Rotor system vibration absorber
AssigneeBell Helicopter Textron Inc.
InventorsAjay Sehgal, Cecil E. Covington, Mithat Yuce, Bryan W. Marshall
Life of this patent
Estimating the term…
Abstract
A vibration absorber having a mass member which when static is supported by in-plane springs spaced apart from a base plate, top plate and spring retaining structures. The mass member has a bumper surface for contacting a motion limiter in the base plate. The mass member, base plate and top plate can have a passageway through the axis. The vibration absorber can be tuned by proper selection of the springs, degree of precompression and the variation of the amount of mass by the addition or removal of mass tuning weights.
Claims19
A vibration absorber comprising:
- (a) a base plate having a top and bottom sides with an axis substantially normal thereto;
- (b) two or more spring retaining structures extending from said plate upwardly;
- (c) a motion limiter extending upwardly from said base plate about said axis;
- (d) a mass member having a predetermined shape having a top side, bottom side and out-of-plane sides and having a cylindrical surface extending downwardly therefrom and encircling said motion limiter;
- (e) one or more in-plane springs positioned between each of said retaining structures and one of the out-of-plane sides of said mass member and holding said mass member when static spaced apart from said retaining structures;
- and
- wherein said springs are selected such that said mass member during operation runs up against said motion limiter substantially continuously in a rapidly vibrating manner.
A vibration absorber for helicopter rotor systems comprising:
- (a) a base plate having a top and bottom side and an axis perpendicular thereto and defining a passageway concentric about the axis and a motion limiter assembly extending therefrom;
- (b) two or more spring retaining structures extending upwardly from said base plate, said structures being spaced apart from said axis;
- (c) a mass member having an axis therethrough and defining a passageway therethrough about the axis, said mass member having top side bottom side and out-of-plane sides and having a bumper surface;
- (d) one or more in-plane springs positioned between each of said spring retaining structures and a corresponding out-of-plane side of said mass member to hold the mass member spaced apart from each of said retaining structures;
- and
- (e) said motion limiter assembly comprising a bearing assembly having one side attached to said base plate and the other side attached to a contact ring such that the ring is rotatable with respect to said base plate.
A vibration absorber for helicopter rotor systems comprising:
- (a) a base plate having a top and bottom side and an axis perpendicular thereto and defining a passageway concentric to said axis, and spring receptacles on the top side of said base;
- (b) spring retaining structure extending upwardly from said base plate, said structures being spaced apart from said axis;
- (c) a mass member defining a passageway therethrough about an axis, and having a top side, bottom side, and out-of-plane sides, and spring receptacles on the top and bottom side and a bumper surface;
- (d) a top plate attached to said base and defining a passageway about its axis, top and bottom side, and spring receptacles in said bottom side;
- (e) one or more lower out-of-plane springs having a top and bottom end, the ends being positioned in the receptacles of said base plate and said mass member;
- (f) one or more upper out-of-plane springs having a top and bottom end, the ends being positioned in the receptacles of said base plate and said mass member;
- (g) one or more in-plane springs positioned between each of said retaining structures and corresponding out-of-plane of said mass member;
- (h) wherein said mass member is held by said spring spaced apart from said base plate, top plate and retaining structures when at rest;
- and
- (i) a motion limiter extending from said base plate and positioned such that it will be contacted by said bumper surface when the mass member is subjected to vibrating loads.
Dependencies are inferred from the claim text.