Ring cam and ring cam assembly for dynamically controlling pitch of cycloidal rotor blades
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B64C-011/30
B64C-027/605
F01D-005/12
B64C-027/72
B64C-039/00
출원번호
US-0764957
(2013-02-12)
등록번호
US-9346535
(2016-05-24)
발명자
/ 주소
Adams, Zachary H.
출원인 / 주소
The United States of America as represented by the Secretary of the Air Force
대리인 / 주소
AFMCLO/JAZ
인용정보
피인용 횟수 :
0인용 특허 :
11
초록▼
A new ring cam and ring cam assembly, developed for providing more diverse dynamic pitching schedules for cyclorotor blades, particularly for providing both cyclic and collective pitch control, can be used for any apparatus where dynamic variation of cam controlled movement is needed. The new ring c
A new ring cam and ring cam assembly, developed for providing more diverse dynamic pitching schedules for cyclorotor blades, particularly for providing both cyclic and collective pitch control, can be used for any apparatus where dynamic variation of cam controlled movement is needed. The new ring cam has its cam surface on the inside of a ring, the cam surface defining a plurality of different cam profiles which can be dynamically chosen and applied according to need. The different cam profiles are provided by different configurations and by combinations of those configurations. One configuration uses a plurality of adjacent different cam profiles across the inside width of the ring, so that a cam follower follows different cam profiles as it moves across or relative to the cam surface. Another configuration moves a center axis of the ring in relation to the axis of rotation of the cyclorotor, or other rotating device, to dynamically change the effective cam profile. Still another configuration rotates the ring to dynamically change the effective cam profile. The new ring cam assembly includes a cam follower which, for its originally developed use, is operatively interconnected with a cyclorotor blade.
대표청구항▼
1. A ring cam, comprising a ring, having: (a) a perimeter about a center axis;(b) a width generally parallel with the center axis; and,(c) an inside cam surface, facing the center axis, defining a cam profile, wherein the cam profile varies along both the perimeter and the width. 2. The ring cam acc
1. A ring cam, comprising a ring, having: (a) a perimeter about a center axis;(b) a width generally parallel with the center axis; and,(c) an inside cam surface, facing the center axis, defining a cam profile, wherein the cam profile varies along both the perimeter and the width. 2. The ring cam according to claim 1, wherein the inside cam surface defines a plurality of adjacent cam profiles across the width. 3. A ring cam assembly, comprising: (a) a ring, having: (i) a perimeter about a center axis;(ii) a width generally parallel with the center axis; and,(iii) an inside cam surface, facing the center axis, defining a cam profile,wherein the cam profile varies along both the perimeter and the width; and,(b) a cam follower for following the inside cam surface. 4. The ring cam assembly according to claim 3, wherein the inside cam surface defines a plurality of adjacent cam profiles across the width. 5. The ring cam assembly according to claim 4, wherein the cam follower is point-like where it contacts a cam profile. 6. A ring cam assembly for controlling the pitch of a cyclorotor blade of a cyclogyro, comprising: (a) a ring, having: (i) a perimeter about a center axis;(ii) a width generally parallel with the center axis; and,(iii) an inside cam surface, facing the center axis, defining a cam profile;wherein the cam profile varies along both the perimeter and the width; and,(b) a cam follower for following the inside cam surface, wherein the cam follower is operatively interconnected with the cyclorotor blade. 7. The ring cam assembly for controlling the pitch of a cyclorotor blade according to claim 6, wherein the inside cam surface defines a plurality of adjacent cam profiles across the width. 8. The ring cam assembly for controlling the pitch of a cyclorotor blade according to claim 7, wherein the cam follower is point-like where it contacts a cam profile. 9. The ring cam assembly for controlling the pitch of a cyclorotor blade according to claim 6, wherein the cyclorotor has an axis of rotation and the ring cam assembly is configured so that the ring center axis can be moved relative to the axis of rotation of the cyclorotor. 10. The ring cam assembly for controlling the pitch of a cyclorotor blade according to claim 6, wherein the cyclorotor has an axis of rotation and the ring cam assembly is configured so that the ring can be rotated about its center axis. 11. A method for controlling the movement of an apparatus part, comprising the steps of: (a) providing a ring cam, having: (i) a perimeter about a center axis;(ii) a width generally parallel with the center axis; and,(iii) an inside cam surface, facing the center axis, defining a cam profile, wherein the cam profile varies along both the perimeter and the width;(b) providing a cam follower for following the cam surface, wherein the cam follower is operatively connected to the apparatus part; and,(c) moving the cam follower across the cam surface to follow different cam profiles. 12. A method for controlling the pitch of a cyclorotor blade, comprising the steps of: (a) providing a ring cam, having: (i) a perimeter about a center axis;(ii) a width generally parallel with the center axis; and,(iii) an inside cam surface, facing the center axis, defining a cam profile, wherein the cam profile varies along both the perimeter and the width;(b) providing a cam follower for following the cam surface, wherein the cam follower is operatively connected to the cyclorotor blade; and,(c) moving the cam follower across the cam surface to follow different cam profiles.
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이 특허에 인용된 특허 (11)
Bogrash, Philip, Cycloidal rotor with non-circular blade orbit.
Gonzales Gilbert R. (677 Creed Ave. Las Cruces NM 88005) La Monica ; Jr. John A. (1607 N. Euclid Tucson AZ 85719), Lift generating mechanism for an aircraft.
Servanty Pierre (14 Avenue Jean-Jacques Rousseau 93600 Aulnay Sous Bois FRX), Rotor for developing sustaining and propelling forces in a fluid, steering process, and aircraft equipped with such roto.
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