Helicopter blade droop stop with slidable droop stop seat

• US 4,549,852 A
• Filed: 12/16/1983
• Issued: 10/29/1985
• Est. Priority Date: 12/16/1983
• Status: Expired due to Fees

• Current Assignee: United Technologies Corporation (Rtx Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Hibyan, Edward S.
• Primary Examiner(s): Powell, Jr., Everette A.
• Application Number:
  US06/562,056
• Time in Patent Office: 683 Days
• Field of Search: 416/134 A, 416/138 A, 416/140 A, 416/140 R, 416/141
• US Class Current: 416/140
• CPC Class Codes: B64C 27/322 Blade travel limiting devices, e.g. droop stops

Abstract

Apparatus for supporting the rotor blades of a helicopter is disclosed. Support in droop under both statically and dynamically loaded conditions is discussed. The droop stop mechanism 34 has low susceptibility to the deleterious effects of snow/ice or dirt contamination. The droop stop seat 42 is mounted for rotation in a corresponding receptacle 50 at the base of the rotor blade assembly 14 and is slidable between static stop and dynamic stop positions along the pitch axis of the blade to be supported.

Claims

1. In a helicopter rotor hub assembly of the type having a plurality of rotor blades extending outwardly from a central hub, each blade joined thereto at an elastomeric bearing permitting universal movement of the mounted blade with respect to the hub, improved apparatus for supporting the blades under static and dynamic blade loads comprising:

a droop stop mounted on the rotor hub and facing outwardly toward the airfoil section of the rotor blade to be supported; and

a droop stop seat attached to the base of the rotor blade to be supported and having a conical surface at one end thereof facing inwardly toward the rotor hub in opposition to the fixed droop stop, wherein the droop stop seat is mounted on the pitch axis of the blade and is slidable along the pitch axis to a first position for limiting, in conjunction with the droop stop, blade droop under statically loaded conditions and to a second position for limiting, in conjunction with the droop stop, blade droop under dynamically loaded conditions.

2. The invention according to claim 1 which further includes means responsive to rotational forces on the rotor hub for sliding the droop stop seat along the pitch axis of the blade to said second position for limiting blade droop under dynamic blade loads.

3. The invention according to claim 2 which further includes means for sliding the droop stop seat along the pitch axis of the blade to said first position in the absence of rotational forces on the rotor hub for limiting blade droop under static blade loads.

4. The invention according to claim 3 where said means for sliding the droop stop seat along the pitch axis of the blade to said first position in the absence of rotational forces includes:

a cammed seat actuator, having a dynamic surface and a static surface,

a pin attaching the seat actuator to the blade in a manner affixing the seat actuator to the blade in proximity to the end of said droop stop seat opposite said conical surface, yet permitting rotation of the dynamic and static surface of the actuator about the pin; and

a restoring spring attached at one end to the actuator and at the other end to the blade for rotating the actuator about the pin such that the static stop surface of the actuator opposes said end of the droop stop seat in the absence of rotational forces on the blade,

wherein the cammed actuator further has a weighted portion located remotely from the dynamic and static surfaces and oriented so as to be capable of rotating the dynamic surface about the pin in response to rotational forces on the blade and into opposition with said end of the droop stop seat.

5. The invention according to claim 4 which further includes a plug disposed in the end of the slidable droop stop seat opposite said conically surfaced end where said plug is rotatable with respect to the seat when contacted by the cammed seat actuator.

6. The invention according to claim 1 wherein the droop stop mounted on the rotor hub is pinned thereto and rotatable about said pin for alignment of the droop stop when in contact with the droop stop seat.

7. The invention according to claim 6 which further includes a compliant material disposed between the droop stop and the rotor hub for supporting the pinned droop stop in a manner permitting limited rotation of the stop about the pin for purposes of alignment with the droop stop seat.

8. The invention according to claim 7 which further includes a flapping stop pinned to the rotor hub in a position opposing the droop stop seat wherein the flapping stop is rotatable about said pin for alignment of the flapping stop when in contact with the droop stop seat.