[특허]Aircraft data acquisition and recording system

Aircraft data acquisition and recording system 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	G11B-005/02 G06F-015/74
출원번호	US-0664157 (1984-10-24)
발명자 / 주소	Miller Jr. Lawrence D. (Redmond WA) Owen Robert J. (Mercer Island WA) Kiltz Richard M. (Maple Valley WA)
출원인 / 주소	Sundstrand Data Control, Inc. (Redmond WA 02)
인용정보	피인용 횟수 : 139 인용 특허 : 0

초록 ▼

Disclosed is a combined flight data recorder data aquisition circuitry (10) and airborne integrated data circuitry (12) that can be variously packaged to supplement and update existing aircraft systems or serve as a standalone flight data recording and/or airborne integrated data system. The flight data recorder system circuitry (10) and airborne integrated data system circuitry (12) are separately programmed microprocessor based systems that are capable of processing aircraft parametric signals provided by a variety of aircraft signal sources. In the disclosed arrangement, the airborne integrated data system circuitry (12) is arranged and programmed to automatically monitor engine start and shutdown procedures, aircraft takeoff and cruise and to provide a landing report that indicates fuel consumption and landing weight. To minimize memory storage requirements and provide readily available engine condition information, the automatic monitoring consists of a single set of signals for each monitored condition and the information is converted to standard engineering units. Monitoring of selected parametric signals to detect excessive levels also is provided. Stored data is periodically retrieved by means of a ground readout unit (30).

대표청구항 ▼

An aircraft data acquisition and recording system for supplying retrievable digitally encoded signals representative of a pluralty of applied parametric flight data and aircraft performance signals, said plurality of parametric flight data and aircraft performance signals including analog signals and discrete signals, said aircraft data acquisition and recording system comprising: a data acquisition unit having a plurality of input ports, each input port being connected for receiving one of said applied parametric flight data and aircraft performance signals, said data acquisition unit including means for sequentially accessing selected ones of said applied parametric flight data and aircraft performance signals and for processing each accessed signal in response to an applied command signal, said data acquisition unit forther including means for supplying a digitally encoded signal representative of each accessed parametric flight data and aircraft performance signal; a central processing unit connected for receiving each of said digitally encoded signals supplied by said data acquisition unit, said data acquisition unit being responsive to program instructions to sequentially supply said command signals to said data acquisition unit and being responsive to program instructions to detect the time at which a plurality of predetermined aircraft procedures are undertaken, said central processing unit further being responsive to program instructions to process said digitally encoded signals supplied by said data acquisition unit to supply a single set of digitally encoded signals representative of selected aircraft performance information each time a procedure of said plurality of predetermined aircraft procedures is undertaken; program memory means for storage of said program instructions, said program memory means being connected to said central processing unit, said program memory means including programmable read only memory for storing program instructions that sequence said central processing unit for adapting said data acquisition unit to the specific parametric flight data and aircraft performance signals applied to said data acquisition unit, said program memory means further including memory for storing program instructions for sequencing said central processing unit for sequential access and processing of selected ones of said parametric flight data and aircraft performance signals; and nonvolatile memory means for temporary storage of the sets of digitally encoded signals supplied by said central processing unit.

이 특허를 인용한 특허 (139)

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IPC	Description
A	생활필수품
A62	인명구조; 소방(사다리 E06C)
A62B	인명구조용의 기구, 장치 또는 방법(특히 의료용에 사용되는 밸브 A61M 39/00; 특히 물에서 쓰이는 인명구조 장치 또는 방법 B63C 9/00; 잠수장비 B63C 11/00; 특히 항공기에 쓰는 것, 예. 낙하산, 투출좌석 B64D; 특히 광산에서 쓰이는 구조장치 E21F 11/00)
A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

내보내기 구분	파일저장 인쇄 메일전송
구성항목	기본정보 상세정보 관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표IPC 관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 공고번호, 공고일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표출원인, 출원인국적, 출원인주소, 발명자, 발명자E, 발명자코드, 발명자주소, 발명자 우편번호, 발명자국적, 대표IPC, IPC코드, 요약, 미국특허분류, 대리인주소, 대리인코드, 대리인(한글), 대리인(영문), 국제공개일자, 국제공개번호, 국제출원일자, 국제출원번호, 우선권, 우선권주장일, 우선권국가, 우선권출원번호, 원출원일자, 원출원번호, 지정국, Citing Patents, Cited Patents
저장형식	Text(ASCII format) Excel format PIAS분석(.xls)
메일정보	받는사람 (필수) @ 보내는사람 (선택) @ 제목 내용 KISTI 검색결과 이메일 서비스
안내	총 건의 자료가 검색되었습니다. 다운받으실 자료의 인덱스를 입력하세요. (1-10,000) 검색결과의 순서대로 최대 10,000건 까지 다운로드가 가능합니다. 데이타가 많을 경우 속도가 느려질 수 있습니다.(최대 2~3분 소요) 다운로드 파일은 UTF-8 형태로 저장됩니다. 파일의 내용이 제대로 보이지 않을실 때는 웹브라우저 상단의 보기 -> 인코딩 -> 자동선택 여부를 확인하십시오. ~ Text(ASCII format) Excel format

연합인증

Aircraft data acquisition and recording system 원문보기

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Aircraft data acquisition and recording system 원문보기

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