$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

과학기술 지식인프라 ScienceON

상세검색 다국어 입력
도움말도움말

특허 상세정보

MyON담기
내보내기

Fin control actuator having a fin shaft lock device

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/24   
미국특허분류(USC) 244/75R ; 244/324 ; 244/224
출원번호 US-0090801 (1993-07-12)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 11  인용 특허 : 0
초록
▼

A fin control actuator for missiles carried on aircraft has a device which locks the fin shaft against aerodynamic loads and prevents the transmission of these loads through the drive train. The fin shaft lock includes a plunger which has a cam having a locking portion for engaging the output shaft and preventing the output shaft from rotating in one direction when the plunger is in the locking position. The cam also has a camming portion for engaging the output shaft and pushing the plunger to the retracted position when the output shaft rotates in the ...

대표
청구항
▼

A fin control actuator for airborne missiles, which comprises: an actuating motor having a brake; a output shaft connected to a fin shaft and capable of rotating in a first direction and a second direction; a drive train connecting the motor to the output shaft; and a fin lock device for holding the output shaft when the motor brake is on, the fin lock device including a plunger capable of movement toward the output shaft into a locking position and away from the output shaft into a retracted position, spring means for urging the plunger into the locking...

이 특허를 인용한 특허 피인용횟수: 11

  1. Russom,Jeffery D.; White,Lawrence R.; Greenwood,James. Control surface assemblies with torque tube base. USP2008087410120.
  2. Mock, M Robert. Eccentric drive control actuation system. USP2010077755012.
  3. Wingett, Paul T.; Hanlon, Casey; Potter, Calvin C.. Flight control surface actuator assembly including a free trial mechanism. USP2009117610828.
  4. Betts, Byron; Ronquillo, John. Landing gear control system. USP2016089403591.
  5. Mock, M. Robert; Woodruff, Mark. Locking assembly for rotary shafts. USP2010047700902.
  6. Hawthorne,Dana D.. Locking device with solenoid release pin. USP2006107125058.
  7. William W. Hsu ; Matthew Miotla. Missile fin locking and unlocking mechanism including a mechanical force amplifier. USP2002036352217.
  8. Hsu William W. ; Bragg Duncan D.. Missile fin locking mechanism. USP2001066250584.
  9. Sankovic,John; Byrne,James; Piltz,Daniel. Missile fin locking method and assembly. USP2008017316370.
  10. Bugge, John F.; Willems, John D.. Resettable missile control fin lock assembly. USP2014048686328.
  11. DeHart, John K.. Rotational lock mechanism for actuator. USP2018019863745.

IPC 상위 출원인