Hub assembly and propeller assemblies

Patent metadata

Field	Value
Publication number	US-10137980-B2
Application number	US-201514797233-A
Country	US
Kind code	B2
Filing date	Jul 13, 2015
Priority date	Jul 13, 2015
Publication date	Nov 27, 2018
Grant date	Nov 27, 2018

Abstract

Hub assembly and propeller blade assemblies incorporating partial hub assembly having a backing plate with a set of partial root seats and a set of clamps selectively operably couplable to the backing plate with each clamp defining a second partial root seat and wherein when a clamp is coupled to the backing plate a root seat is formed, propeller blades having roots are received within the root seats.

First claim

What is claimed is:

1. A propeller assembly, comprising:
a partial hub, comprising:
a backing plate comprising a plate portion having contoured portions defining a set of partial root seats extending from the plate portion along its periphery; and
a set of clamps selectively operably couplable to the backing plate with each clamp defining a second partial root seat and wherein when a clamp is coupled to the backing plate, a root seat is formed; and

a variable pitch propeller blade having a root rotatably received within the root seat;
further comprising a cover operably coupled over the set of clamps, wherein the cover comprises at least one opening configured to accommodate a pitch control unit.

2. The propeller assembly of claim 1 , wherein the backing plate of the partial hub is at a rear side of the propeller assembly and provides a mounting surface to an engine.

3. The propeller assembly of claim 1 , wherein each clamp of the set of clamps is fastened to the backing plate.

4. The propeller assembly of claim 1 , further comprising a retainer selectively operably coupled to the partial hub and configured to retain the root of the propeller blade within the partial hub when the retainer is coupled to the partial hub.

5. The propeller assembly of claim 4 , further comprising a seal located within a portion of the retainer.

6. The propeller assembly of claim 4 , further comprising a ring nut between the retainer and a bearing assembly located between the root and the partial hub.

7. The propeller assembly of claim 1 , further comprising a bearing assembly between the root and the partial hub, wherein the bearing assembly allows the propeller blade to rotate within the partial hub.

8. The propeller assembly of claim 7 , wherein the bearing assembly comprises a parallel roller bearing assembly, a ball bearing assembly, or a taper roller bearing assembly.

9. The propeller assembly of claim 1 , comprising multiple bearing assemblies between the root and the partial hub and at least one bearing assembly of the multiple bearing assemblies is preloaded.

10. A propeller assembly, comprising:
a partial hub, comprising:
a backing plate comprising a plate portion having a contour portion partially defining a root seat extending from the plate portion along its periphery; and
a clamp selectively operably couplable to the backing plate to define a second partial root seat and wherein when a clamp is coupled to the backing plate, a root seat is formed;

a variable pitch propeller blade having a root rotatably received within the root seat;
a bearing assembly provided between the root and the partial hub, wherein the bearing assembly allows the blade to rotate within the partial hub; and
a retainer mounted to an outer periphery of the backing plate and an outer periphery of the clamp, and configured to retain the propeller blade within the root seat,
further comprising a cover operably coupled over the set of clamps, wherein the cover comprises at least one opening configured to accommodate a pitch control unit.

11. The propeller assembly of claim 10 , wherein the partial hub comprises a backing plate comprising a plate portion having multiple partial root seats and complementary clamps defining multiple second partial root seats.

12. The propeller assembly of claim 10 , wherein the contour portion and an interior of the clamp define a contoured root seat.

Assignees

• Ge Aviation Systems Llc

Inventors

• Pawar Rajendra Vishwanath
• Yamarthi David Raju
• Kurvinkop Amit Arvind
• Kumar Sandeep
• Periasamy Murugesan
• Ganiger Ravindra Shankar
• Agrawal Bajarang
• G Nagashiresha

Classifications

• F01D5/3015

  with side plates · CPC title

• B64C11/06 Primary

  for variable-pitch blades · CPC title

• F01D5/30

  Fixing blades to rotors; Blade roots {; Blade spacers} · CPC title

• B64C11/02 Primary

  Hub construction · CPC title

• B64C11/30

  Blade pitch-changing mechanisms · CPC title