Damping device for a supercritical transmission shaft
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B60K-017/24
F16C-027/02
F16F-015/02
B64C-027/14
출원번호
US-0595574
(2015-01-13)
등록번호
US-9677607
(2017-06-13)
발명자
/ 주소
Nevers, Romain
Aubertin, Ludovic
Marchand, Francois
출원인 / 주소
Airbus Helicopters
대리인 / 주소
Brooks Kushman P.C.
인용정보
피인용 횟수 :
0인용 특허 :
6
초록▼
A damping device for a shaft in rotation around an axis of rotation parallel to a direction (A). The said damping device includes a support, a plate, a collar, and clamping means. The said support is stationary and is provided with a first opening, with the said plate being provided with a second op
A damping device for a shaft in rotation around an axis of rotation parallel to a direction (A). The said damping device includes a support, a plate, a collar, and clamping means. The said support is stationary and is provided with a first opening, with the said plate being provided with a second opening and the said collar being provided with a third opening. The said shaft passes simultaneously through the said first, second, and third openings with, respectively, a first radial gap, a second radial gap, and a third radial gap, with the said third radial gap being smaller than the said first and second radial gaps. The said collar is movable with respect to the said support in a plane perpendicular to the said direction (A), with the said clamping means pressing the said plate against the said collar and the said collar against the said support.
대표청구항▼
1. A damping device for a shaft in rotation around an axis of rotation parallel to a direction with respect to a structure, with the damping device comprising: a support suitable for forming an integral part of the structure, with the support being provided with a first opening positioned perpendicu
1. A damping device for a shaft in rotation around an axis of rotation parallel to a direction with respect to a structure, with the damping device comprising: a support suitable for forming an integral part of the structure, with the support being provided with a first opening positioned perpendicular to the direction, anda plate provided with a second opening positioned perpendicular to the direction, with the shaft being suitable for passing simultaneously through the first opening and the second opening, with, respectively, a first radial gap with the support and a second radial gap with the plate;a collar provided with a third opening positioned perpendicular to the direction, with the collar being positioned between the support and the plate and being movable with respect to the support in a plane perpendicular to the direction, with the shaft being suitable for passing through the third opening, with a third radial gap with the collar, with the third radial gap being smaller than the first radial gap and the second radial gap; andclamping means that press, parallel to the direction, the plate in direct frictional contact with the collar and the collar in direct frictional contact with the support;wherein the damping device includes elastic centering means positioned radially around the collar; andwherein the elastic centering means consist of an elastic return ring positioned radially around the collar to re-center the collar. 2. The damping device according to claim 1, wherein the third radial gap is between 1 and 8 mm. 3. The damping device according to claim 1, wherein the clamping means include at least one elastic deformable means. 4. The damping device according to claim 3, wherein the clamping means include three compression springs. 5. The damping device according to claim 1, wherein said collar is made of a polyamide-imide thermoplastic. 6. The damping device according to claim 1, wherein the support and the plate are metallic. 7. The damping device according to claim 6, wherein the support and the plate are made of aluminum. 8. The damping device according to claim 6, wherein the support and the plate are made of steel. 9. The damping device according to claim 1, wherein the elastic centering means are positioned between the collar and the plate. 10. The damping device according to claim 1, wherein the elastic centering means are positioned between the collar and the support. 11. The damping device according to claim 1, wherein the damping device is suitable for a supercritical shaft. 12. A mechanical transmission system that includes: a structure;a shaft in rotation around an axis of rotation parallel to a direction with respect to the structure; andat least two bearings that are attached to the structure and that guide the shaft in rotation;wherein the mechanical transmission system includes at least one damping device according to claim 1. 13. The mechanical transmission system according to claim 12, wherein the shaft is a supercritical shaft. 14. The mechanical transmission system according to claim 12, wherein the structure is a tail boom of a rotary-wing aircraft, with the shaft being a transmission shaft that rotationally drives a rear rotor of the aircraft. 15. The mechanical transmission system according to claim 12 wherein the shaft in deformation comes into contact with the collar to displace the collar in in translation and in rotation; and wherein the elastic centering means apply a radial restoring force that moves the collar toward the axis of rotation of the shaft to counteract friction forces during the displacement of the collar and to re-center the collar.
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