GB978029A - Improvements in or relating to automatic controlling devices for the altitude of flight vehicles - Google Patents

Improvements in or relating to automatic controlling devices for the altitude of flight vehicles

Info

Publication number
GB978029A
GB978029A GB13916/63A GB1391663A GB978029A GB 978029 A GB978029 A GB 978029A GB 13916/63 A GB13916/63 A GB 13916/63A GB 1391663 A GB1391663 A GB 1391663A GB 978029 A GB978029 A GB 978029A
Authority
GB
United Kingdom
Prior art keywords
housing
gas
casing
april
rotor
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
GB13916/63A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bendix Corp
Original Assignee
Bendix Corp
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.)
Filing date
Publication date
Priority claimed from US18625262 external-priority patent/US3180592A/en
Application filed by Bendix Corp filed Critical Bendix Corp
Publication of GB978029A publication Critical patent/GB978029A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

978,029. Gyroscopic apparatus. BENDIX CORPORATION. April 8, 1963 [April 9, 1962; April 20, 1962], No. 13916/63. Heading G1C. [Also in Division G3] A gas spun rate gyro comprises a rotor housing 304, Fig. 7, supported in a sealed casing 302 by flexible members 410 and turning about an axis formed by a torque tube gas inlet 314 to the casing and a housing gas outlet 312 supported in a gas bearing 318. Rotation of the housing is damped by devices 135, 334 each comprising a cup shaped member 337 closed by a diaphragm 139 and having a restricted connection 141 with the casing, the diaphragms being connected to housing by flexible members 143, 145. Gas in the casing is supplied to the housing by two jets (not shown) to spin the rotor 106, Fig. 10. Gas is also supplied through ports 182, 184 so that the rotor is fully supported by gas in the housing. Rotation of the housing varies the gas supply to two jets of a control system (see Division G3). Specification 915, 918 is referred to.
GB13916/63A 1962-04-09 1963-04-08 Improvements in or relating to automatic controlling devices for the altitude of flight vehicles Expired GB978029A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US18625262 US3180592A (en) 1962-04-09 1962-04-09 Hot gas control device
US18914463A 1963-04-20 1963-04-20

Publications (1)

Publication Number Publication Date
GB978029A true GB978029A (en) 1964-12-16

Family

ID=26881907

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13916/63A Expired GB978029A (en) 1962-04-09 1963-04-08 Improvements in or relating to automatic controlling devices for the altitude of flight vehicles

Country Status (1)

Country Link
GB (1) GB978029A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0078893A2 (en) * 1981-11-10 1983-05-18 Rheinmetall GmbH Steerable projectile
GB2124373A (en) * 1982-07-23 1984-02-15 Pfister Gmbh Gyroscope device

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0078893A2 (en) * 1981-11-10 1983-05-18 Rheinmetall GmbH Steerable projectile
EP0078893A3 (en) * 1981-11-10 1983-12-14 Rheinmetall Gmbh Steerable projectile
US4541592A (en) * 1981-11-10 1985-09-17 Rheinmetall Gmbh. Wing-stabilized projectile
GB2124373A (en) * 1982-07-23 1984-02-15 Pfister Gmbh Gyroscope device

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