Ram air turbines
AssigneeA/S Kongsberg Vapenfabrikk
InventorSten O. Olsen
Life of this patent
Estimating the term…
Abstract
A cup shaped disc (13) consisting of a central portion (20) having radially extending blades (18) is attached with its central portion to the protruding hub portion (12) of a radial flow turbine wheel (2) consisting of a backing plate (10) extending transversely to its rotational axis (7) and having axially protruding turbine blades (11) in addition to the protruding hub. At high rotational speeds this disc (13) will tend to straighten out, whereby the effective portion of the turbine blades will be reduced and the increase in the rotational speed restricted. This is of importance in ram air turbines for missiles.
Claims8
A ram air turbine for driving an electric generator in a missile, the turbine comprising a turbine housing having a flow passage for ducting the incoming ram air, a turbine wheel having blades to which the ram air is supplied from said flow passage, wherein the turbine wheel includes means actuated by centrifugal force upon an increase in the rotational speed of the turbine sheel for uniformly restricting the cross section of the flow passage to all of said turbine blades and thus the amount of ram air acting on the blades of the turbine wheel to an extent depending upon the rotational speed of the turbine wheel,
- wherein the turbine wheel is a radial turbine wheel having a protruding central hub portion and the incoming ram air is incident upon the turbine wheel along the axial direction and thereafter flows past the blades in a radial direction, and wherein the centrifugal force actuated means comprises a disc of cup shape and inverted relative to the axial direction of the incoming ram air, the central portion of said disc being attached to said protruding hub of said radial turbine wheel, said disc being manufactured from a resilient material which upon rotation of the turbine wheel allows straightening-out deflection of the cup-shaped disc due to centrifugal forces, the outer edges of the disc lifting from an undeflected position against the turbine wheel.
Dependencies are inferred from the claim text.