Epicyclic speed reducer designed for fitment to the transmission between the gas turbine and air compressor of an aircraft engine

• US 5,391,125 A
• Filed: 11/12/1992
• Issued: 02/21/1995
• Est. Priority Date: 11/12/1991
• Status: Expired due to Term

• Current Assignee: Calyon S.A. - Succursale di Milano, Credit Agricole Corporate & Investment Bank (Milan Branch), Royal Bank of Scotland Group PLC (Her Majesty's Treasury), Royal Bank Of Scotland PLC, Bayerische Hypo- Und Vereinsbank AG (Unicredit SPA)
• Original Assignee: Fiatavio S.p.A.
• Inventors: Turra, Sergio, Bologna, Valter
• Primary Examiner(s): Pitts, Andrea L.
• Application Number:
  US07/975,414
• Time in Patent Office: 831 Days
• Field of Search: 475/317, 475/331, 475/346
• US Class Current: 475/346
• CPC Class Codes: F16H 1/2836 by allowing limited movement of the planets relative to the planet carrier or by using free floating planets

Abstract

A speed reducer has a sun gear for connection to a turbine of an engine and a planet carrier supporting a number of planetary gears meshing with the sun gear and with the ring gear fitted to the engine mounting. According to the present invention, the planet carrier has a first annular element having pairs of seats for pins on each of which rotates one of the planetary gears. A second annular element for connection to a compressor of the engine has a number of axial arms fitted inside respective cavities of the first annular element. An end of each axial arm is connected to a portion of the first annular element that is substantially equidistant between to the seats of each of the pairs of seats.

Claims

1. An epicyclic speed reducer designed for fitment to a transmission between a gas turbine and air compressor of an aircraft turbine engine, said reducer comprising a sun gear (5) connected to said turbine;

a planet carrier (6) connected to said air compressor coaxially to said sun gear (5) and supporting a number of planetary gear (7) meshing with one of said sun gear (5); and

a ring gear (8) fitted to a mounting (9) of said engine and with which said planetary gear (7) mesh;

characterized by the fact that said planet carrier (6) comprising a first annular element (10) having a number of pairs of seats (11) for pins (13) on each of which rotates one of said planetary gears (7), and a number of holes (16) each interposed between two continuous planetary gears (7);

a second annular element (17) connected to said compressor and having a number of cantilever axial arms (18), each designed to fit inside one of said holes (16) on said first element (10);

connecting means (19) for connecting the end of each said cantilever axial arms (18) to a portion (20) of said first element (10), which portion (20) is substantially equidistant in relation to these seats (11) in each said pair of seats of said pins (13);

said connecting means comprising a hinge (19) having a proper axis which is positioned radially in relation to a reducer axis, and is equidistant in relation to the seats (11) in each said pair of seats of said pins (13).

2. A speed reducer as claimed in claim 1, characterized by the fact that each said arm (18) presents a rectangular section, and said hinge comprises a radial pin (25) inserted inside a radial hole on said first element (10) and inside a hole on said arm (18);

bushings (26) being inserted between said pin (25) and said holes.

3. A speed reducer as claimed in claim 1, characterized by the fact that said arms project from one side of said second element (17) and said second element (17) presents a sleeve (33) connected to said air compressor and projecting from an opposite side of said second element (17).

4. A speed reducer as claimed in claim 1, characterized by the fact that each of said pins (13) on which rotate said planetary gears (7) presents a cylindrical central portion (35) constituting a supporting seat for a respective said planetary gear (7);

and two cylindrical end portions (36) smaller in diameter than said central portion (35) and each force fitted inside a respective said seat (11) on said first element (10) of said planet carrier (6);

said central portion (35) presenting two annular grooves (50), each open on a side facing a respective end portion (36) and each defined by a surface (51) blending with an outer surface of said end portion (36).

5. A speed reducer as claimed in claim 4, characterized by the fact that an axial depth of each said annular groove (50) is at least equal to 1/5 of the axial length of said central portion (35) of said pin (13).

6. A speed reducer as claimed in claim 4, characterized by the fact that, between each said pin (13) and respective said planetary gear (7), there is inserted a bushing (52) force fitted inside said planetary gear (7).

7. A speed reducer as claimed in claim 1, characterized by the fact that said ring gear (8) is fitted to said mounting (9) by means of elastic connecting elements.

8. A speed reducer as claimed in claim 7, characterized by the fact that said elastic connecting elements comprise flexible blades (68) arranged about said ring gear (8) and each having one end fitted to said ring gear (8) and an opposite end fitted to said mounting (9).

9. A speed reducer as claimed in claim 7, characterized by the fact that said elastic elements comprise flexible rings coaxial with said ring gear (8) and fitted to one of said ring gear (8) and said mounting (9).

10. A speed reducer as claimed in claim 1, wherein said sun gear (5) and said planetary gears (7) comprise two sets of external helical teeth;

characterized by the fact that said ring gear (8) comprises two rings (59), each having internal helical teeth meshing with one of said sets of teeth on said planetary gears, and external teeth meshing with internal teeth on a sleeve (61) having an annular rib (62) to which are fitted two shoulder rings (63), each of which provides for axially locking one of said rings (59) to said sleeve (61).

11. A speed reducer as claimed in claim 10, characterized by the fact that it comprises an annular box (65) fitted to said mounting (9) and housing said rings (59), said sleeve (61) and said shoulder rings (63);

each said shoulder ring (63) presenting a number of outward radial projections;

said annular box (65) presenting two sets of inward radial projections (67); and

at least one flexible blades (68) being inserted between each said projection (66) on one of said shoulder rings (63) and a corresponding radial projection (67) on said box (65).

12. A speed reducer as claimed in claim 1, characterized by the fact that said sun gear (5) presents a hollow shaft (69) housed substantially inside said sleeve (33) of said planet carrier (6);

said hollow shaft (69) presenting convex internal teeth (70) meshing with convex teeth on a shaft (3) of said turbine.

13. A planet carrier for an epicyclic speed reducer between a gas turbine and air compressor of an aircraft turbine engine, said speed reducer having a sun gear (5) for connection to said gas turbine and a ring gear (8) for fitting to a mounting (9) of said engine, said planet carrier (6) being for connection to said air compressor coaxially of said sun gear (5) and for supporting planetary gears (7) meshing with said sun gear and said ring gear, said planet carrier (6) comprising:

a first annular element (10) having an axis and pairs of seats (11) on axially opposite sides;

pins (13) respectively in said seats for each pin to rotatably carry a planetary gear (7);

holes (16) in said first annular element respectively interposed between each adjacent two of said planetary gears (7);

a second annular element (17) for connection to a compressor and having a number of cantilever axial arms (18) respectively fitting inside said holes (16) with clearance; and

connecting means (19) respectively connecting respective ends of said cantilever axial arms (18) to respective portions (20) of said first annular element (10) that are substantially equidistant between said seats (11) of respective of said pairs of seats, each said connecting means comprising a hinge (19) having an axis positioned radially in relation to said axis of said first annular element and equidistant said seats (11) of said respective of said pair of seats.