Aircraft propulsion means

Claim 2

An aircraft adapted to cruise at high subsonic speeds including propulsion means mounted thereon, said propulsion means including a propeller fan having at least 10 blades wherein the ratio of the total blade area to the area swept by the blades is at least 0.8 and which operates in the cruise condition at disc loading of at least 30 lb/ft 2 and consequently imparts to its slipstream a component of swirl of at least 10° in a given sense, and a multibladed stator arranged with respect to said propeller fan to impart a considerable component of swirl in the opposite sense so that the total swirl imparted to the slipstream is nil or relatively low, whereby the diameter of the propeller fan may be relatively low whilst maintaining a relatively high propulsive efficiency and thrust.

Claim 3

An aircraft adapted to cruise at high subsonic speeds including propulsion means mounted thereon, said propulsion means including a multibladed unshrouded propeller fan of relatively small diameter wherein the ratio of the area swept by the blades is relatively high and which in use operates in the cruise condition at such high disc loadings that it imparts to the slipstream a component of swirl of at least 10° in a given sense and a multibladed stator of similar diameter to the propeller fan disposed adjacent the propeller fan and including a sufficient number of blades to impart a considerable component of swirl in the opposite sense so that the total swirl imparted to the slipstream is nil or relatively low, whereby the proposal means may be mounted relatively close to a surface of the aircraft without causing significant interferences.

Claim 4

An aircraft adapted to cruise at high subsonic speeds including propulsion means mounted thereon, said propulsion means including a multibladed unshrouded propeller fan of relatively small diameter wherein the ratio of the area swept by the blades is relatively high and which in use operates in the cruise condition at such high disc loadings that it imparts to the slipstream a component of swirl of at least 10° in a given sense and a multibladed stator of similar diameter to the propeller fan disposed adjacent the propeller fan and including a sufficient number of blades to impart a considerable component of swirl in the opposite sense so that the total swirl imparted to the slipstream is nil or relatively low, whereby the proposal means may be mounted relatively close to a surface of the aircraft without causing significant interferences.

Claim 5

An aircraft propulsion means according to claim 2 or claim 1, wherein the propeller fan includes from 10 to 15 blades.

Claim 6

An aircraft propulsion means according to claim 2 or claim 1, wherein said stator includes 10 to 15 blades.

Claim 7

An aircraft propulsion means according to claim 2 or claim 1, wherein the swirl angle generated by the propeller fan lies in the range of from 10° to 25°.

Claim 8

An aircraft propulsion means according to claim 2 or claim 1, wherein the pitch of the blades of the propeller fan may be varied.

Claim 9

An aircraft propulsion means according to claim 2 or claim 1, wherein the pitch of the blades of the stator may be varied.

Claim 10

An aircraft as claimed in claim 2 or claim 1, propulsion means are mounted generally below a wing portion of the aircraft, wherein the diameter of the propeller fan is such that substantially all the slipstream passes below the wing, but that sufficient ground clearance is maintained to allow take-off and landing maneuvers.

Claim 11

An aircraft as claimed in claim 2 or claim 1, wherein the propeller fan includes a center body portion from which the blades extend, the body portion being shaped so that the velocity of the air flow through the propeller fan adjacent the body portion is reduced.