Rotor deployment mechanism for vertical take-off and landing aircraft
A deployment mechanism for use on an aerial vehicle adapted for vertical takeoff and landing using deployable thrust producing elements for takeoff and landing. The deployment mechanism may use linear actuation of a linkage assembly to deploy thrust producing rotor assemblies from a vertical thrust hove configuration to a horizontal thrust forward flight configuration. The aerial vehicle may include left side rotor assemblies and right side rotor assemblies which may be deployed by deployment mechanisms.
1. A propeller deployment mechanism for an electric vertical take-off and landing aircraft, said propeller deployment mechanism comprising:
an extendable linkage assembly, said extendable linkage assembly comprising one or more pivoting mounting points on a first end, said pivoting mounting points adapted to mount to fixed mounting points on an electric vertical take-off and landing aircraft;
an outboard bracket, said outboard bracket comprising a central axis, said outboard bracket coupled to a second end of said extendable linkage; and
and a deployment drive unit,
wherein said extendable linkage assembly is adapted to deploy said outboard bracket from a first position where said central axis of said outboard bracket is horizontal to a second position wherein said central axis of said outboard bracket is vertical.
2. The propeller deployment mechanism of claim 1 wherein said deployment drive unit is a linear drive unit.
3. The propeller deployment mechanism of claim 2 wherein said deployment drive unit comprises a drive screw.
4. The propeller deployment mechanism of claim 1 wherein said deployment drive unit wherein all of said outboard bracket is further forward from said plurality of main pivoting mounting points in said second position than in said first position, and wherein all of said outboard bracket is higher in said second position than in said first position.
5. The propeller deployment mechanism of claim 3 wherein said deployment drive unit wherein all of said outboard bracket is further forward from said plurality of main pivoting mounting points in said second position than in said first position, and wherein all of said outboard bracket is higher in said second position than in said first position.
6. The propeller deployment mechanism of claim 1 further comprising:
an electric motor, said electric motor comprising:
a rotor; and
a stator, wherein said stator is structurally coupled to said outboard bracket, and wherein said stator is rotationally coupled to said rotor; and
a propeller main hub, said propeller hub is structurally coupled to said rotor of said motor,
wherein said electric motor and said propeller hub deploy with said outboard bracket.
7. The propeller deployment mechanism of claim 2 further comprising:
an electric motor, said electric motor comprising:
a rotor; and
a stator, wherein said stator is structurally coupled to said outboard bracket, and wherein said stator is rotationally coupled to said rotor; and
a propeller main hub, said propeller hub is structurally coupled to said rotor of said motor,
wherein said electric motor and said propeller hub deploy with said outboard bracket.
8. The propeller deployment mechanism of claim 5 further comprising:
an electric motor, said electric motor comprising:
a rotor; and
a stator, wherein said stator is structurally coupled to said outboard bracket, and wherein said stator is rotationally coupled to said rotor; and
a propeller main hub, said propeller hub is structurally coupled to said rotor of said motor,
wherein said electric motor and said propeller hub deploy with said outboard bracket.
9. The propeller deployment mechanism of claim 7 further comprising a plurality of blades structurally coupled to said propeller main hub.
10. The propeller deployment mechanism of claim 8 further comprising a plurality of blades structurally coupled to said propeller main hub.
11. The propeller deployment mechanism of claim 9 further comprising a plurality of blades structurally coupled to said propeller main hub.
12. The propeller deployment mechanism of claim 1 wherein said extendable linkage assembly further comprises one or more multi-arm linkages.
13. The propeller deployment mechanism of claim 4 wherein said extendable linkage assembly further comprises one or more multi-arm linkages.
14. The propeller deployment mechanism of claim 6 wherein said extendable linkage assembly further comprises one or more multi-arm linkages.
15. The propeller deployment mechanism of claim 12 wherein said extendable linkage assembly further comprises;
a first multi-arm linkage comprising a first end and a second end, said first multi-arm linkage comprising first pivoting mounting point at its first end, said second end of said first multi-arm linkage pivotally coupled to said outboard bracket;
a second multi-arm linkage comprising a first end and a second end, said second multi-arm linkage comprising second pivoting mounting point at its first end, said second end of said second multi-arm linkage pivotally coupled to said outboard bracket;
wherein said an arm of said first multi-arm linkage is pivotally coupled to an arm of said second multi-arm linkage.
16. The propeller deployment mechanism of claim 13 wherein said extendable linkage assembly further comprises;
a first multi-arm linkage comprising a first end and a second end, said first multi-arm linkage comprising first pivoting mounting point at its first end, said second end of said first multi-arm linkage pivotally coupled to said outboard bracket;
a second multi-arm linkage comprising a first end and a second end, said second multi-arm linkage comprising second pivoting mounting point at its first end, said second end of said second multi-arm linkage pivotally coupled to said outboard bracket;
wherein said an arm of said first multi-arm linkage is pivotally coupled to an arm of said second multi-arm linkage.
17. The propeller deployment mechanism of claim 15 wherein said first multi-arm linkage is pivotally coupled to a first end of said outboard bracket, and wherein said second multi-arm linkage is pivotally coupled to a second end of said outboard bracket.
18. The propeller deployment mechanism of claim 16 wherein said first multi-arm linkage is pivotally coupled to a first end of said outboard bracket, and wherein said second multi-arm linkage is pivotally coupled to a second end of said outboard bracket.