Aircraft with a modified gear, and method of producing the gear
There is described a helicopter having a transmission for transmitting motion from a driving member to a driven member; the transmission has at least a first gear driven by the driving member, and a second gear meshing with the first gear and in turn driving the driven member; the first and second gear have teeth shaped so that the gears mesh with one another at at least two pairs of respective simultaneously meshing teeth; the teeth of at least one of the gears have a profile having an end portion relieved with respect to a starting theoretical involute; and the pattern of the distance between the points of the end portion and the starting involute along an axis of the tooth has at least a first and a second segment sloping with respect to each other.
1. An aircraft ( 1 ) comprising:
a transmission ( 5 ) for transmitting motion from a driving member to a driven member;
said transmission ( 5 ) comprising a first gear ( 8 ; 10 ) driven by said driving member and a second gear ( 10 ; 12 ) meshing with said first gear ( 8 ; 10 ) and in turn driving said driven member;
each of said first and said second gears ( 8 , 10 ; 10 , 12 ) having teeth ( 16 , 17 , 18 ) shaped so that said first and second gears ( 8 , 10 ) mesh with one another at at least two pairs of respective simultaneously meshing teeth ( 16 , 17 ; 17 , 18 );
each of said teeth ( 16 , 17 , 18 ) of at least one of said first and second gears ( 8 , 10 , 12 ) has a profile ( 19 ) comprising a root portion ( 20 ) in the form of a starting theoretical involute (E) and an end portion ( 21 ) relieved with respect to said starting theoretical involute (E);
a pattern (G) of the distance between the points of said end portion ( 21 ) and said starting theoretical involute (E) along an axis (A, H) of said tooth ( 16 , 17 , 18 ) comprising at least a first segment (B) and a second segment (C) sloping with respect to each other and with respect to said starting theoretical involute (E).
2. The aircraft as claimed in claim 1 , wherein said distance increases along said axis (A, H) from a root ( 27 ) of said tooth ( 16 , 17 , 18 ) to a free end ( 22 ) of said tooth ( 16 , 17 , 18 ).
3. The aircraft as claimed in claim 2 , wherein said first segment (B) slopes less than said second segment (C) with respect to said axis (A, H); and in that said first segment (B) precedes said second segment (C) along said axis (A, H) from said root to said free end ( 22 ) of said tooth ( 16 , 17 , 18 ).
4. The aircraft as claimed in claim 1 , wherein said pattern (G) comprises a curved portion (L) interposed between said first and said second segment (B, C).
5. The aircraft as claimed in claim 4 , wherein a slope, with respect to said axis (A, H), of a driven tangent at each point of said curved portion (L) ranges between said slope of said first segment (B) and said slope of said second segment (C) with respect to said axis (A, H).
6. The aircraft as claimed in claim 1 , wherein said first and said second gear ( 8 , 10 ) mesh with each other at a pressure angle (α) of less than twenty degrees.
7. A method of producing a gear ( 8 , 10 , 12 ) for an aircraft ( 1 ), comprising the steps of:
generating a gear ( 8 ) comprising a number of teeth ( 16 ), each having an outer involute profile (E); said teeth ( 16 ) being shaped so that at least two said teeth ( 16 ) of said gear ( 8 ) mesh with a further gear ( 10 ); and
removing material from an end portion ( 21 ) of each said tooth ( 16 ) to impart to said end portion ( 21 ) a profile in the form of a relieved involute (E);
said end portion ( 21 ) being shaped so that a pattern (G) of the distance between the points of said end portion ( 21 ) and said involute (E) comprises at least a first and a second segment (B, C) sloping with respect to each other and with respect to said involute (E).
8. The method as claimed in claim 7 , wherein said step of removing material shapes said profile ( 19 ) so that said pattern (G) comprises a curved portion (L) interposed between said first and said second segment (B, C).