IP Library Patent Application 18685374
Patent Application
App. No. 18/685,374

Proprotor Blade Retention System

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Quick Facts
Patent No.
US None
App. No.
18/685,374
Abstract

In one aspect, this application describes a blade retention system—for a variable pitch aircraft proprotor system—comprising a double conical blade root encapsulated by a split sleeve. Some embodiments described additionally include fail-operational features. The preload of the blade pitch bearings pushes the metallic split sleeve into the bond line with the blade root.

Claims (16)

1 . A proprotor system comprising:

a proprotor blade root;

a first and second proprotor blade pitch bearing;

a split sleeve interposed between the proprotor blade root and the first proprotor blade pitch bearing;

a preload system configured to apply a preload force to the first and second blade pitch bearing; and

wherein the preload system is configured to maintain the split sleeve in compression against the blade in a first and second direction.

2 . The proprotor system of claim 1 wherein the split sleeve comprises metal.

3 . The proprotor system of claim 1 wherein the split sleeve is configured to accommodate the proprotor blade pitch bearings.

4 . The proprotor system of claim 1 additionally comprising a redundant centrifugal force retention device.

5 . The proprotor system of claim 4 wherein the redundant centrifugal force retention device comprises a threaded split collar.

6 . The proprotor system of claim 5 wherein the redundant centrifugal force retention device additionally comprises a nut configured to transmit torque between the proprotor blade root and the split sleeve.

7 . The proprotor system of claim 6 wherein the threaded split collar is larger in diameter than an inside diameter of the first proprotor blade pitch bearing.

8 . The proprotor system of claim 7 wherein the split sleeve comprises a groove and wherein the split collar is disposed at least partially in the groove.

9 . The proprotor system of claim 1 additionally comprising a blade pitch horn.

10 . The proprotor system of claim 9 wherein the proprotor blade retention system does not comprise any composite to metallic fasteners.

11 . The proprotor system of claim 1 where the first and second direction are opposite.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 6, 2025
From: OVERAIR, INC.
To: ARCHER AVIATION INC.
Reel/Frame 071041/0433 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 24, 2025
From: ORBON, JAMES, MR.; KETCHAM, SCOTT, MR.; BUEHNE, ALAN, MR.
To: OVERAIR, INC.
Reel/Frame 070305/0824 →