BR8506687A - Recinto para a unidade de referencia inercial de uma aeronave - Google Patents

Recinto para a unidade de referencia inercial de uma aeronave

Info

Publication number: BR8506687A
Authority: BR; Brazil
Prior art keywords: inerial; aircraft; enclosure; reference unit; unit
Prior art date: 1984-04-20

Application number

BR8506687A

Other languages

English (en)

Inventor

William S Nye

Original Assignee

Sundstrand Data Control

Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)

1984-04-20

Filing date

1985-04-18

Publication date

1986-04-15

1985-04-18 Application filed by Sundstrand Data Control filed Critical Sundstrand Data Control

1986-04-15 Publication of BR8506687A publication Critical patent/BR8506687A/pt

Classifications

- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D43/00—Arrangements or adaptations of instruments

Landscapes

Engineering & Computer Science (AREA)
Aviation & Aerospace Engineering (AREA)
Cooling Or The Like Of Electrical Apparatus (AREA)
Control Of Motors That Do Not Use Commutators (AREA)

BR8506687A 1984-04-20 1985-04-18 Recinto para a unidade de referencia inercial de uma aeronave BR8506687A (pt)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
US60242184A	1984-04-20	1984-04-20
PCT/US1985/000688 WO1985004847A1 (en)	1984-04-20	1985-04-18	Enclosure for an aircraft inertial reference unit

Publications (1)

Publication Number	Publication Date
BR8506687A true BR8506687A (pt)	1986-04-15

Family

ID=24411282

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BR8506687A BR8506687A (pt)	1984-04-20	1985-04-18	Recinto para a unidade de referencia inercial de uma aeronave

Country Status (6)

Country	Link
EP (1)	EP0181370A4 (pt)
JP (1)	JPS61501944A (pt)
AU (1)	AU4355785A (pt)
BR (1)	BR8506687A (pt)
IT (1)	IT1215614B (pt)
WO (1)	WO1985004847A1 (pt)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US5309315A (en) *	1991-08-09	1994-05-03	Pulse Embedded Computer Systems, Inc.	Severe environment enclosure with thermal heat sink and EMI protection
ES2099015B1 (es) *	1994-03-28	1997-12-16	Ford Motor Co	Sensor de flujo de aire de montaje a distancia.
US8711223B2 (en)	2011-06-21	2014-04-29	Flir Systems, Inc.	Vehicle-mounted camera stabilized passively by vibration isolators

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB543917A (en) *	1940-10-19	1942-03-19	Metalastik Ltd	Improvements relating to resilient mountings for machines and instruments
US2470185A (en) *	1945-05-29	1949-05-17	Lawrence N Barry	Vibration isolator
US3140538A (en) *	1960-01-20	1964-07-14	Stewart Warner Corp	Method of forming a brazed joint
US3139679A (en) *	1961-05-16	1964-07-07	Saj Stanley	Method for forming heat-exchange devices
US3212564A (en) *	1962-10-05	1965-10-19	Harry M Passman	Heat conductive resiliently compressible structure for space electronics package modules
US3368117A (en) *	1966-06-13	1968-02-06	Ncr Co	Voltage distribution circuit arrangements for high-density packaging of electronic systems
US3575335A (en) *	1968-10-23	1971-04-20	Custom Glass Ltd	Apparatus for making window spacer corner connections
US3631325A (en) *	1970-06-15	1971-12-28	Sperry Rand Corp	Card module and end wall treatment facilitating heat transfer and sliding
DE2443122B2 (de) *	1974-09-09	1979-05-17	Siemens Ag, 1000 Berlin Und 8000 Muenchen	Gerät für die Hochfrequenz- und Nachrichtentechnik
US4125017A (en) *	1977-07-29	1978-11-14	Mcdonnell Douglas Corporation	Redundant inertial measurement system
US4212443A (en) *	1978-05-18	1980-07-15	Sperry Corporation	Strapped down attitude and heading reference system for aircraft employing skewed axis two-degree-of-freedom rate gyros
US4236190A (en) *	1978-05-31	1980-11-25	Hollingsead-Pryor Enterprises, Inc.	Electrical connector structure
US4454566A (en) *	1981-11-27	1984-06-12	Bell Telephone Laboratories, Incorporated	Heat removal from cabinets housing electronic equipment
US4562978A (en) *	1983-11-21	1986-01-07	Sperry Corporation	Adjustable mounting tray for aircraft inertial reference units and the like

1985
- 1985-04-18 JP JP60502091A patent/JPS61501944A/ja active Pending
- 1985-04-18 EP EP19850902302 patent/EP0181370A4/en not_active Withdrawn
- 1985-04-18 AU AU43557/85A patent/AU4355785A/en not_active Abandoned
- 1985-04-18 WO PCT/US1985/000688 patent/WO1985004847A1/en not_active Application Discontinuation
- 1985-04-18 BR BR8506687A patent/BR8506687A/pt unknown
- 1985-04-19 IT IT8547979A patent/IT1215614B/it active

Also Published As

Publication number	Publication date
AU4355785A (en)	1985-11-15
WO1985004847A1 (en)	1985-11-07
EP0181370A1 (en)	1986-05-21
JPS61501944A (ja)	1986-09-04
IT1215614B (it)	1990-02-22
EP0181370A4 (en)	1986-09-15
IT8547979A0 (it)	1985-04-19

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