GB603383A - Improvements in and relating to flight instruments - Google Patents
Improvements in and relating to flight instrumentsInfo
- Publication number
- GB603383A GB603383A GB27503/45A GB2750345A GB603383A GB 603383 A GB603383 A GB 603383A GB 27503/45 A GB27503/45 A GB 27503/45A GB 2750345 A GB2750345 A GB 2750345A GB 603383 A GB603383 A GB 603383A
- Authority
- GB
- United Kingdom
- Prior art keywords
- climb
- rate
- indicator
- dive
- bank
- 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
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/02—Rotary gyroscopes
- G01C19/42—Rotary gyroscopes for indicating rate of turn; for integrating rate of turn
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Force Measurement Appropriate To Specific Purposes (AREA)
- Measuring Fluid Pressure (AREA)
Abstract
603,383. Aircraft instruments. JACK & HEINTZ, Inc. Oct. 19, 1945, No. 27503. Convention date, Nov. 2, 1944. [Classes 97 (ii) and 97 (iii)] [Also in Group XIX] The dial has a number of separate windows with movable indicators, indicating respectively climb or dive, bank, air-speed, rate of turn and rate of dive or climb. The rate of turn indicating pointer 2 extends from a gyroscope, constrained by an adjustable spring, damped by a dashpot, and housed at the rear of the instrument casing. The climb or dive indicator 8 and bank indicators 10, 11 consist of transparent tubular loops arranged in the fore-and-aft and transverse vertical planes respectively and half filled with liquid. The air-speed indicator 5 and rate of climb indicator 7 are operated respectively by a bellows subject internally to the dynamic pressure and externally to the static pressure of a pitot head and by a bellows with a leak subject externally to the static pressure (see Group XIX). An index member 9 co-operating with the climb indicator 8 may be vertically adjusted from the knob 60.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US603383XA | 1944-11-02 | 1944-11-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB603383A true GB603383A (en) | 1948-06-15 |
Family
ID=22028879
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB27503/45A Expired GB603383A (en) | 1944-11-02 | 1945-10-19 | Improvements in and relating to flight instruments |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB603383A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2920603A (en) * | 1958-02-28 | 1960-01-12 | Fremont W Burger | Attitude reference device |
| US2941400A (en) * | 1955-09-29 | 1960-06-21 | James O Nesbitt | Pilot's flight control indicator |
-
1945
- 1945-10-19 GB GB27503/45A patent/GB603383A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2941400A (en) * | 1955-09-29 | 1960-06-21 | James O Nesbitt | Pilot's flight control indicator |
| US2920603A (en) * | 1958-02-28 | 1960-01-12 | Fremont W Burger | Attitude reference device |
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