/fr
Application granted granted Critical
Publication of FR2984848B1 publication Critical patent/FR2984848B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B64C11/16—Blades
    • B64C11/20—Constructional features
    • B64C11/26—Fabricated blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • 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
    • 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
    • B64C11/16—Blades
    • B64C11/20—Constructional features
    • 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
    • B64C11/16—Blades
    • B64C11/20—Constructional features
    • B64C11/24—Hollow 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
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Architecture (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Toys (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Confectionery (AREA)
  • Catching Or Destruction (AREA)
  • Wind Motors (AREA)
FR1104086A 2011-12-23 2011-12-23 Pale d'helice avec caissons et longerons de renfort et helice comprenant au moins une telle pale Active FR2984848B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1104086A FR2984848B1 (fr) 2011-12-23 2011-12-23 Pale d'helice avec caissons et longerons de renfort et helice comprenant au moins une telle pale
GB1222809.4A GB2498076B (en) 2011-12-23 2012-12-18 Propeller blade with reinforcing spars and boxes, and propeller comprising at least one such blade
US13/721,727 US9365285B2 (en) 2011-12-23 2012-12-20 Propeller blade with reinforcing spars and boxes, and propeller comprising at least one such blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1104086A FR2984848B1 (fr) 2011-12-23 2011-12-23 Pale d'helice avec caissons et longerons de renfort et helice comprenant au moins une telle pale

Publications (2)

Publication Number Publication Date
FR2984848A1 FR2984848A1 (fr) 2013-06-28
FR2984848B1 true FR2984848B1 (fr) 2016-01-15

Family

ID=47630933

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1104086A Active FR2984848B1 (fr) 2011-12-23 2011-12-23 Pale d'helice avec caissons et longerons de renfort et helice comprenant au moins une telle pale

Country Status (3)

Country Link
US (1) US9365285B2 (fr)
FR (1) FR2984848B1 (fr)
GB (1) GB2498076B (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3021030B1 (fr) * 2014-05-14 2018-01-05 Ratier Figeac Pale a ancrage securise en translation radiale, helice, turbomachine et aeronef
EP3148876B1 (fr) * 2014-05-30 2019-11-06 Sikorsky Aircraft Corporation Enveloppe de tige structurellement efficace
GB201414495D0 (en) * 2014-08-15 2014-10-01 Rolls Royce Plc Blade
EP3034783B1 (fr) 2014-12-17 2019-11-20 Rolls-Royce Deutschland Ltd & Co KG Agencement d'aubes d'un turboréacteur ou d'une hélice d'avion et propulseur associé
GB2535231A (en) * 2015-02-13 2016-08-17 Reiter Johannes Propeller for an aircraft for vertical take-off and landing
CN107472513A (zh) * 2017-08-21 2017-12-15 滁州万际航空器产业研究院有限公司 一种用于无人直升机的空心桨叶及其制造方法
US11346363B2 (en) * 2018-04-30 2022-05-31 Raytheon Technologies Corporation Composite airfoil for gas turbine

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB871625A (en) * 1956-11-13 1961-06-28 Parsons Corp Rotor blade structure and method of molding same
DE1259560B (de) * 1962-03-15 1968-01-25 Eugen Haenle Verfahren und Vorrichtung zum Herstellen von biege- und drehfesten Schalenbauteilen,die aus einer Schalenaussenwand mit inneren Rippen bzw. Gurten aus glasfaserverstaerktem Kunststoff bestehen
US3586460A (en) * 1969-05-14 1971-06-22 Us Air Force Rotor blade variable modulus trailing edge
US3694104A (en) * 1970-10-07 1972-09-26 Garrett Corp Turbomachinery blade
IT7967327A0 (it) * 1979-02-15 1979-02-15 Fiat Ricerche Pala per motori eolici
FR2542695B1 (fr) * 1983-03-18 1985-07-26 Aerospatiale Helice multipale a pas variable a pale s en materiaux composites demontables individuellement, procede de fabrication de telles pales et pales ainsi realisees
GB2168111B (en) * 1984-12-08 1988-05-18 Rolls Royce Rotor aerofoil blade containment
US4784575A (en) * 1986-11-19 1988-11-15 General Electric Company Counterrotating aircraft propulsor blades
US4833911A (en) * 1988-07-01 1989-05-30 The Boeing Company System for measuring aircraft engine thrust
DE3826378A1 (de) * 1988-08-03 1990-02-08 Mtu Muenchen Gmbh Fasertechnische propellerschaufeln
US5129787A (en) * 1991-02-13 1992-07-14 United Technologies Corporation Lightweight propulsor blade with internal spars and rigid base members
US5330092A (en) * 1991-12-17 1994-07-19 The Boeing Company Multiple density sandwich structures and method of fabrication
US6431837B1 (en) * 1999-06-01 2002-08-13 Alexander Velicki Stitched composite fan blade
US7600978B2 (en) * 2006-07-27 2009-10-13 Siemens Energy, Inc. Hollow CMC airfoil with internal stitch
FR2942277B1 (fr) * 2009-02-17 2015-06-19 Airbus France Aube pour recepteur de turbomachine d'aeronef, pourvue de deux ames creuses se succedant selon le squelette

Also Published As

Publication number Publication date
FR2984848A1 (fr) 2013-06-28
GB201222809D0 (fr) 2013-01-30
GB2498076B (en) 2018-02-14
US20130164142A1 (en) 2013-06-27
GB2498076A (en) 2013-07-03
US9365285B2 (en) 2016-06-14

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