GB1352956A - Aircraft instrumentation apparatus - Google Patents

Aircraft instrumentation apparatus

Info

Publication number
GB1352956A
GB1352956A GB4812572A GB4812572A GB1352956A GB 1352956 A GB1352956 A GB 1352956A GB 4812572 A GB4812572 A GB 4812572A GB 4812572 A GB4812572 A GB 4812572A GB 1352956 A GB1352956 A GB 1352956A
Authority
GB
United Kingdom
Prior art keywords
specific energy
aircraft
manoeuvre
altitude
oct
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
GB4812572A
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.)
Honeywell Inc
Original Assignee
Honeywell Inc
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
Application filed by Honeywell Inc filed Critical Honeywell Inc
Publication of GB1352956A publication Critical patent/GB1352956A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06GANALOGUE COMPUTERS
    • G06G7/00Devices in which the computing operation is performed by varying electric or magnetic quantities
    • G06G7/48Analogue computers for specific processes, systems or devices, e.g. simulators
    • G06G7/78Analogue computers for specific processes, systems or devices, e.g. simulators for direction-finding, locating, distance or velocity measuring, or navigation systems
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C23/00Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • Computer Hardware Design (AREA)
  • General Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Mathematical Physics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Navigation (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

1352956 Aircraft instrument HONEYWELL Inc 19 Oct 1972 [21 Oct 1971 4 Nov 1971] 48125/72 Heading B7W An aircraft instrument determines and displays a signal related to the specific energy, that is, the total energy per unit weight, of the aircraft. The specific energy, calculated from the altitude and airspeed measured by sensors (10), (11), Fig. 1 (not shown) is indicated on a meter (18) by a pointer 32 on a scale 33, and the optimum Mach number in accordance with a minimum time manoeuvre schedule is indicated on a concentric scale 34, while further concentric scales 35, 36 indicate respectively the maximum safe Mach number or altitude obtainable in a constant energy diving or climbing manoeuvre. A further meter (26) indicates the rate of change of specific energy calculated from the airspeed and the flight path acceleration, which is in turn determined from the accelerations along and normal to the flight path and the angle of attack, as measured by sensors (12), (14) and (13).
GB4812572A 1971-10-21 1972-10-19 Aircraft instrumentation apparatus Expired GB1352956A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US19122271A 1971-10-21 1971-10-21
US19574471A 1971-11-04 1971-11-04

Publications (1)

Publication Number Publication Date
GB1352956A true GB1352956A (en) 1974-05-15

Family

ID=26886868

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4812572A Expired GB1352956A (en) 1971-10-21 1972-10-19 Aircraft instrumentation apparatus

Country Status (5)

Country Link
DE (1) DE2250747A1 (en)
FR (1) FR2156809B3 (en)
GB (1) GB1352956A (en)
IT (1) IT972374B (en)
NL (1) NL7214159A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4127249A (en) * 1977-02-07 1978-11-28 The Boeing Company Apparatus for computing the rate of change of energy of an aircraft
WO1984001345A1 (en) * 1982-09-30 1984-04-12 Boeing Co Total energy based flight control system

Also Published As

Publication number Publication date
FR2156809B3 (en) 1975-11-28
IT972374B (en) 1974-05-20
NL7214159A (en) 1973-04-25
FR2156809A1 (en) 1973-06-01
DE2250747A1 (en) 1973-04-26

Similar Documents

Publication Publication Date Title
US4590475A (en) Stall avoidance system for aircraft
US3077110A (en) System for monitoring the take-off performance of an aircraft
JPS5934559B2 (en) wind shear indicating device
US3222926A (en) Air mass relative motion meter
US3789661A (en) Aircraft glide angle and rate of change of total energy indication means
GB886136A (en) Improvements in or relating to visual indicating devices for use in aircraft
US3774017A (en) Apparatus and method for achieving optimum performance of an airplane
US3748900A (en) Rate of change of energy indicator
GB921216A (en) Aircraft take-off safety indicating device
GB1352956A (en) Aircraft instrumentation apparatus
US3188861A (en) Aircraft performance indicating apparatus
US2177244A (en) Anemometer with altitude correction
GB1334680A (en) Read-out instrument for an aircraft collis2on avoidance system
US4413321A (en) Rapid detector of a wind gradient
GB913840A (en) Improvements in or relating to airborne glide slope director systems
US3152248A (en) Indicator device for vertical landings
GB919360A (en) Aircraft take-off performance monitoring apparatus
US3205707A (en) Performance meter
US3280625A (en) Projected optimum flight path landing assist system
GB774327A (en) Means for indicating equivalent airspeed
US3895528A (en) Aircraft instrumentation displays
US3213683A (en) Aircraft critical acceleration indicating device
GB928946A (en) Sensing flight conditions
GB938081A (en) Improvements in or relating to pilot static pressure sensing devices
US3120756A (en) Acoustic probe

Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee