Blade retention apparatus with elastomeric preload
AssigneeUnited Technologies Corporation
InventorsJohn A. Violette, Peter D. Ventura
Life of this patent
Estimating the term…
Abstract
Preloading and retention of a variable-pitch, light-weight propeller blade (10) are achieved through a retention assembly wherein the blade shank (20) is retained within a hub arm (24) with an inboard angular contact pitch change bearing (30) and an outboard angular contact anti-rocking bearing (50) which is elastomerically preloaded. The outboard bearing (50) is disposed intermediate a bearing race (34) on the shank (20) and an annular frusto-conical rigid support member (62) which is biased outboardly against the anti-rocking bearing (50) by an annular frusto-conical body (72) of elastomeric material selected to impart a desired stiffness and/or damping effect to the retention assembly.
Claims10
A blade retention assembly for mounting a variable-pitch propulsor blade in a propulsor hub, said blade retention assembly comprising:
- a) a blade retention member extending axially from said blade;
- b) hub arm means extending radially outwardly from the propulsor hub and defining a retention socket for receiving therein said blade retention member;
- c) inboard pitch change bearing means operatively disposed in said retention socket intermediate said blade retention member and said hub arm means;
- d) outboard anti-rocking bearing means operatively disposed about said blade retention member at a location outboard of said inboard pitch change bearing means;
- and
- e) elastomeric preloading means operatively disposed intermediate said outboard anti-working bearing means and said hub arm means for selectively preloading said outboard anti-rocking bearing means outboardly whereby said inboard pitch change bearing means is thereby preloaded against said hub arm means, said elastomeric preloading means being preselected to provide a desired damping effect and to impart a desired stiffness to said retention assembly.
A blade retention assembly for mounting a variable-pitch propulsor blade in a propulsor hub, said blade retention assembly comprising:
- a) a blade retention member extending axially from said blade, said blade retention member having a primary bearing race and a secondary bearing race, the secondary bearing race disposed axially outboard of the primary bearing race;
- b) hub arm means extending radially outwardly from the propulsor hub and defining a retention socket for receiving therein said blade retention member, said hub arm means having a radially inboard generally cylindrical body portion, a radially outboard generally cylindrical lip portion, and a circumferentially outwardly diverging wall portion extending therebetween, said inboard body portion having an inner circumferential surface providing a primary bearing race and said diverging wall portion providing an angled interiorly facing surface;
- c) inboard pitch change bearing means operatively disposed in said retention socket in angular contact relationship intermediate the primary bearing race of said blade retention member and the primary bearing race of said hub arm means;
- d) outboard anti-rocking bearing means operatively disposed in the secondary bearing race about said blade retention member at a location outboard of said inboard pitch change bearing means;
- and
- e) elastomeric preloading means for selectively preloading said outboard anti-rocking bearing means outboardly whereby said inboard pitch change bearing means is thereby preloaded against said hub arm means, said elastomeric preloading means having an annular frusto-conical rigid support member having an angled interiorly facing surface disposed in opposed facing relationship to the secondary bearing race of said blade retention member with said outboard anti-rocking bearing means operatively disposed therebetween, and an annular frusto-conical body of elastomeric material having an interiorly facing surface abutting an exteriorly facing surface of said rigid support member and an exteriorly facing surface abutting the angled interiorly facing surface of the diverging wall portion of said hub arm means.
Dependencies are inferred from the claim text.